Robinson R-66 Series Lithium-Ion Скачать руководство пользователя страница 37

Страница: 37 / 950

Page 5 of 5

R00015LA

NOTE 4.

Deleted as of March 10, 2015.

NOTE 5.

Any cockpit instruments installed by a 3

party must be marked with limit markings and range

markings in accordance with Robinson’s marking scheme.

NOTE 6.

Deleted as of March 10, 2015.

NOTE 7.

Exemption No. 9589, dated January 28, 2008, has been removed since Robinson Helicopter

Company was granted an Equivalent Level of Safety (ELOS) finding to CFR §27.695(a)(1), Number

AT14992LA-R-S-1, dated February 20, 2013. The exemption allowed a powered flight control

system without considering the jamming of a control valve as a possible single failure. There is no

impact to R66 helicopters that have been delivered or are in service.

NOTE 8.

R66 helicopters equipped with the G132 Cargo Hook installation may be operated at up to 2900

pounds gross weight when the portion above 2700 pounds is jettisonable load on the cargo hook and

the helicopter is operating at or below 7000 feet density altitude. See Cargo Hook Supplement to

R66 Pilot’s Operating Handbook and FAA Approved Rotorcraft Flight Manual (RTR 661) for

additional operating limitations.

--- END ---

JUL 2020

Chapter 4 Airworthiness Limitations

Page 4.7

Содержание R-66 Series Lithium-Ion

Страница 1: ...RS Monday through Friday 7 30 a m to 4 30 p m Pacific Time Lunch hour is 11 30 a m to 12 30 p m HOLIDAYS Please visit www robinsonheli com for a complete list of holidays and company shutdowns CUSTOMER SUPPORT AND SPARES ORDERS Please visit www robinsonheli com for a complete service directory Procure parts from any R66 Dealer or Service Center or order directly from RHC Customer Service via email...

Страница 2: ... AND RENEWAL FORMS Subscription order and renewal forms are located at www robinsonheli com WARRANTY INFORMATION Helicopter and parts warranty information is located at www robinsonheli com Page ii Introduction APR 2019 ...

Страница 3: ... Furnishings Chapter 28 Fuel System Chapter 29 Hydraulics Chapter 32 Landing Gear Chapter 33 Lights Chapter 52 Doors and Windows Chapter 53 Fuselage Chapter 62 Main Rotor Chapter 63 Main Rotor Drive System Chapter 64 Tail Rotor Chapter 65 Tail Rotor Drive System Chapter 67 Flight Controls Chapter 71 Powerplant Chapter 75 Engine Air Systems Chapter 76 Engine Controls Chapter 79 Engine Oil System Ch...

Страница 4: ...Intentionally Blank Page iv Introduction JUL 2020 ...

Страница 5: ...ormation detailed in this form Recommended changes may include but are not limited to general comments corrections omitted information or clarification of instructions Please send recommendations to Email techpubs robinsonheli com Phone 310 539 0508 Fax 310 539 5198 Robinson Helicopter Company Attention Technical Publications 2901 Airport Drive Torrance CA 90505 6115 UNITED STATES Date Publication...

Страница 6: ...Intentionally Blank Page vi Introduction APR 2017 ...

Страница 7: ... Parts Catalog References 1 3 1 60 Definitions and Abbreviations 1 4 1 70 Service Information 1 4B 1 71 Part Designation 1 4B 1 72 Returning Parts 1 4B 1 73 Ordering and Shipping 1 4B 1 74 Warranty Claims 1 4B 1 75 Customer Service Directory 1 4B 1 80 Assembly Instructions for R66 Helicopter Crated for Export 1 5 1 90 Helicopter Servicing 1 11 1 91 Scheduled Maintenance and Inspections 1 11 1 92 A...

Страница 8: ...Intentionally Blank Page 1 ii Chapter 1 General JUL 2020 ...

Страница 9: ...ts obsolescence equipment upgrades or provisions for upgrades Kit instructions issued by RHC either implement approved type design data or are approved as type design data The R66 Maintenance Manual is formatted in Air Transport Association of America Specification No 100 ATA 100 Style content and structure deviates from ATA 100 when necessary for clarity and for logic of presentation A list of ch...

Страница 10: ...k PDF forms may be used for R22 series R44 series and R66 Turbine helicopters Component Record blank PDF forms may be used for life limited or TBO components Blank paper copies are available for purchase P N R8478 Airframe Maintenance Record and P N R8479 Component Record pack of 20 A Component Record is a maintenance record of the removals installations or maintenance performed on a life limited ...

Страница 11: ...ustrated Parts Catalog References Maintenance Manual and Illustrated Parts Catalog Section and Figure references are subject to relocation and renumeration Effort will be made at the time of RHC technical document revisions to correct superseded references however certain documents may not otherwise require revision and superseded references may remain A keyword or part number search in online doc...

Страница 12: ...he preceding 12 calendar months Datum An imaginary vertical plane from which all horizontal measurements are taken for balance purposes with the aircraft in level flight attitude Refer to 6 20 for R66 datum location Empty Weight Empty Weight includes the weight of the airframe powerplant required and installed equipment fixed ballast unusable fuel and gearbox oil Refer to R66 Turbine Type Certific...

Страница 13: ... Butt Line Station locations LED Light Emitting Diode LH Left hand LRU Line Replaceable Unit MRDS Main Rotor Drive Shaft MRGB Main Rotor Gearbox OEM Original Equipment Manufacturer PTG Power Turbine Governor R66 IPC R66 Illustrated Parts Catalog R66 MM R66 Maintenance Manual R66 POH R66 Pilot s Operating Handbook RBL Right Butt Line Station locations RH Right hand RHC Robinson Helicopter Company R...

Страница 14: ...t weldments for hydraulic R44s Similarly part numbers F049 6 and F049 06 are not interchangeable because the dash numbers are different 1 72 Returning Parts All parts shipped to RHC must include a signed Component Return Authorization CRA Form available online at www robinsonheli com 1 73 Ordering and Shipping Procure parts from any R66 Dealer or Service Center or order directly from assigned RHC ...

Страница 15: ...through the door Remove main rotor gearbox mounting hardware nylon spacers and upper frame strut assemblies 5 Remove top of main rotor gearbox crate and position crate so gearbox is upright Refer to Section 7 20 Install hoisting equipment and lifting fixture or nylon rope on main rotor hub Remove hoist slack to support gearbox remove lag bolts securing gearbox to wooden divider and carefully hoist...

Страница 16: ...Page 1 6 Chapter 1 General R66 Maintenance Manual SEP 2012 FIGURE 1 1 ASSEMBLY INSTRUCTIONS FOR R66 HELICOPTER CRATED FOR EXPORT FIGURE 1 2 ASSEMBLY INSTRUCTIONS FOR R66 HELICOPTER CRATED FOR EXPORT ...

Страница 17: ...e F237 1 tailcone frame weldment and F305 5 aft inlet Install tail rotor drive fan shaft fanwheel installed through scroll assembly Install hardware securing aft inlet to scroll assembly Verify security 12 Refer to IPC Figure 65 1 Install hardware securing C947 3 plate assembly to F908 1 yoke and tail rotor drive fan shaft Standard torque bolts and palnuts per 20 32 and torque stripe per Figure 5 ...

Страница 18: ...tic Compass Installation 1 Locate airframe wiring in windshield center bow install 2 inch length of B158 3 heat shrink over wiring and connect compass pins to airframe sockets polarity is not critical Slide heat shrink over connection and apply heat Install 4 screws securing compass to mount securing wiring atop compass 21 Connect battery per 96 10 NOTE Check battery open circuit voltage and perfo...

Страница 19: ...3 step 1 DO NOT proceed into forward flight 34 Track and balance main rotor per 18 12 35 While climbing at maximum continuous torque 60 KIAS a Evaluate vibration level and controllability b Perform momentary 30 left yaw to check for adequate directional control 36 Level flight at 2000 feet density altitude deviate as required for weather and terrain maximum continuous torque a Evaluate longitudina...

Страница 20: ...0 Series Operation and Maintenance Manual OMM perform maintenance and inspection Service inlet barrier filter per 71 21 Replace main gearbox oil per 12 11 Drain and flush tail rotor gearbox per 12 23 Replace hydraulic filter per 12 32 Clean gearbox chip detectors per 12 13 12 22 Lubricate swashplate bearings per 12 90 Perform 2000 hour inspection per 5 50 Perform main gearbox internal visual inspe...

Страница 21: ...ctions in addition to the requirements in Table 1 Aircraft maintenance records Manufacturers Service Bulletins SBs Aviation regulations Airworthiness Limitations Airworthiness Directives ADs Preventive maintenance is required between scheduled inspections Fluid leaks discoloration fretting galling chafing nicks scratches dents cracks and corrosion all warrant further investigation Unairworthy item...

Страница 22: ...bly Perform inspection and repair per 62 22 return to RHC for inspection and repair or replace with new C005 13 Main Rotor Blade and Spindle Assembly Submit to RHC authorized component maintenance facility for 12 year maintenance or replace with new or overhaul exchange 12 year maintenance includes blade replacement boot and o ring replacement spindle bearing replacement as required pitch horn scr...

Страница 23: ...ew F018 1 Clutch Assembly Revision C prior Replace with new or overhaul exchange clutch assembly F018 1 Clutch Assembly Revision D subsequent Submit to RHC for 12 year maintenance or replace with new or overhaul exchange 12 year maintenance includes seal replacement o ring replacement and inspection F121 3 5 7 Push Pull Tube Assembly Disassemble and visually inspect exterior and interior Verify no...

Страница 24: ...18 1 thru 8 19 or 20 Elastic Cord Assembly Replace with new Dash number is selected during flight test evaluation A947 2 Flex Plate Assembly engine driveline Replace with new B173 5 V Belt Compressor Drive cabin air conditioning Replace with new B277 32 Clamp inducer bleed hose at engine Replace with new C005 4 Main Rotor Hub C154 1 Bearing Assembly Replace with new C005 13 Main Rotor Blade and Sp...

Страница 25: ...new or overhaul exchange pump assembly D918 1 Elastic Cord Longitudinal cyclic pivot Replace with new D918 2 Elastic Cord Lateral cyclic pivot Replace with new D918 3 Elastic Cord collective Replace with new D930 2 Spring Safety FCU throttle input Replace with new F006 1 6 Main Rotor Gearbox Assembly Replace with new or overhaul exchange F006 1 or F006 6 gearbox assembly as required F018 1 Clutch ...

Страница 26: ... on helicopter S N 0222 and prior Replace with new A880 908 or AN815 8D Union Oil Tank Vent at engine Replace with new A880 910 or AN815 10D Union Engine Oil Inlet Replace with new MS16562 4 Spring Pin at D333 13 fitting on PTG lever Replace with new MS29512 10 Packing left rollover valve Replace with new NAS1149E0363R Washer at A462 4 fittings Replace with new NAS557 32A Grommet Firewall engine d...

Страница 27: ...engine for Rolls Royce maintenance facility per 71 11 as required D Airframe and Engine Accessory Maintenance Refer to accessory manufacturer s instructions for continued airworthiness for accessory maintenance Remove accessories per R66 Maintenance Manual or RR300 Operation and Maintenance Manual OMM as applicable JUL 2020 Chapter 1 General Page 1 17 ...

Страница 28: ...Intentionally Blank Page 1 18 Chapter 1 General JUL 2020 ...

Страница 29: ... Title Page 4 10 Life Limited Components 4 1 4 11 Time in Service Records 4 1 4 12 Fatigue Life Limited Parts 4 2 4 20 Type Certificate Data Sheet TCDS 4 2 4 30 Airworthiness Limitations 4 9 JUL 2020 Chapter 4 Airworthiness Limitations Page 4 i ...

Страница 30: ...Intentionally Blank Page 4 ii Chapter 4 Airworthiness Limitations JUL 2020 ...

Страница 31: ...ut a storage limit specified in 10 20 calendar time in service begins on the date of the RHC issued Airworthiness Approval Tag Authorized Release Certificate issued with the invoice If a component or an inspection is scheduled for hourly and calendar intervals comply with whichever requirement comes first then reset interval unless otherwise specified Engine life is limited by engine time in servi...

Страница 32: ... requirement and the accumulated cycles and or time in service are known but the helicopter type is unknown the shorter life limit or overhaul requirement must be used Listed items ref 4 30 must be removed from the helicopter at the specified intervals and permanently retired from service preferably by destroying or damaging each part so it cannot inadvertently be returned to service 4 20 Type Cer...

Страница 33: ...C300 A1 Type Certificate number E4CE Fuel Jet A or Jet A 1 conforming to ASTM D 1655 Jet B conforming to ASTM D 6615 JP 4 or JP 5 conforming to MIL DTL 5624 JP 8 conforming to MIL DTL 83133 Engine Limits Power Ratings at N2 speed of 6016 rpm 100 rpm Maximum continuous 224 hp 83 Torque Takeoff 5 minute 270 hp 100 Torque Maximum speeds Output shaft N2 101 6076 rpm Gas producer shaft N1 105 53519 rpm...

Страница 34: ... Center of Gravity C G Range Notes 1 Straight line variation between points shown 2 Lateral C G limits valid for all gross weights 3 See R66 Pilot s Operating Handbook and FAA Approved Rotorcraft Flight Manual RTR 661 for expanded limits with external load Empty Weight C G Range None The aircraft s empty weight and empty weight C G must be determined by the procedures in Chapter 8 of the R66 Maint...

Страница 35: ...eight is 250 lb at STA 103 0 in for Police and Electronic News Gathering versions Maximim weight is 100 lb at STA 117 0 in with auxiliary fuel tank installed Maximum loading density is 50 lb ft2 Underseat baggage compartments Forward seats Maximum weight is 50 lb at STA 42 0 in Rear seats Maximum weight is 50 lb at STA 82 0 in Note For any seat location the maximum combined weight of the load on t...

Страница 36: ...torcraft Flight Manual is required R66 Pilot s Operating Handbook and FAA Approved Rotorcraft Flight Manual RTR 661 dated October 25 2010 or later approved revision GENERAL NOTES NOTE 1 A current weight and balance report including a list of equipment included in the certificated empty weight and loading instructions when necessary must be provided for each aircraft at the time of original airwort...

Страница 37: ...ion allowed a powered flight control system without considering the jamming of a control valve as a possible single failure There is no impact to R66 helicopters that have been delivered or are in service NOTE 8 R66 helicopters equipped with the G132 Cargo Hook installation may be operated at up to 2900 pounds gross weight when the portion above 2700 pounds is jettisonable load on the cargo hook a...

Страница 38: ...Intentionally Blank Page 4 8 Chapter 4 Airworthiness Limitations JUL 2020 ...

Страница 39: ... Stabilizer 2000 Hours C154 1 Main Rotor Hub 2000 Hours C158 1 Main Rotor Spindle 2000 Hours C251 3 Main Rotor Shaft 2000 Hours C545 1 Gear Set Tail Gearbox 2000 Hours C545 2 Pinion Tail Gearbox 2000 Hours C647 12 Bearing Set Swashplate 2000 Hours D079 1 Tail Rotor Guard 2000 Hours D196 1 Tail Rotor Drive Shaft 2000 Hours F016 2 Main Rotor Blade 2000 Hours or 12 years1 F020 1 Upper Frame 2000 Hour...

Страница 40: ...Intentionally Blank Page 4 10 Chapter 4 Airworthiness Limitations JUL 2020 ...

Страница 41: ... Landing Gear Assembly 12 Year Inspection 5 39C 5 54 Hydraulic Reservoir 12 Year Inspection 5 39D 5 60 Special Maintenance and Inspections 5 41 5 61 Tail Skid Strike 5 41 5 62 Tail Rotor Strike 5 42 5 63 Main Rotor Strike 5 43 5 64 Rotor Engine Overspeed 5 44 5 65 Hard Landing 5 47 5 66 Dye Penetrant Inspection of F020 1 Upper Frame 5 48 5 67 Corrosion on F020 1 Upper Frame 5 48 5 68 Main Rotor Ge...

Страница 42: ...Page 5 ii Chapter 5 Inspections JUL 2020 CHAPTER 5 INSPECTIONS Continued Section Title Page 5 75 Inspection After Stabilizer Damage 5 52 ...

Страница 43: ...owing general procedures apply to R66 inspection When required magnetic particle inspection may be performed in accordance with ASTM E 1444 and MIL STD 1907 Fluorescent penetrant inspection may be performed in accordance with ASTM E 1417 and MIL STD 1907 5 31 Ball and Roller Bearings The first indication of bearing failure is usually an increase in bearing noise Noise will almost always start seve...

Страница 44: ...FIGURE 5 2 ROD END CENTERING Position rod ends for maximum rotation FIGURE 5 1 ROD END AND SPHERICAL BEARING PLAY LIMITS AND TORQUE STRIPE APPLICATION Page 5 2 Chapter 5 Inspections JUL 2020 ...

Страница 45: ...gh witness hole Refer to Figure 5 1 for maximum rod end extension when no witness hole is provided 4 Rod end jam nuts and palnuts must be torqued per 20 32 and torque striped per Figure 5 1 at the most visible position for pre flight inspection Torque stripe must extend across nuts to both rod end shank and push pull tube or pitch link barrel yoke support strut etc Torque stripes are subject to de...

Страница 46: ...Elastomer Fatigue Elastomer Oil Contamination Elastomer Overload FIGURE 5 3 ELASTOMERIC BEARING DAMAGE Page 5 4 Chapter 5 Inspections JUL 2020 ...

Страница 47: ...inch or cracks are present over more than 25 of elastomer face Avoid elastomer exposure to oil grease hydraulic fluid cleaning solvent and rust preventative fluids Immediately wash off contaminants with detergent and water Replace a contaminated bearing that exhibits swelling wavy edges or debonding Overload occurs when elastomer s tensile strength or rubber to metal bond strength is exceeded This...

Страница 48: ...cated temperature increase cannot be accounted for by a change in operating conditions carefully examine the component before further flight NOTE Telatemps can indicate erroneously if contaminated by a petroleum product typically appearing as white unactivated square s between darkened squares at each end replace any Telatemp indicating as such and clean area with acetone prior to installing Part ...

Страница 49: ...alnut as required and apply specified torque to fastener If fastener moves disassemble joint and inspect parts for damage such as fretting thread deformation hole elongation etc replace damaged parts If fastener does not move install new palnut as required standard torque per 20 32 Torque stripe fastener per 20 31 JUL 2020 Chapter 5 Inspections Page 5 7 ...

Страница 50: ...sistance but no binding or locking of control Verify power turbine governor rigging as follows a Turn battery switch on With collective full down hold beep switch actuator all the way down Have a second person verify the PTG reads approximately 45 b With collective full down hold beep switch actuator all the way up Have a second person verify the PTG reads approximately 65 Return actuator to nomin...

Страница 51: ...s illuminate when test button is depressed segments below have additional behaviors i LOW FUEL and 12 GAL FUEL segments take approximately two seconds before they illuminate due to a time delay in circuit If LOW FUEL segment illuminates immediately after test button depress a fault is indicated ii EMU segment will illuminate only when test button is depressed EMU segment takes approximately 10 sec...

Страница 52: ...High engine torque MGT a beeping tone will sound when test button is depressed four beeps per second for two seconds followed by 12 beeps per second Turn battery switch off 8 Aircraft Documents Additional documents may be required in countries other than the US a Inspect condition and verify R66 MT699 1 laminated pilot s checklist is current revision Check revision status online at www robinsonhel...

Страница 53: ...ero 9 Switch battery and generator OFF Verify dual tachometer continues to function then switch battery and generator back ON Ensure avionics master switch is OFF and depress annunciator panel Test button Both sides of dual tachometer should drop to off scale low indication while button is depressed 10 With avionics master switch OFF verify generator continues to supply power with battery OFF inst...

Страница 54: ...cel to 70 following rapid throttle closure should take at least 2 seconds 20 Check hydraulic system operation Using cyclic mounted hydraulics switch turn hydraulics OFF and verify HYD light on if equipped Using small longitudinal cyclic inputs there should be approximately one half inch of freeplay before encountering stiffness and feedback Turn hydraulics ON Controls should be free with no feedba...

Страница 55: ...nditions or nominal weight and CG in middle of envelope will provide the most useful evaluation a Verify tail rotor pedal position when yaw string is centered Right pedal 0 25 to 0 75 inch forward of left pedal b Verify tail rotor elastic trim cord zeros pedal forces cord applies left pedal force c Verify hydraulic system zeros cyclic stick forces and collective is balanced with no feedback d Veri...

Страница 56: ...nd record the following values a N1 b Torque 83 nominal c OAT d MGT e Pressure altitude f Oil pressure g Oil temperature h Determine max allowable MGT from power assurance chart i Calculate margin Margin Max allowable MGT Indicated MGT 4 Autorotation a Autorotate at 100 KIAS Verify normal control forces and flying characteristics 5 Shutdown a Perform POH Shutdown Procedure checklist b Verify rotor...

Страница 57: ...nt swashplate area or bearing seals with high pressure water or solvent as water or solvent may cause corrosion or breakdown of lubricants See RR300 Series Operation and Maintenance Manual OMM for engine cleaning instructions and precautions Access and Inspection Panels Refer to R66 Illustrated Parts Catalog Chapter 6 for access and inspection panel locations Remove or open necessary panels doors ...

Страница 58: ... scratches or dents or cracks in welds Verify security Fire Extinguisher and Mount Inspect condition Inspect fire extinguisher per manufacturer s instructions Verify no loss of charge or obstructions in extinguisher nozzle Verify security Map Holders Inspect condition Verify no defects tears or material deterioration Remove foreign objects and verify security License Holder Inspect condition Verif...

Страница 59: ... and verify no cracks Pay particular attention to area near NAS6603 13 bolts Replace any cracked support prior to flight Tail Rotor Controls Examine accessible portion with inspection light and mirror Inspect tail rotor control components for obvious defects Verify operating clearance Cabin Heater Hose Inspect condition Verify no collapsed areas or chafing Verify hose clamp and hose security Coppe...

Страница 60: ... Verify no corrosion or bends in bus bars Verify bus bar security and isolation from surrounding structure Wiring Inspect condition Verify no loose chafed or broken wires or terminals Verify neatness proper routing and installation and security Fasteners Torque Stripes Inspect condition Verify proper installation and security of fasteners Renew deteriorated torque stripes per Figure 5 1 Close Secu...

Страница 61: ...Verify no nicks scratches dents cracks or corrosion Verify no cracks in welds Verify security proper operating clearance and smooth actuation Verify security of co pilot control and locking pin Cyclic Boot Inspect condition Verify proper locking function of boot snaps Verify no defects tears or material deterioration Verify security Cyclic Friction Assembly Inspect condition Inspect link rod end b...

Страница 62: ...Intentionally Blank Page 5 16B Chapter 5 Inspections APR 2017 ...

Страница 63: ...Verify ty rap is properly installed loosely securing boot around collective stick Verify no defects tears or material deterioration Verify security Fuel Valve Knob and Guard Inspect condition Verify cable and mounting bezel security Verify proper adjustment and smooth operation of valve Verify guard is present Collective Friction Stop Assembly Inspect condition Verify no nicks scratches dents crac...

Страница 64: ... and adjustable controls Fasten cyclic collective and removable collective boot snaps HORIZONTAL CONTROL TUNNEL Aft seats Covers Inspect condition Verify marking legibility Antenna Wiring Connectors Inspect condition Verify no loose chafed frayed or broken wires Verify no damaged connectors Verify neatness proper routing and installation and security Cyclic Yoke Inspect condition Verify no cracks ...

Страница 65: ...d frayed or broken wires Verify proper installation and security of blower and evaporator components Evaporator Drain Tubes and Valve Air Conditioning if installed Remove middle seat assembly and cover and covers inside left and right seat compartments to access drain system Verify tubes are unobstructed Function check drain system by simultaneously squeezing drain tube and sediment tube near tee ...

Страница 66: ...r to 28 23 Visually inspect adapter for any obvious damage verify proper installation and security Inspect wiring for loose chafed frayed or broken wires Verify no damaged connectors Verify wiring neatness proper routing and installation and security Cabin Bulkhead Examine accessible portion with inspection light and mirror Verify no nicks scratches dents cracks corrosion or loose rivets Verify st...

Страница 67: ...t or replace battery per manufacturer s instructions Verify battery cable security Verify no corrosion in surrounding structure Lithium Ion Battery Installation if equipped Refer to 96 12 Inspect condition Verify no cracks or corrosion on or near battery terminals Verify vent hose comm connector wiring and battery cable security Perform scheduled maintenance as required Verify no corrosion in surr...

Страница 68: ... Cowling Doors Inspect condition Verify proper operation of fasteners Antenna Wiring Connectors Inspect condition Verify no loose chafed frayed or broken wires Verify no damaged connectors Verify neatness proper routing and installation and security Check grommets for proper installation Placards Verify placard legibility proper installation and security Refer to Chapter 11 Fuel Tank Examine acces...

Страница 69: ...st tube for cracks With ship on level ground verify correct oil level and cleanliness through sight gage and adjust or flush as required Verify security of Hall Effect senders and yoke magnets Inspect oil lines for leakage chafing or obvious damage Inspect oil pump mounting and fittings for leaking or obvious damage Inspect gearbox oil filter for leakage or for tripped bypass indicator Verify oil ...

Страница 70: ...and palnut and jam nut are tight Check witness holes for proper thread engagement Verify proper installation security and operating clearance Tail Rotor Push Pull Tube Forward Bellcrank Examine accessible portion with inspection light and mirror Inspect condition per 5 32 Verify no nicks scratches chafing dents cracks or corrosion Inspect rod end bearings per 5 33 verify rod ends are centered and ...

Страница 71: ...tion Inspect Telatemp per 5 35 Verify no significant leakage Verify proper installation and security Upper Steel Tube Frame Inspect condition Verify no nicks scratches dents cracks or corrosion Verify no chafing where wires hoses or clamps attach to frame Examine each weld for cracks with an inspection light and mirror CAUTION Upper steel tube frame is fatigue loaded and therefore susceptible to f...

Страница 72: ...lines Refrigerant Hose Assemblies Air Conditioning if installed Verify security no damage and clearance to adjacent structure Verify dust caps installed on service fittings where lines mount to compressor F196 1 Tail Rotor Drive Fan Shaft Inspect condition Verify no shaft corrosion Remove any light surface corrosion and apply wax or suitable corrosion inhibitor Verify no cracks corrosion or fretti...

Страница 73: ...led Inspect condition Comply with 14 CFR 91 207 d if required Verify proper installation security and clearance from drive train components Verify D693 4 strap assembly is installed and buckled securely Pitot Line Static Vent Inspect pitot and static lines for obstructions cracking chafing pinching or kinking Verify integrity of pitot and static line connections Verify line security Horizontal Fir...

Страница 74: ...ents cracks corrosion fretting or loose rivets Verify no leakage from fuel tanks Engine Oil Tank Inspect condition Verify no leakage or obvious damage to oil tank exterior Check tank interior for foreign objects Add oil as required per R66 POH Section 8 Verify tank security Tailcone Attachment Inspect condition Verify no cracks near fasteners attaching tailcone to upper frame Verify proper install...

Страница 75: ...ion Verify no cracks where antennas mount to cowling Verify security Close Secure Verify foreign objects are removed Verify equipment security Verify cleanliness of interior and of inspection and access doors and cowlings Connect antenna leads and ground wires if installed Install close doors and cowlings removed in preceding steps Verify security ...

Страница 76: ...Intentionally Blank Page 5 26 Chapter 5 Inspections APR 2019 ...

Страница 77: ...d per 71 21 Part D Verify proper installation and security Inlet Barrier Filter if installed Inspect condition Verify no tears punctures or damage to filter media or cage assembly verify no corrosion cracks or distortion to filter assembly components Service or replace filter assemblies as required per 71 21 Part E Note indication on filter maintenance aid Verify proper installation and security E...

Страница 78: ... maximum throttle stop with twist grip open Verify FCU cutoff lever rests in detent when control is OFF and has 0 030 0 090 inch clearance from maximum fuel stop when control is ON Fuel Filter Inspect condition service fuel filter per RR300 OMM as required Verify proper installation and security of wiring and housing Fuel Hose Inspect condition Verify no leakage chafing or obvious damage to fuel l...

Страница 79: ...l supports Verify security of desiccant cap Refrigerant Line Assemblies Air Conditioning if installed Inspect condition Verify security no damage and clearance to adjacent structure Wiring Inspect condition Verify no loose chafed or broken wires or terminals Check for heat or fluid damage Verify neatness proper routing and installation and security Fasteners Torque Stripes Inspect condition Verify...

Страница 80: ...herical bearings per 5 33 Verify proper installation security and operating clearance Verify tail rotor guard mounting screw shanks clear push pull tube Tail Rotor Drive Shaft Hanger Bearing Hanger Inspect condition Inspect bearing for obvious damage Verify integrity of bearing seals Verify bearing s inner race to drive shaft torque stripe is intact and no evidence of bearing slippage on shaft Ver...

Страница 81: ...nts to tailcone Verify lens cleanliness clarity and security Verify proper operation Tail Rotor Visual Warning Guard Inspect condition Verify no cracks where guard mounts to tailcone Inspect guard welds for cracks or corrosion Verify security Wiring Inspect condition Verify no loose chafed or broken wires or terminals Verify neatness proper routing and installation and security Fasteners Torque St...

Страница 82: ...perating clearance Tail Rotor Gearbox Inspect condition Verify gearbox to tailcone mounting security Verify no leakage at input or output seals chip detector vent plug filler assembly or sight gage With ship on level ground verify correct oil level and oil cleanliness through sight gage and adjust or flush as required Inspect Telatemp per 5 35 Inspect output shaft for nicks scratches dents cracks ...

Страница 83: ...ts at respective attachment points for balance purposes Verify proper installation of hat washers Verify proper installation security and operating clearance Tail Rotor Blades Inspect condition Inspect blade surfaces for excessive erosion nicks scratches buckling voids or debonding dents cracks or corrosion Refer to 64 30 for tap testing instructions and damage limitations Verify no fretting of ta...

Страница 84: ...clearance Pitot Tube Line Inspect pitot lines for obstructions cracking chafing pinching or kinking Verify integrity of pitot and static line connections Verify proper routing and security of pitot tube and line Verify no cracks where pitot tube mounts to mast fairing Verify no obstructions in pitot tube Fuel Vent Weldment and Tygon Tubes Inspect condition Verify no obstructions cracking chafing p...

Страница 85: ...ion light and mirror Verify no corrosion or debris between main rotor drive shaft and inside of slider tube Install swashplate boot lower ty rap Verify proper boot position security and operating clearance Swashplate Inspect condition Verify no nicks scratches gouges dents cracks or corrosion Verify 0 020 inch maximum radial play between swashplate ball and slider tube Rotate rotor by hand and ver...

Страница 86: ...perating clearance Blade Spindles Root Fittings Inspect condition Verify no cracks corrosion or obvious damage to blade spindles and horns Verify no cracks corrosion or missing paint in blade root fittings especially in area adjacent to inboard edges of skin and doublers Blade Boots Inspect condition Verify no boot defects tears material deterioration or pinholes resulting in oil leakage Verify pr...

Страница 87: ... if rain cap is loose or damaged verify no internal corrosion Note that one vent hole per cross tube is located near left or right end of tube to prevent pressurization Landing Gear Attach Points Inspect condition Verify no buckling cracks fretting or loose fasteners Inspect mounts and verify no loose swages or worn bearings Fasteners Torque Stripes Inspect condition Verify proper installation and...

Страница 88: ...lts or shoulder harnesses Verify no significant UV damage Check inertia reels for proper operation by pulling harness quickly to verify locking function Check buckles for proper operation Check belt and reel attachment points for security Verify no cracks in seat belt anchor welds Verify security NOTE TSO tag not required on factory installed harnesses Windshields Windows Inspect condition Verify ...

Страница 89: ...Verify proper operation of door latching and locking mechanisms Ensure door hinge pins are secured with cotter rings Verify security of hinge mounting screws Verify proper installation and operation of gas struts and door vent assembly SPECIAL EQUIPMENT Transmit and Intercom Switches Verify proper operation of special transmit and intercom switches PA Siren Speaker Inspect condition Verify no crac...

Страница 90: ...sonheli com under the Publications tab REQUIRED DOCUMENTS AND PLACARDS Documents Check that required documents Airworthiness Certificate Registration applicable Radio Station License Pilot s Operating Handbook Equipment List Weight Balance Data are onboard legible and current Placards Verify required placards are properly installed legible and current Refer to Pilot s Operating Handbook Section 2 ...

Страница 91: ...esidue microbial growth or damage to fabric Visually inspect adjacent structure for evidence of bladder leakage Replace roll over vent valve o rings and packings per 28 11 Remove any foreign object debris Install bladder s per Chapter 28 5 Perform engine driveline forward flex plate shimming per 63 11 and tail rotor driveline intermediate flex plate shimming per 65 30 6 Fill and bleed hydraulic sy...

Страница 92: ...g aircraft return to service 5 51 C258 5 Main Rotor Pitch Link Assembly Inspection 1 Temporarily mark each pitch link and associated swashplate ear with unique color Record overall lengths of both links 2 Remove pitch links 3 Disassemble pitch links keeping parts from each link separate from the other 4 Evaluate rod ends per 5 33 and replace as required 5 Visually inspect parts with 10X magnificat...

Страница 93: ...age is detected on either upper or lower swashplate Replace damaged parts 9 Perform swashplate tilting friction adjustment per 67 41 step 4 10 Lubricate swashplate bearings per 12 90 steps 7 thru 11 Install new upper seal during procedure 11 Remove rod end form upper fork Using non metallic tools remove majority of sealant in threaded hole of fork Visually inspect parts with 10X magnification for ...

Страница 94: ...ct exterior of struts using minimum 3X magnification for obvious damage Any corrosion on or adjacent to a weld requires corrosion paint removal followed by MPI Upon favorable MPI results apply 20 76 powder coat 9 Refer to 32 30 Visually inspect interior of skid tube with borescope or similar Visually inspect exterior of parts using minimum 3X magnification As required touch up coatings with 20 75 ...

Страница 95: ...itable clean plastic tube do not use metal tool Wipe out any residue from both traps with clean foam tip swab 3 Inspect interior of reservoir for corrosion with borescope or similar Replace reservoir if corrosion is detected 4 Perform hydraulic system drain and flush per 12 33 steps 2 thru 12 JUL 2020 Chapter 5 Inspections Page 5 39D FIGURE 5 5 HYDRAULIC RESERVOIR INSPECTION ...

Страница 96: ...Intentionally Blank Page 5 40 Chapter 5 Inspections JUL 2020 ...

Страница 97: ... lower vertical stabilizer perform the following inspections in addition to those listed in Step A 1 Perform tail rotor drive shaft runout per 65 21 2 Remove tailcone assembly per 53 40 Perform dye penetrant inspection of F020 upper frame at tailcone attach points per 5 66 3 Visually inspect tailcone attachment points for elongated holes 0 454 inch diameter maximum 4 Remove empennage assembly per ...

Страница 98: ...rotor gearbox per 65 40 and return to RHC c Visually inspect D224 tail rotor drive shaft for evidence of twisting nicks dents or scratches Nicks and scratches may be polished out to a maximum of 0 003 inch deep Evidence of twisting or dents is cause for replacement of the drive shaft d Remove yokes from each end of tail rotor drive shaft Inspect arms for deformation and holes for any elongation St...

Страница 99: ...e and requires a sudden stoppage inspection of the entire rotorcraft 2 If main rotor blade or blades have contacted ground or a solid object they must be inspected for sudden stoppage Sudden stoppage is evident when buckling or bending of the main rotor blades has occurred Use the following procedure for inspecting rotorcraft after main rotor sudden stoppage has occurred a Perform tail rotor drive...

Страница 100: ...ve shaft runout per 65 21 2 If an overspeed at or above 112 is reported or suspected or if balance changes or pitch bearing roughness is evident perform following inspections in addition to Part 1 NOTE Refer to Part 3 if a power on overspeed occurs a Perform Part 1 inspection b Check coning hinge bolts for evidence of bending Replace any bent bolts c Coning hinge bolts washers and journals must be...

Страница 101: ...Intentionally Blank APR 2019 Chapter 5 Inspections Page 5 45 ...

Страница 102: ...Page 5 46 Chapter 5 Inspections APR 2019 FIGURE 5 6 SYMMETRY CHECK ...

Страница 103: ... steel tube structure are evidence of side loads on the airframe 1 Yielding of cross tube due to hard landing with no side loads a Perform tail rotor drive shaft runout per 65 21 b Visually inspect main rotor blades for oil canning of skins and buckling Inspect and repair main rotor blades per 62 40 and 62 50 c Check landing gear cross tubes for yielding beyond serviceable limit Place rotorcraft o...

Страница 104: ... structure or tailcone are cause for replacement or factory repair h Replace parts as required i Check for symmetry if there is evidence of buckling of the cabin assembly per Figure 5 6 Position helicopter on a hard level surface with the weight of the helicopter settled on the skids Measure and record distances of lines A B C and D Verify the difference between lines A B is not more than 0 30 inc...

Страница 105: ...Intentionally Blank APR 2017 Chapter 5 Inspections Page 5 47B ...

Страница 106: ...ime 7 Refinish area with gray epoxy top coat or equivalent 5 67 Corrosion on F020 1 Upper Frame 1 Polish out corrosion on steel frame tube members a Polish out light surface corrosion on frame members using Scotchbrite or 400 grit wet or dry sandpaper Verify 0 002 inch maximum depth after rework b Polish out corrosion pitting using 320 grit wet or dry sandpaper Verify 0 004 inch maximum depth and ...

Страница 107: ... CHIP annunciator segment illuminates 1 Drain the gearbox per 12 21 straining the oil through a 190 micron or finer paint filter into a clean container 2 Inspect any particles found in the paint filter or on the chip detector Examine the particles for size any particles larger 0 09 inch long or 0 02 inch wide than fine fuzz normal wear should be identified as ferrous or non ferrous by using a magn...

Страница 108: ...ected in any of the above mentioned systems additional components may require replacement Contact RHC Technical Support with detailed documentation for further guidance prior to approving aircraft for return to service 5 73 Pop Out Float Equipped Helicopter Water Landing with Tail Rotor Contact 1 Clean tail rotor blades hub and airframe exterior with a mild soap and water solution per Chapter 20 C...

Страница 109: ... main gearbox filler plug 2 Via filler plug hole and using borescope miniature camera or smartphone camera with flash visually inspect specified area of gear carrier Rotate gearbox by hand turning main or tail rotor as required to view entire circumference 3 If no corrosion is evident install filler plug and special torque per 20 33 4 If corrosion is detected contact RHC Technical Support ...

Страница 110: ...stabilizer that results in denting tearing or cracking of stabilizer metal 1 On associated tailcone s aft casting strip paint from cross hatched surfaces shown in Figure 5 8 2 Perform fluorescent penetrant inspection FPI per ASTM E 1417 of stripped surfaces Replace tailcone if crack is indicated 3 Prime paint stripped surfaces per 20 60 FIGURE 5 8 CROSS HATCHED SURFACES OF TAILCONE S AFT CASTING ...

Страница 111: ...Compartment Dimensions 6 4 6 60 Station Diagrams 6 6 6 61 Fuselage Station FS Locations 6 6 6 62 Tailcone Station TS Locations 6 7 6 63 Water Line WL Station Locations 6 8 6 64 Butt Line BL Station Locations 6 9 6 70 Access and Inspection Panels 6 10 6 71 B526 Screws and B527 08 Washers 6 10 6 80 Antenna Locations 6 11 APR 2017 Chapter 6 Dimensions and Descriptions Page 6 i ...

Страница 112: ...Intentionally Blank Page 6 ii Chapter 6 Dimensions and Descriptions APR 2017 ...

Страница 113: ...e normally rated at 300 shaft horsepower SHP 270 SHP 5 minute take off rating Maximum gross weight 2700 pounds Primary fuel is Jet A see R66 Pilot s Operating Handbook 74 6 US gallon fuel tank capacity 6 20 Datum The datum is located 100 inches forward of main rotor centerline 6 30 Method of Measurement Fuselage station tailcone station water line station and butt line station values are measured ...

Страница 114: ...Intentionally Blank Page 6 2 Chapter 6 Dimensions and Descriptions R66 Maintenance Manual 25 OCT 2010 ...

Страница 115: ...FIGURE 6 1 EXTERNAL DIMENSIONS 6 40 External Dimensions 25 OCT 2010 R66 Maintenance Manual Chapter 6 Dimensions and Descriptions Page 6 3 ...

Страница 116: ...6 50 Baggage Compartment Dimensions FIGURE 6 2 BAGGAGE COMPARTMENT INTERIOR DIMENSIONS Dimensions given are approximate Page 6 4 Chapter 6 Dimensions and Descriptions R66 Maintenance Manual 25 OCT 2010 ...

Страница 117: ...RE 6 3 BAGGAGE COMPARTMENT ACCESS DIMENSIONS Dimensions given are approximate 6 50 Baggage Compartment Dimensions continued 25 OCT 2010 R66 Maintenance Manual Chapter 6 Dimensions and Descriptions Page 6 5 ...

Страница 118: ...ss Tube Forward centerline at strut FS 71 56 7 Baggage Compartment forward wall FS 92 00 8 Main Rotor Drive Shaft centerline FS 100 00 9 Fuel Cell Structure aft wall FS 115 00 10 Engine Firewall Vertical FS 125 00 11 Cross Tube Aft centerline at strut FS 127 35 12 Skid Extension aft edge FS 134 78 13 Engine Cowling aft point FS 171 45 FIGURE 6 4 FUSELAGE STATION LOCATIONS Page 6 6 Chapter 6 Dimens...

Страница 119: ...00 3 Aft Edge C023 7 Skin Tailcone Centerline Intersection TS 51 00 4 Aft Edge C023 8 Skin Tailcone Centerline Intersection TS 74 00 5 Aft Edge C023 9 Skin Tailcone Centerline Intersection TS 98 00 6 Aft Edge C023 10 Skin Tailcone Centerline Intersection TS 122 00 7 Aft Edge C023 11 Skin Tailcone Centerline Intersection TS 146 00 8 Aft Edge C023 12 Skin TS 177 30 9 Tail Rotor Gearbox centerline FS...

Страница 120: ...rbox tail rotor and main rotor drive shaft intersection point WL 66 00 7 Baggage Compartment ceiling lowest point WL 45 60 8 Baggage Compartment floor WL 22 59 9 Belly WL 20 78 10 Landing Gear WL 0 79 11 Origin WL 0 00 6 63 Water Line WL Station Locations FIGURE 6 6 WATER LINE STATION LOCATIONS Page 6 8 Chapter 6 Dimensions and Descriptions R66 Maintenance Manual 25 OCT 2010 ...

Страница 121: ...3 Door Post between forward aft doors BL 28 25 4 Jack Lug Tab aft strut assembly BL 16 73 5 Ground Handling Ball jack point BL 4 13 6 Origin BL 0 00 7 Teeter Hinge Bolt tail rotor LBL 11 01 8 Jack Tab aft strut assembly LBL 16 73 JUL 2020 Chapter 6 Dimensions and Descriptions Page 6 9 6 64 Butt Line BL Station Locations ...

Страница 122: ...rchangeable with MS27039C080_ screws used to secure cowlings and access panels as follows PART INTERCHANGEABLE WITH MS27039C0806 screw B526 6 screw MS27039C0807 screw B526 8 screw MS27039C0808 screw B526 8 screw B526 screws are interchangeable with AN525 832R_ AN526C832R_ screws as follows PART INTERCHANGEABLE WITH AN525 832R6 or AN526C832R6 screw B526 6 screw AN525 832R7 or AN526C832R7 screw B526...

Страница 123: ... 118 329 335 D20543 VOR LOCALIZER 108 118 329 335 D20543 VOR LOCALIZER W DIPLEXER 11 ELT AV 300 ITEM ANTENNA MHz PART NO 12 Cowling GPS GA 35 Cowling XM GA 55 13 Upper Fwd COM CI 121 CI 248 5 Upper Fwd FM CI 177 Upper Fwd FM 403 512 CI 273 CI 272 1 CI 271 800 870 CI 306 Upper Fwd COM GPS CI 2580 200 14 Upper Mid RSM GPS 921 00003 001 15 Upper Aft COM CI 121 CI 248 5 Upper Aft FM CI 177 Upper Aft F...

Страница 124: ...Intentionally Blank Page 6 12 Chapter 6 Dimensions and Descriptions APR 2017 ...

Страница 125: ...CHAPTER 7 JACKING AND HOISTING Section Title Page 7 10 Jacking 7 1 7 20 Hoisting 7 5 25 OCT 2010 R66 Maintenance Manual Chapter 7 Jacking and Hoisting Page 7 i ...

Страница 126: ...Intentionally Blank Page 7 ii Chapter 7 Jacking and Hoisting R66 Maintenance Manual 25 OCT 2010 ...

Страница 127: ...opter is raised A Jacking 1 Refer to Figure 7 1 Place one appropriate capacity jack under each landing gear aft strut assembly jack lug tab and under the ground handling ball Install jacking point adapters as required CAUTION Ground handling ball must slide unrestricted across a flat surface during jacking When weighing verify ball is not under side load which could produce an erroneous weight ind...

Страница 128: ...FIGURE 7 1 JACKING Page 7 2 Chapter 7 Jacking and Hoisting R66 Maintenance Manual SEP 2012 ...

Страница 129: ... 1 Refer to Figure 7 1 Slowly and simultaneously one person per jack recommended lower each jack ram maintaining helicopter stability Lower aircraft to ground 2 Clear jacks from lugs tabs and ball and clear equipment from area SEP 2012 R66 Maintenance Manual Chapter 7 Jacking and Hoisting Page 7 3 ...

Страница 130: ...FIGURE 7 2 HOISTING Page 7 4 Chapter 7 Jacking and Hoisting R66 Maintenance Manual SEP 2012 ...

Страница 131: ...ns through fixture and bushings until pins lock Verify security 4 Connect hoist to lifting fixture Verify security 5 Stabilize helicopter as required by guiding tail skid but do not exert force tail skid is secondary structure Raise helicopter to required height B Hoisting with Nylon Rope 1 Refer to Figure 7 2 Verify hoisting equipment has minimum load capacity of 3000 lbs Verify minimum work load...

Страница 132: ...ize helicopter as required by guiding tail skid but do not exert force tail skid is secondary structure Slowly lower aircraft to ground 2 Disconnect hoisting equipment remove lifting fixture or nylon rope from main rotor hub and clear equipment from area Page 7 6 Chapter 7 Jacking and Hoisting R66 Maintenance Manual 25 OCT 2010 ...

Страница 133: ...BALANCE Section Title Page 8 10 Leveling 8 1 8 11 Leveling for Weight and Balance 8 1 8 12 Leveling for Rigging 8 3 8 20 Weighing 8 5 8 21 Preparing Helicopter for Weighing 8 5 8 22 Weighing Procedure and Calculations 8 7 8 30 Fixed Ballast 8 11 8 31 Nose Ballast 8 11 8 32 Empennage Ballast 8 13 ...

Страница 134: ...Intentionally Blank Page 8 ii Chapter 8 Weight and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 135: ...ions 1 Jack helicopter per Section 7 10 2 Refer to Figure 8 1 Place a spirit level laterally on F463 1 aft tunnel cover Verify cover is flat if cover is not flat remove cover and place spirit level across keel panel flanges 3 Adjust jacks at landing gear aft strut assembly jack lugs tabs until helicopter is level laterally 4 Position spirit level longitudinally on aft tunnel cover or atop left or ...

Страница 136: ... 1 LEVELING FOR WEIGHT AND BALANCE Lateral shown view looking down between aft seat footwells Page 8 2 Chapter 8 Weight and Balance R66 Maintenance Manual SEP 2012 FIGURE 8 2 LEVELING FOR RIGGING Lateral shown ...

Страница 137: ... bolt at location marked LEVEL HERE on top of main rotor hub 4 Adjust jack at landing gear aft strut assembly jack lugs tabs until helicopter is level laterally 5 Release rotor brake and rotate main rotor until teeter hinge bolt is aligned with longitudinal axis of the helicopter Apply rotor brake Verify cyclic stick is in vertical position with friction applied 6 Adjust jack under ground handling...

Страница 138: ...Intentionally Blank Page 8 4 Chapter 8 Weight and Balance R66 Maintenance Manual SEP 2012 ...

Страница 139: ... the wind Weigh helicopter on a flat hard surface in a zero wind environment for accurate scale readings 8 21 Preparing Helicopter for Weighing 1 Defuel helicopter per Section 12 42 2 Service engine oil hydraulic fluid and main tail rotor gearboxes per Chapter 12 3 Clean aircraft per Section 20 10 Ensure helicopter is completely dry prior to weighing 4 Remove foreign objects from baggage compartme...

Страница 140: ...Page 8 6 Chapter 8 Weight and Balance R66 Maintenance Manual 25 OCT 2010 FIGURE 8 3 WEIGHING Scale indications for demonstration only ...

Страница 141: ... Figure 8 3 Place a jack and one 1000 lb capacity minimum scale under each landing gear aft strut assembly jack lug tab and under the ground handling ball 3 Zero scales or record tare weight items between scale and weighing point such as adapter jack stand sandbags etc at each scale 4 Level helicopter for weight and balance per Sections 8 10 and 8 11 Remove spirit level If removed carefully replac...

Страница 142: ...icopter and calculate new weight and CG per the previous steps c If Calculated CG is less than 101 50 and nose ballast is installed determine minimum nose ballast to remove 102 50 Calculated CG X Calculated weight 97 35 lb Round down to nearest 0 25 lb Remove nose ballast per Section 8 31 Reweigh helicopter and calculate new weight and CG per the previous steps d If Calculated CG is greater than 1...

Страница 143: ...ngitudinal CG arm inches Moment in lb Forward Net x 32 67 Left Net x 127 35 Right Net x 127 35 Unusable fuel add 6 70 x 110 40 739 68 Basic empty weight and longitudinal CG 9 Calculate basic empty weight and lateral CG Item Weight lb Lateral CG arm inches Moment in lb Forward Net x 4 13 Left Net x 16 73 Right Net x 16 73 Unusable fuel add 6 70 x 20 70 138 69 Basic empty weight and lateral CG ...

Страница 144: ...FIGURE 8 4 NOSE BALLAST View inside lower console assembly with upper console hinged aft Page 8 10 Chapter 8 Weight and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 145: ...1 1 panel 3 Remove or install ballast plates per calculations performed in Section 8 22 Select NAS6603 bolt length to meet torque requirements per Section 20 30 Install hardware torque bolts per Section 20 32 and torque stripe per Figure 5 1 4 Hinge upper console assembly forward and install screws securing upper and lower console assemblies Verify security 5 Reweigh and or calculate basic empty w...

Страница 146: ...FIGURE 8 5 EMPENNAGE BALLAST Page 8 12 Chapter 8 Weight and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 147: ...per 53 50 Topcoat hardware with colored paint as desired 4 Reweigh and or calculate basic empty weight and CG per 8 22 5 Revise Weight and Balance Record in R66 Pilot s Operating Handbook POH Section 6 to reflect ballast removal using the following data Item Weight Longitudinal Arm Longitudinal Moment Lateral Arm Lateral Moment Empennage Ballast 3 00 lb 325 44 in 976 32 in lb 4 45 in 13 35 in lb B...

Страница 148: ...l clamp against stabilizer 6 Remove tracing media Solvent clean bare metal on horizontal stabilizer and weight clamping surfaces 7 Reweigh and or calculate basic empty weight and CG per 8 22 8 Revise Weight and Balance Record in R66 Pilot s Operating Handbook POH Section 6 to reflect ballast installation using the following data Item Weight Longitudinal Arm Longitudinal Moment Lateral Arm Lateral ...

Страница 149: ... Handling Page 9 i CHAPTER 9 GROUND HANDLING Section Title Page 9 10 Ground Handling 9 1 9 11 Ground Handling Wheels 9 1 9 12 Moving Helicopter on Ground Handling Wheels 9 3 9 13 Ground Handling Carts 9 3 9 14 Ground Power Start 9 3 9 20 Trailering 9 4 ...

Страница 150: ...Intentionally Blank Page 9 ii Chapter 9 Ground Handling R66 Maintenance Manual 25 OCT 2010 ...

Страница 151: ...s raised WARNING Remove ground handling wheels for flight A Installation NOTE Verify proper inflation of ground handling wheel tires Maximum tire inflation pressure is 70 psi 1 Extend ground handling wheel retractable handle by depressing locking pins and sliding handle out until pins engage outer holes Verify security 2 Refer to Figure 9 1 Hold ground handling wheel assembly inboard of skid with ...

Страница 152: ... of cradle 3 Pull handle in rearward arc to raise helicopter NOTE R66 ground handling wheels are installed inboard of landing gear skid tubes C063 5 LH and C063 6 RH ground handling wheel assemblies are not interchangeable When wheels are installed and in locked position both handles point aft Page 9 2 Chapter 9 Ground Handling R66 Maintenance Manual 25 OCT 2010 ...

Страница 153: ...ar extensions NOTE Steer helicopter by gripping the tail rotor gearbox aft tailcone section or inboard part of horizontal stabilizer between tailcone and vertical stabilizers CAUTION Do not steer helicopter by gripping the tail rotor guard vertical stabilizers outboard part of horizontal stabilizer tail rotor tail rotor controls or tail skid 5 a If moving helicopter forward nose first Open engine ...

Страница 154: ...upport point s to prevent tailcone damage 3 Perform one of the following options a Remove main rotor blades per Section 62 10 Pack blades in shipping crate See R66 Illustrated Parts Catalog IPC Figure 99 11 b Install main rotor blade supports per Section 10 13 c Fabricate blade supports to unload droop stops Position supports inboard of blade extended tab Cushion support points to prevent blade da...

Страница 155: ... and Storage Page 10 i CHAPTER 10 PARKING AND STORAGE Section Title Page 10 10 Parking 10 1 10 11 Parking in High Wind or Turbulent Air 10 1 10 12 Main Rotor Blade Tie Downs 10 3 10 13 Main Rotor Blade Supports 10 5 10 20 Storage Greater than 30 days 10 6 ...

Страница 156: ...Intentionally Blank Page 10 ii Chapter 10 Parking and Storage R66 Maintenance Manual 25 OCT 2010 ...

Страница 157: ...bulent Air Helicopter should be hangared or moved to a safe area during storm conditions or when storm conditions are forecasted When parking helicopter in high winds or when aircraft is exposed to prop rotor wash or jet blast 1 Position helicopter with nose pointed in the direction of prevailing wind or turbulent air 2 Park helicopter per Section 10 10 Position rotor blades slightly offset from f...

Страница 158: ...FIGURE 10 1 MAIN ROTOR BLADE TIE DOWNS Page 10 2 Chapter 10 Parking and Storage R66 Maintenance Manual SEP 2012 ...

Страница 159: ... Maximum tie down tension is 5 lb 1 Park helicopter and position blades per Section 10 10 or 10 11 2 Refer to Figure 10 1 Slide MT290 3 tie down jacket over forward lowered main rotor blade tip with white lettering facing down Thread strap through nose bracket and secure tie down hook and loop tape Push up on secured blade to remove slack in tie down strap 3 As required install MT290 3 tie down on...

Страница 160: ...FIGURE 10 2 MAIN ROTOR BLADE SUPPORTS Page 10 4 Chapter 10 Parking and Storage R66 Maintenance Manual 25 OCT 2010 ...

Страница 161: ...ation landing gear eyebolts and roof mounted cleat is required for mounting blade supports 1 Refer to Figure 10 2 Position main rotor blades approximately fore and aft 2 Install MT564 1 cradle assembly inboard of forward blade extended tab with MT568 3 strap assembly attached Thread opposite end of strap assembly through roof mounted cleat and secure strap hook and loop tape 3 Secure one MT347 8 s...

Страница 162: ...lades per Section 64 36 4 Open applicable circuit breakers 5 RemovebatteryperChapter96 Inspect servicebatteryaccordingtobatterymanufacturer s instructions 6 Service engine oil hydraulic fluid and main tail rotor gearboxes per Chapter 12 7 Fuel helicopter per Section 12 41 NOTE Fuel lubricates bladder inner liner and keeps it from drying out or cracking Refuel helicopter after run ups during storag...

Страница 163: ...CHAPTER 11 PLACARDS AND MARKINGS Section Title Page 11 10 Placards and Markings 11 1 APR 2017 Chapter 11 Placards and Markings Page 11 i ...

Страница 164: ...Intentionally Blank Page 11 ii Chapter 11 Placards and Markings APR 2017 ...

Страница 165: ...dge Avoid damaging or removing paint or primer from surfaces Remove decal entirely B Installation Verify surfaces are clean and dry before attaching decals Use a clean cloth wet with acetone or mild soapy water to clean surfaces but use caution when using acetone near silk screened lettering Acetone can smudge or remove silk screened letters Attach decal and rub decal surface with finger applying ...

Страница 166: ...Intentionally Blank Page 11 2 Chapter 11 Placards and Markings APR 2017 ...

Страница 167: ...n and Flush 12 11 12 34 Bleeding 12 12 12 40 Fuel System 12 13 12 41 Fueling 12 13 12 42 Defueling 12 13A 12 50 Main Rotor Blades 12 15 12 51 Pitch Bearing Housing 12 15 12 60 Engine Oil Servicing 12 16 12 70 Engine Compressor Rinse and Wash 12 17 12 71 Drainage Spotface Inspection During Cleaning or Rinsing of RR300 Engine 12 17A 12 80 Air Conditioning System 12 18 12 81 Refrigerant Recovery and ...

Страница 168: ...Intentionally Blank Page 12 ii Chapter 12 Servicing JUL 2020 ...

Страница 169: ...tion drain hose overboard into a suitable drain container Jam wedge between support panel stiffener and drain assembly fitting to open valve B Adding Fluid 1 Install chip detector per Section 12 13 if removed 2 Refer to Figure 12 1 Remove gearbox filler plug Fill gearbox with A257 22 lubricant to center of sight glass 3 Rotate rotor system by hand for several revolutions and pull down on tail roto...

Страница 170: ...FIGURE 12 1 MAIN ROTOR GEARBOX SERVICING Page 12 2 Chapter 12 Servicing R66 Maintenance Manual SEP 2012 ...

Страница 171: ...ight Gage A Removal 1 Refer to Figure 12 1 Disconnect chip detector wiring as required Remove chip detector from housing NOTE Remove chip detector housing and inspect for obvious damage if housing leaks 2 Drain main rotor gearbox oil per 12 11 if removing chip detector housing or sight gage Remove housing and or gage as required B Cleaning Chip Detector and Housing 1 Clean chip detector using a to...

Страница 172: ...Page 12 4 Chapter 12 Servicing APR 2019 FIGURE 12 2 DRAINING MAIN ROTOR GEARBOX OIL ...

Страница 173: ...ight gage and special torque per Section 20 33 2 Verify cleanliness of chip detector and housing As required remove and clean chip detector and housing per Parts A and B Install housing and special torque per Section 20 33 Install chip detector 3 Turn BATTERY switch ON Verify MR CHIP warning segment illuminates when test button is depressed Turn BATTERY switch OFF SEP 2012 R66 Maintenance Manual C...

Страница 174: ...FIGURE 12 3 TAIL ROTOR GEARBOX Page 12 6 Chapter 12 Servicing R66 Maintenance Manual SEP 2012 ...

Страница 175: ...level A Draining Fluid 1 Refer to Figure 12 3 Cut and discard ty raps as required and disconnect chip detector wiring from airframe harness at connectors 2 Place a suitable drain container under gearbox to catch oil then remove chip detector B Adding Fluid 1 Install chip detector per Section 12 22 2 Refer to Figure 12 3 Remove filler vent plug and fill gearbox with A257 22 lubricant to center of s...

Страница 176: ...as required Cinch ty raps until snug without over tightening and trim tips flush with heads 4 Turn BATTERY switch ON Verify TR CHIP warning segment illuminates when test button is depressed Turn BATTERY switch OFF 5 Service tail rotor gearbox per Section 12 21 12 23 Drain and Flush 1 Drain tail rotor gearbox oil per Section 12 21 2 Install chip detector and special torque per Section 20 33 3 Remov...

Страница 177: ...move D516 1 cap and filter and visually inspect element for contaminants If element is clear proceed to step 3 If metal contamination is found use a magnet to determine if metal is ferrous If metal is ferrous perform the following a Install new filter per steps 3 thru 5 b After one flight hour remove filter and inspect for ferrous metal If ferrous metal is found upon second inspection replace hydr...

Страница 178: ...FIGURE 12 4 HYDRAULIC SYSTEM Page 12 10 Chapter 12 Servicing R66 Maintenance Manual SEP 2012 ...

Страница 179: ...eaks 7 Simultaneously fully raise collective and move cyclic fully forward then simultaneously fully lower collective and move cyclic fully aft Monitor reservoir fluid level and fill as required Repeat procedure until return line fluid is clean 8 Simultaneously fully raise collective and move cyclic fully aft then simultaneously fully lower collective and move cyclic fully forward Monitor reservoi...

Страница 180: ...pect hydraulic system for leaks 4 Simultaneously fully raise collective and move cyclic fully forward then simultaneously fully lower collective and move cyclic fully aft Repeat procedure ten times 5 Simultaneously fully raise collective and move cyclic fully aft then simultaneously fully lower collective and move cyclic fully forward Repeat procedure ten times 6 Turn off test pump and verify no l...

Страница 181: ... helicopter and ground fuel vehicle Open baggage compartment door and connect fuel vehicle ground cable to aux fuel tank at location identified by decal 3 Verify proper grade of aviation fuel See R66 Pilot s Operating Handbook POH Section 2 for approved fuel grades and instructions for use of anti ice additive 4 Remove fuel cap and fuel helicopter as required NOTE If auxiliary fuel system is insta...

Страница 182: ... inlet fitting Connect B283 12 hose special torque hose nut per 20 33 and torque stripe per Figure 5 1 8 Defuel engine as required per RR300 Series Operation and Maintenance Manual OMM B Auxiliary Fuel System 1 Turn battery switch off Open baggage compartment door 2 Release D205 35 large tank drain or D205 37 small tank drain hose assembly from tab Position hose overboard into a suitable grounded ...

Страница 183: ...Intentionally Blank APR 2017 Chapter 12 Servicing Page 12 13B ...

Страница 184: ...FIGURE 12 5 MAIN ROTOR BLADE PITCH BEARING HOUSING Page 12 14 Chapter 12 Servicing APR 2017 ...

Страница 185: ...er 4 Place supply container with sufficient A257 4 fluid approximately 3 feet above spindle Route fill hose assembly into drain container and open brass valve Open supply container plastic valve and purge air from hose Close valves 5 Connect brass valve to bottom bleed fitting by tightening brass compression sleeve 6 Open valves and fill spindle housing until no air bubbles are visible in drain ho...

Страница 186: ...ed containers using clean tools NOTE When servicing airframe oil tank full oil quantity is six quarts minimum quantity for takeoff is four quarts Six quart indication is top of knurled section of dipstick Four quart indication is bottom of knurled section of dipstick or center of oil tank sight gage 1 Install B289 2 bolt in bend of F723 1 line assembly and special torque per 20 33 2 Install AS5169...

Страница 187: ...cleaning system hose to delivery tube 5 Refer to RR300 Series OMM for compressor rinse and wash procedures To motor engine without ignition system a Release rotor brake b Turn battery switch on c Verify fuel cutoff pulled OFF Verify igniter key switched OFF d Verify area is clear e Close throttle f Push and release start button as required to maintain N1 speed for required interval 6 Disconnect cl...

Страница 188: ... the Engine after Operation in a Corrosive Environment and NTO Notice To Operators No RR300 020 RR300 Engine Wash Procedures Refer to Figure 12 6 During cleaning or rinsing of engine RHC recommends verifying the drainage spotface on the magnesium gearbox cover is unobstructed Follow OMM guidance do NOT use metallic tools or wire to remove debris VIEW LOOKING UP FORWARD FIGURE 12 6 DRAINAGE SPOTFAC...

Страница 189: ...Intentionally Blank JUL 2020 Chapter 12 Servicing Page 12 17B ...

Страница 190: ...NOTE If a leak or other service problem is encountered after system is charged with refrigerant refrigerant must be recovered before work on system can proceed 1 Remove tailcone cowling per 53 23 2 Automotive style high and low side system service ports are located on G794 hose assemblies where they mount to the compressor assembly Connect service equipment to system quick disconnect ports and rec...

Страница 191: ...nce from the vacuum pump for 20 minutes minimum If a vacuumed system creeps up in pressure a leak may be present The technician should be thoroughly familiar with vacuum equipment to ensure leak is in aircraft system and not in vacuum equipment or connections Leaks in a charged system may be detected using a mild soap and water solution applied to lines and fittings in suspected leak areas bubbles...

Страница 192: ...arge system to 200 psi maximum Use commercially available electronic helium detector or soap and water solution to locate leaks Leaks are most likely to occur at fittings and crimped transitions between hard line and flexible hose Concentrate initial leak detection efforts in these areas Page 12 20 Chapter 12 Servicing JUL 2020 FIGURE 12 7 C017 6 REV AD OR LATER SWASHPLATE ASSEMBLY ...

Страница 193: ...grease is just below top of C205 1 sleeve approx 20 ml grease Do not allow grease into screw holes 8 Position C217 1 seal atop grease followed by C219 3 spacer C200 3 retainer and NAS1352N08 8 screws with NAS620 8L washers Finger tighten all screws then snug any 4 screws that are 90 apart depressing seal and forcing grease into underlying bearing set Rotate upper swashplate several revolutions Wip...

Страница 194: ...15 While observing swashplate have someone fully manipulate cyclic and collective controls Verify swashplate movement corresponds with cyclic and collective movement and without interference 16 Position swashplate boot on upper swashplate and secure with MS3367 6 0 ty rap 17 With appropriately rated person at controls start helicopter run up to 100 NR then shutdown 18 Remove ty rap and raise swash...

Страница 195: ...r Dynamic Balance 18 17 18 22 Ground Checks 18 19 18 23 Balance Adjustment 18 19 18 30 Main Rotor Flight Control Rigging 18 21 18 40 Main Rotor Blade Angle Rigging 18 23 18 41 Collective Travel 18 24 18 42 Cyclic Travel 18 26 18 50 Tail Rotor Flight Control Rigging 18 28 18 51 Pedals 18 28 18 52 Forward Bellcrank 18 28 18 53 Intermediate Bellcrank 18 28 18 60 Tail Rotor Blade Rigging 18 29 18 70 F...

Страница 196: ...Intentionally Blank Page 18 ii Chapter 18 Track and Balance APR 2019 ...

Страница 197: ... once a year or if equipment is dropped misused or calibration is suspect NOTE The Chadwick Helmuth Vibrex system the TEC ACES system the Dynamic Solutions Systems MicroVib system or equivalent equipment is required to perform dynamic rotor balancing and in flight track checks 25 OCT 2010 R66 Maintenance Manual Chapter 18 Track and Balance Page 18 1 ...

Страница 198: ...FIGURE 18 1 MAIN ROTOR BALANCING EQUIPMENT INSTALLATION Page 18 2 Chapter 18 Track and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 199: ...ate bracket Set swashplate mounted interrupter to pickup gap to 0 030 inch 0 010 inch and tighten pickup nuts against bracket Safety nuts using 0 020 inch diameter lockwire Recheck gap 5 Pull collective stick full up push cyclic stick full left and apply frictions Connect proper cable to magnetic pickup Route cable down seam and to base of mast fairing across the cabin roof left side and through t...

Страница 200: ...R 50 60 70 80 90 100 110 120 130 140 I I I I I I I I I I I I I I I I I I I I I I FIGURE 18 2 MAIN ROTOR TRACK AND BALANCE CHART TIP WEIGHTS 1 AN960 10 Washer 2 AN960 10L Washers 1 C298 2 Weight 5 AN960 10 Washers 1 C298 3 Weight 11 AN960 10 Washers 1 C298 4 Weight 4 C298 3 Weights CHORD ARM WEIGHTS 1 A255 1 Weight 8 AN970 4 Washers 1 A255 2 Weight 3 A255 1 Weights TEETER HINGE SHIMS C117 8 0 012 i...

Страница 201: ...er and record data Maximum vibration allowance is 0 2 ips inches per second Adjust balance per 18 14 as required record data and recheck balance in a hover Repeat step as required until main rotor balance is within limits 4 Fly helicopter at 50 60 70 80 90 100 110 120 130 and 140 knots Check main rotor blade track at each airspeed and record data Maximum blade spread between airspeeds is 3 8 inch ...

Страница 202: ...Page 18 6 Chapter 18 Track and Balance APR 2017 FIGURE 18 3A C258 5 MAIN ROTOR PITCH LINK ...

Страница 203: ...backup wrench on barrel assembly special torque 21FKF 813 nut per 20 33 and standard torque upper rod end jam nut and palnut per 20 32 v Repeat steps on opposite pitch link as required torque stripe per Figure 5 1 b C258 1 Pitch Link Adjust fitting only per the following i Refer to Figure 18 3B Cut and discard pitch link assembly safety wire Using backup wrench on link assembly loosen 21FKF 813 nu...

Страница 204: ...FIGURE 18 3B C258 1 MAIN ROTOR PITCH LINK Page 18 7A Chapter 18 Track and Balance APR 2019 ...

Страница 205: ... as possible without binding Using backup wrench on barrel assembly or fitting standard torque upper rod end jam nut and palnut per 20 32 e Repeat steps on opposite pitch link as required torque stripe per Figure 5 1 3 For coarse length adjustment a C258 5 Pitch Link Adjust lower rod end per the following i Refer to Figure 18 3A Using backup wrench on barrel assembly loosen 21FKF 813 nut at lower ...

Страница 206: ...hanges blade angle by approximately 0 44 iii Refer to Figure 5 1 Verify rod end threaded shank blocks passage of 0 020 inch diameter lockwire through link assembly witness hole Install hardware securing rod end to swashplate and standard torque fasteners per 20 32 iv Position rod ends to allow as much pitch link rotation as possible without binding Using backup wrench on link assembly special torq...

Страница 207: ...Intentionally Blank APR 2017 Chapter 18 Track and Balance Page 18 7D ...

Страница 208: ...FIGURE 18 4 MAIN ROTOR BLADE TRIM TAB Page 18 8 Chapter 18 Track and Balance APR 2017 ...

Страница 209: ...ibration 1 Using felt tip marker ink mark main rotor blade trim tab per Figure 18 4 Mark line with a measuring point in the center of the tab approximate 2 Position MT352 1 gage chordwise across blade upper surface and tab trailing edge Zero dial indicator on measuring point 3 Position MT526 8 bending tool on tab per Figure 18 4 Slide tool completely over tab until tool stops contact blade trailin...

Страница 210: ...Page 18 10 Chapter 18 Track and Balance APR 2017 FIGURE 18 4A MAIN ROTOR BLADE TIP ...

Страница 211: ...8 2 Weight 5 AN960 10 or NAS1149F0363P Washers 1 C298 3 Weight 11 AN960 10 or NAS1149F0363P Washers 1 C298 4 Weight 4 C298 3 Weights B Teeter Hinge Bolt Shims Chordwise Balance Adjustment Coarse Adjustment 1 Remove and discard teeter hinge nut cotter pin Remove nut thrust washer and any shims 2 Have two people cone the main rotor blades Push out teeter hinge bolt and any shims with another bolt 3 ...

Страница 212: ...Intentionally Blank Page 18 10B Chapter 18 Track and Balance APR 2017 ...

Страница 213: ...placement 2 Excessive Ship Vibration MR out of track and balance Track and balance per Section 18 10 MR teeter or coning hinge friction Adjust hinge friction per Section 62 32 MR teeter or coning hinge binding Replace bearings per Section 62 21 Brinelled spindle bearing rough movement Send blade s to RHC for spindle bearing replacement MR teeter hinge bearings worn Replace bearings per Section 62 ...

Страница 214: ...meter reading 2 Set the altimeter to 29 92 Hg 1013 2 millibars prior to performing the autorotation Autorotate with the collective control firmly held against the down stop with an airspeed of 50 KIAS WARNING Do not allow the rotor to overspeed when performing autorotation checks Progressively lengthen both main rotor pitch link rod ends until full down collective can be obtained without over spee...

Страница 215: ...tside air temperature and draw a vertical line up to pressure altitude b Draw a horizontal line from pressure altitude to rotorcraft gross weight at time of autorotation c Draw a vertical line down from autorotation gross weight to required auto RPM 5 Adjust pitch links based on average RPM correction required Lengthen both pitch links to decrease RPM if test RPM is greater than chart RPM shorten ...

Страница 216: ...ull turn of rod ends approximately 3 RPM change One full turn of rod end 1 turns of barrel Example OAT 20 C Hp 2000 ft GW 1800 lb RPM 103 FIGURE 18 5 AUTOROTATION RPM ADJUSTMENT Page 18 14 Chapter 18 Track and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 217: ...Intentionally Blank 25 OCT 2010 R66 Maintenance Manual Chapter 18 Track and Balance Page 18 15 ...

Страница 218: ...FIGURE 18 6 TAIL ROTOR BALANCING EQUIPMENT INSTALLATION Page 18 16 Chapter 18 Track and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 219: ...arings per 5 33 and 5 34 2 Track tail rotor blades per 64 10 3 Refer to Figure 18 6 If using photocell to obtain clock angle install a target tape spanwise on inboard side of one arm of tail rotor hub if using Strobex install a target tape spanwise on outboard side of hub 4 Using appropriate hardware attach bracket s to vibration transducer and photocell if used Secure bracket to tail rotor gearbo...

Страница 220: ... FASTENER SPANWISE WEIGHTS 1 C141 23 Washer 3 5 NAS1149F0663P Washers 1 C141 24 Washer 7 NAS1149F0663P Washers 2 NAS1149F0632P 1 NAS1149F0663P Washer PITCH HORN TO PITCH LINK FASTENER CHORDWISE WEIGHTS 1 NAS1149F0463P Washer 2 NAS1149F0432P Washers 1 A214 3 Washer 3 5 NAS1149F0432P Washers 1 A141 14 Washer 5 NAS1149F0432P Washers Page 18 18 Chapter 18 Track and Balance APR 2019 ...

Страница 221: ... Install 0 032 inch diameter lockwire securing cap retaining hardware and safety in pairs WARNING A rotor which is smooth after balancing but goes out of balance within a few flights is suspect and must be examined by RHC before further flight 18 23 Balance Adjustment Refer to R66 Illustrated Parts Catalog IPC Figure 64 1 Refer to Section 64 11 for tail rotor assembly static balance procedure A Pi...

Страница 222: ...FIGURE 18 8 SWASHPLATE AND COLLECTIVE CONTROL RIGGING FIGURE 18 9 A205 5 SWASHPLATE FORK RIGGING Page 18 20 Chapter 18 Track and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 223: ...e assemblies and fork assembly located between keel panels to the noted rod end center to center dimensions PART NUMBER DIMENSION C121 1 51 15 0 03 inches F121 1 32 36 0 03 inches G205 1 5 40 0 03 inches 3 Adjust length of F121 1 tube so that with collective full up there is a 0 50 inch gap between G205 1 yoke and F315 1 support 4 Refer to Figure 18 8 Position MT146 4 swashplate rigging blocks bet...

Страница 224: ...FIGURE 18 10 MAIN ROTOR BLADE RIGGING Page 18 22 Chapter 18 Track and Balance R66 Maintenance Manual 25 OCT 2010 ...

Страница 225: ...d mark the opposite blade s tip height Teeter main rotor hub as required until blade tips are level within 1 inch 2 Refer to Figure 18 10 Using felt tip marker mark upper surface of both main rotor blades 49 5 inches inboard of seam between blade tip and tip cover Lay 1 inch wide length of masking tape chordwise on each blade centered over marking Mark each rotor blade with a different color desig...

Страница 226: ...lade angles per Section 18 40 Part B to determine the values below Rotate blades 180 and align per step 3 as required BLUE BLADE RED BLADE Pitch horn forward Pitch horn forward Pitch horn aft Pitch horn aft 2 2 5 Blade angles must average between 1 0 and 2 0 for collective down position Final blade angle for collective down position is determined during autorotation rpm adjustment Adjust main roto...

Страница 227: ...n blade angles must average between 12 5 and 13 5 more than collective down position average Adjust main rotor blade pitch links per Section 18 13 as required one full barrel turn 0 72 until blade angles when blades are positioned pitch horn forward are within 0 2 Adjust pitch links until blade angles when blades are positioned pitch horn aft are also within 0 2 NOTE Remeasure collective down blad...

Страница 228: ...left position Adjust swashplate forward left or right push pull tube as required one full turn 0 6 B Cyclic Right 1 Position collective stick full down Position cyclic stick in the longitudinal neutral mid travel position and against right stop Apply control frictions sandbag cyclic stick as required 2 Rotate blades so pitch links are aligned with helicopter lateral axis 3 Measure and record blade...

Страница 229: ...l tubes exactly the same amount one full turn 0 6 D Cyclic Aft 1 Position collective stick full down Position cyclic stick in the lateral neutral 5 inches to left of right stop position and against aft stop Apply control frictions sandbag cyclic stick as required 2 Rotate blades so pitch links are aligned with helicopter longitudinal axis 3 Measure and record blade angles per 18 40 Part B to deter...

Страница 230: ...the lower forward NAS6604 9 bolt in C317 5 or C317 9 bellcrank and horizontal pedal torque tube 18 52 Forward Bellcrank Remove the rigging pin and place the left pedal against its stop Adjust the F121 11 push pull tube to obtain 1 08 1 18 inches between the end of the rod end and the bulkhead 18 53 Intermediate Bellcrank With left pedal at stop adjust the C121 17 push pull tube length as required ...

Страница 231: ... record data below Rotate the tail rotor 180 and record the opposite blade angle Pedals Full Left Blue Blade Red Blade 2 18 5 19 0 required 7 Difference between blue and red blade angles may not exceed 0 4 If blade angles exceed this limit remove tail rotor assembly per 64 10 rotate assembly one half revolution and install assembly per 64 10 Repeat previous steps If blade angles still exceed relat...

Страница 232: ...r If total is less than 34 0 pedal total travel is too small If total is greater than 35 5 pedal total travel is too great b If pedal total travel is too small increase C343 11 push pull tube length and or decrease C343 13 push pull tube length c If pedal total travel is too great decrease C343 11 push pull tube length and or increase C343 13 push pull tube length d Recheck left and right pedal bl...

Страница 233: ...Intentionally Blank MAY 2015 Chapter 18 Track and Balance Page 18 31 ...

Страница 234: ...Page 18 32 Chapter 18 Track and Balance MAY 2015 FIGURE 18 12 FAN SHAFT AND ENGINE SHAFT BALANCING ...

Страница 235: ... and F642 shaft weldment Inspect condition of flex plates weldment flanges and adjacent yokes Verify proper fastener installation and unbroken torque stripe 2 Refer to Figure 18 12 a Fan Shaft Using a 8 screw attach vibration transducer and photocell cables pointed up to mounting bracket s Secure bracket s to top of tailcone at the forward nutplate aiming photocell toward center of shaft b Engine ...

Страница 236: ...Page 18 34 Chapter 18 Track and Balance APR 2019 FIGURE 18 13 FAN SHAFT BALANCING CHART ...

Страница 237: ...432P NAS1149F0463P A214 3 or A141 14 washers as required and install under one nut of intermediate flex plate tail rotor driveline fastener b Engine Shaft Refer to Figure 18 14 Adjust balance by selecting one or more NAS1149D0463J NAS1149F0432P NAS1149F0463P A214 3 or A141 14 washers as required and install under one nut of aft flex plate engine driveline fastener After first adjustment if engine ...

Страница 238: ...FIGURE 18 14 ENGINE SHAFT BALANCING CHART Page 18 36 Chapter 18 Track and Balance APR 2019 ...

Страница 239: ...cent Penetrant Inspection 20 13 20 50 Corrosion Control 20 13 20 60 Priming and Painting 20 13 20 70 Approved Materials 20 16 20 71 Paint Strippers 20 16 20 72 Solvents and Cleaners 20 16 20 73 Fillers and Putty 20 17 20 74 Torque Seal 20 17 20 75 Primers 20 18 20 76 Powder Coat 20 18A 20 77 Paints 20 18B 20 78 Lubricants 20 21 20 79 Adhesives and Sealants 20 22 20 80 Storage Limits 20 24 20 90 Mi...

Страница 240: ...Intentionally Blank Page 20 ii Chapter 20 Standard Practices JUL 2020 ...

Страница 241: ...les pitot tube or static ports CAUTION Wash helicopter exterior surfaces with mild soap and water Harsh abrasives alkaline soaps or detergents can scratch painted or plastic surfaces or cause corrosion of metal Protect areas where cleaning solution could cause damage 1 Rinse away loose dirt and debris from exterior surface with clean water 2 Apply mild soap and clean warm water solution to exterio...

Страница 242: ...carbonate impact resistant windshields is not recommended as it may thin the protective hardcoat finish C Cleaning Seat Assemblies and Back Rests 1 Vacuum and brush then wipe with damp cloth Dry immediately 2 Soiled upholstery except leather may be cleaned with a good upholstery cleaner suitable for the material Follow manufacturer s instructions Avoid soaking or harsh rubbing 3 Leather should be ...

Страница 243: ...ge engine gearbox or hydraulic oil and clean respective sight gage when oil becomes so dirty its level cannot be determined Change hydraulic oil if notedly odorous When installing a new or overhauled main rotor gearbox replace filter at first 100 hour inspection after installation Thereafter replace filter at scheduled intervals per 5 20 When installing a new or overhauled tail rotor gearbox drain...

Страница 244: ...Intentionally Blank Page 20 2B Chapter 20 Standard Practices JUL 2020 ...

Страница 245: ...NAS1305 bolt used with a NAS1068 nutplate is determined as follows NAS1305 bolt 5 indicates 5 16 inch size dry torque per Section 20 32 240 in lb Add 10 because torque must be applied at bolt head 24 in lb Torque wrench setting 264 in lb C Secondary Locking Mechanism A secondary locking mechanism is required on all critical fasteners B330 stamped nuts palnuts serve as secondary locking mechanisms ...

Страница 246: ...olve for Y T x L 135 x 10 1350 117 39 L A 10 1 5 11 5 Set torque wrench to 117 in lb to torque fastener to 135 in lb Given Symbols Y Unknown Y Torque wrench setting T 135 in lb T Torque applied to fastener L 10 in L Length of torque wrench A 1 5 in A Length of adapter When using an adapter that shortens the torque wrench effective length calculate torque wrench setting using the formula below EXAM...

Страница 247: ...hread exposure beyond primary nut may allow nut to seat against unthreaded shank resulting in insufficient joint clamping 6 Refer to Part A Torque wrenches must be calibrated annually when dropped or when a calibration error is suspected 20 31 Torque Stripe WARNING Refer to Safety Data Sheet SDS and observe precautions when working in proximity to hazardous materials Refer to Figure 5 1 Apply lacq...

Страница 248: ...ews 10 32 NAS6603 50 in lb 1 4 28 NAS6604 120 in lb 5 16 24 NAS6605 240 in lb 3 8 24 NAS6606 350 in lb 7 16 20 NAS6607 665 in lb 1 2 20 NAS6608 995 in lb AN3 Bolts AN4 Bolts AN6 Bolts AN8 Bolts AN502 AN503 Screws AN509 Screws AN525 Screws MS24694 Screws MS27039 Screws 10 32 AN3 37 in lb 1 4 28 AN4 90 in lb 3 8 24 AN6 280 in lb 1 2 20 AN8 795 in lb STAMPED NUTS PALNUTS 10 32 B330 7 MS27151 7 6 15 i...

Страница 249: ...1 D799 9 switch assembly 90 1 G783 condenser dessicant cap 100 1 G784 1 evaporator assembly inlet B nut to TXV 210 1 G794 1 hose assembly B nuts 210 1 G794 2 hose assembly B nuts 210 1 G794 3 hose assembly B nuts 150 1 G810 1 line assembly B nuts 210 1 G811 1 line assembly B nuts 150 2 AN924 8D nuts 360 8 MS27039C1 07 screws at condenser fans 30 2 91292A135 screws 70 CABIN 1 D210 5 nut ground hand...

Страница 250: ...5 nut securing A780 cable to B415 2 relay 80 1 NAS6605 3 bolt securing B237 8 battery ground cable to G131 5 terminal assembly 70 EMPENNAGE 8 NAS6604 6 bolts securing vertical stabilizers to upper horizontal stabilizer 185 1 NAS1352 3 14P screw securing guard assembly blocks to lower vertical stabilizer 40 ENGINE CONTROLS 1 Fuel control unit FCU lever nut 40 50 1 Power turbine governor PTG lever n...

Страница 251: ...y B nuts 100 1 G391 4 line assembly B nuts 100 1 G391 5 line assembly B nuts 230 260 2 G392 3 diffuser assembly B nuts 100 1 D210 3 nut securing control wire 25 30 HYDRAULIC HOSES FITTINGS 2 AN815 3D union 95 105 2 AN815 4D union 135 150 1 AN820 4 cap on reservoir AN804D4 T fitting 60 1 AN820 6 cap on reservoir AN834 6D T fitting 120 2 D452 3 nuts on aft and left hand servos 60 3 D452 4 nuts on af...

Страница 252: ... B nuts 245 2 D674 11 hose assembly B nuts 245 1 D674 12 hose assembly B nuts 245 1 D674 13 hose assembly B nuts 245 2 D770 1 valve assembly 40 2 D770 2 valve assembly 40 2 D770 3 valve assembly 40 2 D770 4 valve assembly 40 2 D770 5 valve assembly 40 2 D770 6 valve assembly 40 MAIN ROTOR BLADE 2 B289 2 bolts per blade self sealing 70 2 A722 4 screws per blade tip balance weight 40 wet 2 NAS1351N3...

Страница 253: ...7 2 line assembly horizontal turbine firewall shield assembly drain 50 65 1 F741 1 line assembly fuel differential pressure switch 80 1 G200 1 engine lifting lug optional 110 1 G426 1 fuel differential pressure switch assembly 100 2 nuts securing harness wire to MGT thermocouple studs engine supplied 20 2 nuts securing harness wires to starter generator small terminals starter generator supplied 2...

Страница 254: ...3 bolt teeter hinge 380 TAIL ROTOR FLIGHT CONTROLS 1 D210 4 nut outboard of F316 1 bellcrank assembly 90 TAIL ROTOR GEARBOX 1 A610 1 vent assembly 100 1 B563 4 sight gage 150 1 B566 2 chip detector 100 1 D210 5 nut pitch control housing 240 1 AN320 8 nut input yoke 35 45 FT LB 4 MS20074 04 06 bolts input cap 60 8 MS20074 04 06 bolts input housing and output cap 100 4 NAS1352 5 12P bolts undrilled ...

Страница 255: ... push pull tube to attachment point per respective instructions 6 Refer to Figure 5 2 Position rod ends to allow as much push pull tube rotation as possible without binding Standard torque jam nuts palnuts per 20 32 torque stripe per Figure 5 1 20 35 D210 series Nuts on Critical Fasteners When performing maintenance that involves disassembly of a critical fastener joints with a secondary lock reas...

Страница 256: ...8 4W AS5175W04 AL 1 4 inch 105 AN818 5D AN818 5W AS5175W05 AL 5 16 inch 106 AN818 6D AN818 6W AS5175W06 AL 3 8 inch 108 AN818 8D AN818 8W AS5175W08 AL 1 2 inch 110 AN818 10D AN818 10W AS5175W10 AL 5 8 inch 202 AN818 2J AS5175J02 CRES 1 8 inch 203 AN818 3J AS5175J03 CRES 3 16 inch 204 AN818 4J AS5175J04 CRES 1 4 inch 205 AN818 5J AS5175J05 CRES 5 16 inch 206 AN818 6J AS5175J06 CRES 3 8 inch 208 AN8...

Страница 257: ...AS3220W04 AL 1 4 inch 305 MS20819 5D AS3220D05 AS3220W05 AL 5 16 inch 306 MS20819 6D AS3220D06 AS3220W06 AL 3 8 inch 308 MS20819 8D AS3220D08 AS3220W08 AL 1 2 inch 310 MS20819 10D AS3220D10 AS3220W10 AL 5 8 inch 402 MS20819 2J AS5176J02 CRES 1 8 inch 403 MS20819 3J AS5176J03 CRES 3 16 inch 404 MS20819 4J AS5176J04 CRES 1 4 inch 405 MS20819 5J AS5176J05 CRES 5 16 inch 406 MS20819 6J AS5176J06 CRES ...

Страница 258: ...06 AL 1 2 inch 510 AN816 10D AS5194D1008 AL 5 8 inch 532 AN816 2J AS5194J0202 CRES 1 8 inch 533 AN816 3J AS5194J0302 CRES 3 16 inch 534 AN816 4J AS5194J0402 CRES 1 4 inch 535 AN816 5J AS5194J0502 CRES 5 16 inch 536 AN816 6J AS5194J0604 CRES 3 8 inch 538 AN816 8J AS5194J0806 CRES 1 2 inch 540 AN816 10J AS5194J1008 CRES 5 8 inch 562 AN816 2 AS5194 0202 STL 1 8 inch 563 AN816 3 AS5194 0302 STL 3 16 i...

Страница 259: ...W1008 AL 5 8 inch 632 AN822 2J MS20822 2J AS5195J0202 CRES 1 8 inch 633 AN822 3J MS20822 3J AS5195J0302 CRES 3 16 inch 634 AN822 4J MS20822 4J AS5195J0402 CRES 1 4 inch 635 AN822 5J MS20822 5J AS5195J0502 CRES 5 16 inch 636 AN822 6J MS20822 6J AS5195J0604 CRES 3 8 inch 638 AN822 8J MS20822 8J AS5195J0806 CRES 1 2 inch 640 AN822 10J MS20822 10J AS5195J1008 CRES 5 8 inch 662 AN822 2 MS20822 2 AS5195...

Страница 260: ...W1008 AL 5 8 inch 732 AN823 2J MS20823 2J AS5196J0202 CRES 1 8 inch 733 AN823 3J MS20823 3J AS5196J0302 CRES 3 16 inch 734 AN823 4J MS20823 4J AS5196J0402 CRES 1 4 inch 735 AN823 5J MS20823 5J AS5196J0502 CRES 5 16 inch 736 AN823 6J MS20823 6J AS5196J0604 CRES 3 8 inch 738 AN823 8J MS20823 8J AS5196J0806 CRES 1 2 inch 740 AN823 10J MS20823 10J AS5196J1008 CRES 5 8 inch 762 AN823 2 MS20823 2 AS5196...

Страница 261: ...h 808 AN833 8D AS1038D0808 AS1038W0808 AL 1 2 inch 810 AN833 10D AS1038D1010 AS1038W1010 AL 5 8 inch 832 AN833 2J AS1038J0202 CRES 1 8 inch 833 AN833 3J AS1038J0303 CRES 3 16 inch 834 AN833 4J AS1038J0404 CRES 1 4 inch 835 AN833 5J AS1038J0505 CRES 5 16 inch 836 AN833 6J AS1038J0606 CRES 3 8 inch 838 AN833 8J AS1038J0808 CRES 1 2 inch 840 AN833 10J AS1038J1010 CRES 5 8 inch 862 AN833 2 AS1038 0202...

Страница 262: ...AN815 8D AS5174D0808 AS5174W0808 AL 1 2 inch 910 AN815 10D AS5174D1010 AS5174W1010 AL 5 8 inch 932 AN815 2J AS5174J0202 CRES 1 8 inch 933 AN815 3J AS5174J0303 CRES 3 16 inch 934 AN815 4J AS5174J0404 CRES 1 4 inch 935 AN815 5J AS5174J0505 CRES 5 16 inch 936 AN815 6J AS5174J0606 CRES 3 8 inch 938 AN815 8J AS5174J0808 CRES 1 2 inch 940 AN815 10J AS5174J1010 CRES 5 8 inch 962 AN815 2 AS5174 0202 STL 1...

Страница 263: ... 8D AN924 8W AS5178W08 AL 1 2 inch 1010 AN924 10D AN924 10W AS5178W10 AL 5 8 inch 1032 AN924 2J AS5178J02 CRES 1 8 inch 1033 AN924 3J AS5178J03 CRES 3 16 inch 1034 AN924 4J AS5178J04 CRES 1 4 inch 1035 AN924 5J AS5178J05 CRES 5 16 inch 1036 AN924 6J AS5178J06 CRES 3 8 inch 1038 AN924 8J AS5178J08 CRES 1 2 inch 1040 AN924 10J AS5178J10 CRES 5 8 inch 1062 AN924 2 AS5178 02 STL 1 8 inch 1063 AN924 3 ...

Страница 264: ...inch 1132 AN826 2J MS20826 2J AS5198J020202 CRES 1 8 inch 1133 AN826 3J MS20826 3J AS5198J030203 CRES 3 16 inch 1134 AN826 4J MS20826 4J AS5198J040204 CRES 1 4 inch 1135 AN826 5J MS20826 5J AS5198J050205 CRES 5 16 inch 1136 AN826 6J MS20826 6J AS5198J060406 CRES 3 8 inch 1138 AN826 8J MS20826 8J AS5198J080608 CRES 1 2 inch 1140 AN826 10J MS20826 10J AS5198J100810 CRES 5 8 inch 1162 AN826 2 MS20826...

Страница 265: ...L 3 8 inch 1208 AN814 8D AN814 8W AS5169D08 AS5169W08 AL 1 2 inch 1210 AN814 10D AN814 10W AS5169D10 AS5169W10 AL 5 8 inch 1232 AN814 2J AS5169J02 CRES 1 8 inch 1233 AN814 3J AS5169J03 CRES 3 16 inch 1234 AN814 4J AS5169J04 CRES 1 4 inch 1235 AN814 5J AS5169J05 CRES 5 16 inch 1236 AN814 6J AS5169J06 CRES 3 8 inch 1238 AN814 8J AS5169J08 CRES 1 2 inch 1240 AN814 10J AS5169J10 CRES 5 8 inch 1262 AN8...

Страница 266: ...h 1308 AN814 8DL AN814 8WL AS5169D08L AS5169W08L AL 1 2 inch 1310 AN814 10DL AN814 10WL AS5169D10L AS5169W10L AL 5 8 inch 1332 AN814 2JL AS5169J02L CRES 1 8 inch 1333 AN814 3JL AS5169J03L CRES 3 16 inch 1334 AN814 4JL AS5169J04L CRES 1 4 inch 1335 AN814 5JL AS5169J0SL CRES 5 16 inch 1336 AN814 6JL AS5169J06L CRES 3 8 inch 1338 AN814 8JL AS5169J0BL CRES 1 2 inch 1340 AN814 10JL AS5169J10L CRES 5 8 ...

Страница 267: ...Intentionally Blank JUL 2020 Chapter 20 Standard Practices Page 20 11N ...

Страница 268: ...ble parts shall be inspected with both circular and longitudinal magnetization A Inspection Criteria Parts except gears which are inspected by magnetic particle inspection shall be accepted or rejected according to the following criteria Acceptable indications y Indications smaller than 0 015 inch are not considered ratable y Indications caused by sharp changes in cross section or part geometry Re...

Страница 269: ...ollowing y y Cracks y y Seams y y Cold shuts or laps y y Surface inclusions y y In castings aligned discontinuous surface indications other than cracks cold shuts and inclusions are rejectable if more than 3 8 inch in length 20 50 Corrosion Control Reserved 20 60 Priming and Painting This specification outlines preparation and application requirements for primers and topcoat Primers provide corros...

Страница 270: ...eign material or damp wipe with an approved solvent d Air dry Do not touch parts with bare hands until primed 2 Preparing Steel Alkaline clean is the preferred method for cleaning stainless steel Alternately stainless steel may be cleaned using an approved solvent Steel parts should only be cleaned using an approved solvent using an alkaline cleaning process on steel may cause a corrosive reaction...

Страница 271: ... have been cleaned and primed In general most parts will be cleaned and primed as detail parts However in some cases such as the gearbox assembly this is not practical and primer and topcoat are applied on the assembled component Previously primed surfaces or primed surfaces that have completely cured require the following preparation before paint 1 Lightly sand using 220 grit or finer sandpaper 2...

Страница 272: ...x plates Plastic Media Blasting System Pauli Griffin Co Vacaville CA Metal parts except blades and unsupported sheet metal less than 0 040 inch thick 20 72 Solvents and Cleaners PRODUCT MANUFACTURER SUPPLIER APPLICATION QSOL 220 Safety Kleen Systems Inc Plano TX General use for cleaning prior to applying primer topcoat adhesive or sealant Benzene 1 Chloro 4 Trifluoromethyl PCBTF Any Final Klean 39...

Страница 273: ...or Swagelok Salon OH Leak detector May be used on acrylic plastic Mix 5 20 by volume titration not required Acetone and PCBTF may be mixed 50 50 20 73 Fillers and Putty PRODUCT MANUFACTURER SUPPLIER APPLICATION 05960 Glazing Putty 05860 Dry Guide Coat 31180 Finishing Glaze 3M St Paul MN Minor surface imperfections SBF1191 Gearhead Products Indianapolis IN FE 351 Cream Hardener Catalyst Systems Gna...

Страница 274: ...utes 30 minutes Dry time 2 hours at 70 F 1 hour at 130 F 3 hours at 70 F 30 minutes at 120 F 3 hours at 70 F 30 minutes at 120 F Recoat window 48 hours 48 hours 48 hours Shelf life per manufacturer s recommendation B Chromate Primers 44GN007 10P20 44 Manufacturer PPG AkzoNobel Base 44GN007 10P20 44 Activator 44GN007CAT EC 265 or EC 273 Reducer Distilled or deionized water TR 114 or TR 102 Base Act...

Страница 275: ...Smooth Matte Black Polyester Topcoat Powder Tiger Drylac USA Cucamonga CA 49 72460 Smooth Glossy Gray RAL 7043 Polyester Topcoat Powder Tiger Drylac USA Cucamonga CA 49 22460 Smooth Glossy Yellow RAL 1028 Polyester Topcoat Powder PFWF104S9 White Polyester Topcoat Powder Dupont Co Wilmington DE Shelf life is 12 months from date of manufacture at ambient temperature JUL 2020 Chapter 20 Standard Prac...

Страница 276: ...rframe Maintenance Record logbook FINISH CODE MATERIAL ADDITIVES MANUFACTURER RHC PART NO APPLICATION A1 Flat Black 18BK006 18BK006CAT Catalyst PPG Aerospace Irvine CA 18BK006 Blade black Abrasion Resistant 23T3 90 Black PC 216 Curing Solution AkzoNobel Waukegan IL 23T3 90 A2 FR2 55 Mat Top Coat Thinner water Mapaero Pamiers France 557Z7038B005 Interior and skid tube black Aerofine 8250 Topcoat Th...

Страница 277: ... D121 D101 2100 P 9T20 Floats K Printcolor White Ink 750 9005 Printcolor Black Ink 750 8005 Printcolor Maize Yellow Ink 750 1205 Printcolor Carnation Red 750 3005 Printcolor Glass Hardener 700 Gensolve Thinner GS 017L Slow Retarder 10 03432 Deco Orance CA 7509005 7508005 7501205 7503005 Silkscreen L Red Imron AF400 AF700 13100S Activator 13110S Activator Axalta Wilmington DE N0759EP Red O Light Gr...

Страница 278: ...FIGURE 20 4 PAINT CODES Page 20 20 Chapter 20 Standard Practices JUL 2020 ...

Страница 279: ...A257 8 Rubber lubricant P 80 International Products Corp Trenton NJ A257 9 Anti seize Silver Grade Loctite Corp Newington CT A257 12 Grease MobilGrease 28 MIL PRF 81322 Exxon Mobil Corp A257 15 Hydraulic fluid Per MIL PRF 5606 Any A257 17 Substitute A257 19 A257 18 O ring lubricant 55 Dow Corning Corp Midland MI A257 19 Valve lubricant and sealant compound 111 Dow Corning Corp Midland MI A257 20 P...

Страница 280: ...fits 1 part Red 271 Henkel Loctite Corp Rocky Hill CT B270 11 Adhesive sealant threadlocker anaerobic loose fits 1 part Red 277 Henkel Loctite Corp Rocky Hill CT B270 12 Sealant electrical potting 2 part Any color except red MIL PRF 8516 Type II Class 2 Category A or B Any B270 13 Sealant silicone rubber noncorrosive 1 part Translu cent 3145 Dow Corning Corp Midland MI B270 14 Substitute B270 8 B2...

Страница 281: ...p Rocky Hill CT B270 24 Activator Primer Anaerobic adhesive 1 part Translucent Green 7649 Henkel Loctite Corp Rocky Hill CT B270 25 Clear Coat automotive touch up brush in bottle 1 part Clear Clear Coat Touch up Bottle Automotivetouchup Harahan LA B270 26 Sealant Polysulfide window glazing 2 Part Black AC 251B 1 3M Co St Paul MN B270 27 Adhesive Epoxy High Strength Structural Flexible 2 part Trans...

Страница 282: ...greases have a 5 year shelf life when stored and kept sealed in their original container Use invoice date or FAA Form 8130 date as start date unless the manufacturer has marked container with manufacture date in which case use manufacture date as start date 5 Rubber o rings seals and gaskets have a 20 quarter five 5 year shelf life from the indicated cure date Flourocarbon Viton and silicon rubber...

Страница 283: ...rometer and thermocouple to the smallest aluminum part in the oven Never depend on the oven control to determine part temperature Cooling a part for thermal fitting at assembly is not recommended Water vapor from the air will condense on the part and frequently introduce water into the assembly causing severe internal corrosion over time 20 93 Replacement Component Identification Data Plates In or...

Страница 284: ...Page 20 26 Chapter 20 Standard Practices APR 2017 20 94 Crimp Inspection Refer to Figure 20 5 FIGURE 20 5 CRIMP INSPECTION ...

Страница 285: ...1 1 21 10 Ventilation 21 3 21 11 Nose Vent 21 3 21 20 Air Conditioning 21 5 21 21 Compressor Assembly 21 5 21 22 Condenser and Fan Assemblies 21 7 21 23 Evaporator Assembly 21 8 21 24 Troubleshooting 21 9 21 30 Cabin Heat 21 11 21 31 Valve Assembly and Control Rigging 21 11 21 32 Muffler Assembly 21 12 21 33 Diffuser and Tee Assemblies 21 12 ...

Страница 286: ...Intentionally Blank Page 21 ii Chapter 21 Environment Control R66 Maintenance Manual SEP 2012 ...

Страница 287: ...ecessary cooling air for the condenser during forward flight In a hover electric fans help to draw cooling air through the condenser The evaporator blower draws warm cabin air though the evaporator inlet grill and evaporator where the air is cooled Cool air is drawn through the blower and blown through ducts under the center seat up the cabin aft wall and to the overhead duct The system is control...

Страница 288: ...FIGURE 21 1 NOSE VENT Page 21 2 Chapter 21 Environment Control MAY 2015 ...

Страница 289: ... control housing but do not tighten jam nut Install AN742 3 clamp and new as required MS35489 4 grommet on control housing 2 Position control in lower console and install screws securing mount assembly to lower console Verify security 3 Rotate control knob until horizontal within 15 when locked tighten jam nut against mount assembly Verify security 4 Route control inner wire through C062 1 vent bo...

Страница 290: ...FIGURE 21 2 AIR CONDITIONING SCHEMATIC Page 21 4 Chapter 21 Environment Control R66 Maintenance Manual SEP 2012 ...

Страница 291: ...or fittings 4 Rotate compressor down and inboard as required to disengage B173 5 v belt from pulleys Route belt around drive shaft flange and remove belt 5 Route new B173 5 v belt around drive shaft flange and fit belt onto G779 1 pulley and compressor pulley 6 Rotate compressor up and outboard to tension belt then tighten hardware securing compressor to weldment Adjust belt until 4 5 5 5 lb of fo...

Страница 292: ...9 1 pulley and compressor pulley and install hardware securing compressor to G782 1 mount weldment Standard torque bolts per 20 32 3 Install hardware securing compressor to G781 1 arm weldment Rotate compressor up and outboard to tension belt then tighten hardware securing compressor to weldment Adjust belt until 4 5 5 5 lb of force applied mid span deflects belt 0 16 inch Standard torque bolts pe...

Страница 293: ...nser to G787 support assemblies Taking care not to damage line assemblies and condenser fittings carefully remove condenser Cap fittings B Installation 1 Remove caps Install hardware securing G783 1 condenser to G787 support assemblies Verify security 2 Connect G810 1 and G811 1 line assembly b nuts to condenser fittings Using backup wrench special torque b nuts per Section 20 33 and torque stripe...

Страница 294: ... cover to middle seat if installed Detach grommet from seat assembly and carefully remove evaporator and attached components forward through seat assembly vertical wall relief Cap fittings B Installation 1 Remove caps Position G784 1 evaporator assembly and associated components in F377 1 middle seat assembly Install screws securing evaporator and D799 7 freeze switch assembly to seat assembly Ins...

Страница 295: ...h each switch All switches should be closed with a properly charged system and aircraft at rest on ground Replace any defective switch Failed Compressor V Belt Inspect belt Replace belt per 21 21 as required Insufficient Condenser Airflow Inspect condenser installation Verify no blockage and all seals in place Remove blockage and or repair seals to ensure airflow through core Extreme Environmental...

Страница 296: ...FIGURE 21 3 CABIN HEAT Page 21 10 Chapter 21 Environment Control JUL 2020 ...

Страница 297: ...tall clamps spacers and hardware securing line assemblies to aft right keel panel Verify security Hinge seat back 3 Position valve assembly so F621 2 bracket is vertical within 5 special torque line assembly B nuts at valve assembly muffler assembly and union and torque stripe per Figure 5 1 4 Perform control rigging per Part C steps 3 thru 6 5 Install engine cowling per Section 53 21 C Control Ri...

Страница 298: ...rity 2 Remove caps and plugs and connect G341 2 and G341 4 line assembly B nuts to muffler assembly fittings Special torque B nuts at AN824 8D tee and muffler assembly and torque stripe per Figure 5 1 3 Remove temporary covers and slide B277 12 clamp and A785 39 hose onto muffler assembly and tighten clamp Verify security 4 Install belly cover panels and install hardware Verify security 21 33 Diff...

Страница 299: ...ard panel and remove panel 2 Refer to Figure 21 3 Hinge aft right and left seats forward Remove hardware securing G394 1 guards and G392 3 diffuser assemblies to aft seat assemblies and remove guards Hinge seats back 3 Disconnect diffuser assembly B nuts from AN824 8D tee and remove diffusers As required disconnect G391 4 line assembly B nut from tee and remove tee Cap fittings D Aft Diffuser Asse...

Страница 300: ...Intentionally Blank Page 21 14 Chapter 21 Environment Control R66 Maintenance Manual SEP 2012 ...

Страница 301: ...y 22 3 22 20 Roll Servo Assembly 22 4 22 30 Flight Control Computer 22 5 22 40 Control Panel 22 6 22 50 Cyclic Grip Assembly 22 7 22 60 Maintenance 22 8 22 61 Scheduled Maintenance and Inspections 22 8 22 62 Special Maintenance and Inspections 22 10 MAY 2015 Chapter 22 Autopilot Page 22 i ...

Страница 302: ...Intentionally Blank Page 22 ii Chapter 22 Autopilot MAY 2015 ...

Страница 303: ...e described in the Normal Procedures section of the R66 Pilot s Operating Handbook POH Autopilot Supplement The control panel has a row of buttons to control autopilot modes and annunciators to indicate mode status A dark annunciator indicates that a mode is off a white annunciator indicates that a mode is armed or on standby and a green annunciator indicates that a mode is active The annunciators...

Страница 304: ...Page 22 2 Chapter 22 Autopilot MAY 2015 FIGURE 22 1 AUTOPILOT SYSTEM ...

Страница 305: ...AUTOPILOT 5 amp circuit breaker at panel Position cyclic stick full aft and apply cyclic friction 2 Position D354 3 pitch servo assembly in control tunnel and install hardware securing servo s D353 4 brace to cyclic box Standard torque bolts per 20 32 and torque stripe per Figure 5 1 Install screws securing brace to keel panels Verify security 3 Route servo harness through access holes and connect...

Страница 306: ...l out AUTOPILOT 5 amp circuit breaker at panel Position cyclic stick full left and apply cyclic friction 2 Position D354 4 roll servo assembly under pilot s seat and install hardware securing servo s D352 14 block assembly to keel panel and D353 5 brace assembly Tighten screws Verify security 3 Connect servo harness to 01311 03 11 flight control computer s J3 ROLL receptacle Install ty raps securi...

Страница 307: ...assemblies and D354 servo assembly harnesses from 01311 03 11 flight control computer s J1 PITCH J2 J3 ROLL and J4 receptacles 4 Disconnect pitot and static tubes from computer Plug elbows and tubes 5 Support computer and remove screws securing computer to D358 1 support assemblies Carefully remove computer from under pilot s seat APR 2017 Chapter 22 Autopilot Page 22 5 FIGURE 22 2 FLIGHT CONTROL ...

Страница 308: ...arness security 5 Verify freedom of flight controls through full travel with and without friction applied 6 Push in AUTOPILOT circuit breaker 5 amp at panel Perform ground checks as appropriate per 22 61 7 Install G702 7 cover assembly under pilot s seat 22 40 Control Panel A Removal 1 Turn battery avionics switches off and pull out AUTOPILOT 5 amp circuit breaker at panel 2 Loosen radio keys secu...

Страница 309: ...moval and Installation Refer to 67 12 for cyclic grip assembly removal and installation procedures To access grip switches 1 Remove MS24693 S1 screws securing C214 27 plate to D379 1 grip Remove switch nuts and lockwashers to free switches from plate 2 Install switch lockwashers new and nuts and tighten switches to plate verify switch security Install screws securing plate to grip 3 Turn battery s...

Страница 310: ...window pull and release caging knob if instrument bank angle exceeds 6 degrees Verify no sound in headset and control panel SAS LED is white other LEDs are dark NO SOUND SAS LED IS WHITE OTHER LEDs DARK 3 Visually verify servo assembly arms do not move when moving cyclic 4 Engage SAS mode cyclic should feel energized Verify no sound in headset and control panel SAS LED is green other LEDs are dark...

Страница 311: ...in headset and SAS LED is green other LEDs are dark 10 Engage SAS HDG and ALT modes Verify no sound in headset and SAS HDG and ALT LEDs are green other LEDs are dark Press AP OFF button on cyclic grip Verify no sound in headset and SAS LED is green other LEDs are dark 11 Engage SAS HDG and ALT modes Verify no sound in headset and SAS HDG and ALT LEDs are green other LEDs are dark Press AP OFF butt...

Страница 312: ... to RHC SAS does not disengage when cyclic grip AP OFF button depressed Check wiring between AP OFF button and computer Verify integrity of AP OFF button Return computer to RHC SAS does not engage or disengage when control panel buttons pressed Engage and or disengage SAS using cyclic grip buttons If system responds properly failure is in control panel or associated wiring to computer Contact RHC ...

Страница 313: ...ncy pitch oscillation when ALT engaged helicopter diverges nose up or nose down when ALT engaged Return computer to RHC ILS glideslope tracking performance is poor Check for excessive friction in longitudinal cyclic Check GPS output to computer Cyclic force seems higher than normal with SAS disengaged Verify servo clutches are disengaged and clutch arms do not move when SAS is Off or in standby mo...

Страница 314: ...Intentionally Blank Page 22 12 Chapter 22 Autopilot MAY 2015 ...

Страница 315: ...s Operating Handbook POH Strap Replacement 25 12 25 52 License Holder Replacement 25 13 25 53 Map Pocket Replacement 25 13 25 60 Emergency Equipment 25 14 25 61 Emergency Locator Transmitter ELT 25 14 25 62 Fire Extinguisher 25 15 25 70 Cargo Hook Installation 25 16 25 71 Description 25 16 25 72 Configurations 25 17 25 73 Cargo Hook 25 18 25 74 Cyclic Grips Electric Cargo Hook Release Remote Equip...

Страница 316: ...Intentionally Blank Page 25 ii Chapter 25 Furnishings APR 2019 ...

Страница 317: ...artment It is accessed via a large door on the aircraft right side The cowl door annunciator illuminates to warn the pilot when the door is not latched A light illuminates the compartment when the battery switch is ON Tie down anchors are provided for securing items in the baggage compartment Observe placarded weight limits Placard locations and illustrations are given in Chapter 11 Additional com...

Страница 318: ...FIGURE 25 1 SEAT HARNESSES SEAT ASSEMBLIES AND BACK RESTS Page 25 2 Chapter 25 Furnishings R66 Maintenance Manual SEP 2012 ...

Страница 319: ...anchors Remove hardware securing fifth point belts to seat boxes 4 Remove hole plugs then remove inertia reel covers and hardware securing reels to F369 and F370 forward seat backs Remove five point harnesses C Aft Left and Right Seat Harness 1 Refer to Figure 25 1 Remove F931 1 seat assembly hinge left and right seat assemblies forward 2 Remove hardware securing each F628 6 buckle assembly to inb...

Страница 320: ...t assemblies forward 5 Position F424 1 bumper assembly on F423 4 tube assembly and install screws Verify security C Aft Left and Right Seat Harness 1 Refer to Figure 25 1 Install hardware securing inertia reels to cabin bulkhead Install reel covers 2 Install hardware securing shoulder strap guides to door frames Standard torque bolts per Section 20 32 Install guide covers 3 Install hardware securi...

Страница 321: ...eat assembly hinge to seat box and remove seat assembly B Left and Right Seat Assembly Installation 1 If heated seats are installed turn battery switch off and pull out SEAT HEATERS circuit breaker 20 amp on circuit breaker panel 2 Refer to Figure 25 1 Position seat assembly on seat box and install hardware securing hinge to box Verify security 3 If heated seats are installed connect F940 3 forwar...

Страница 322: ...orward seats or F940 4 aft seats wire harness to F939 2 pad assembly wiring at connector Verify security 2 Refer to Figure 25 1 Install hardware securing back rest assembly to cabin bulkhead Verify security 3 If heated seats are installed push in circuit breaker on circuit breaker panel and turn battery switch on Verify proper function of switches at control panel Verify temperature setting system...

Страница 323: ...s 6 Apply B270 18 adhesive to underside of back rest cushion flap and to mating portion of support tube Pull flap around tube smooth wrinkles and trim excess flap Remove excess adhesive prior to curing 7 If heated seats are installed push in circuit breaker on circuit breaker panel and turn battery switch on Verify proper function of switches at control panel Verify temperature setting system func...

Страница 324: ...dule Clean up debris 4 Cleco sheet metal fastener new module to seat assembly pan Progressively remove clecos and install B204 1 rivets securing module to pan Verify security 5 Connect F940 harness to module at connector Verify security 6 Install seat assembly per 25 21 Part A D Scheduled Maintenance and Inspections Refer to 5 45 100 Hour Annual Inspection F Special Maintenance and Inspections 1 O...

Страница 325: ...Intentionally Blank APR 2019 Chapter 25 Furnishings Page 25 9 ...

Страница 326: ...FIGURE 25 2 CARPET AND INSULATION Page 25 10 Chapter 25 Furnishings APR 2019 ...

Страница 327: ... pedals as required C Aft Floor Carpet Assembly Removal and Installation 1 Refer to Figure 25 2 Attach or detach carpet to and from floor via hook and loop tape Velcro D Carpet and Liner CAUTION Use caution when removing adhered carpet if carpet is intended for reuse 1 Removal a Starting at corners gently peel back carpet by hand or with plastic wedge or putty knife b Dampen old adhesive with Dupo...

Страница 328: ...th clean cloth wet with acetone B Installation 1 Verify proper insulation fit Trim as required 2 Apply B270 8 adhesive to bonding surface and insulation backing Press insulation to surface smooth wrinkles and remove excess adhesive prior to curing 25 50 General Maintenance 25 51 Pilot s Operating Handbook POH Strap Replacement A Removal 1 Remove POH 2 Drill out rivets securing POH retaining strap ...

Страница 329: ... upper flap into frame 25 53 Map Pocket Replacement A Removal 1 Drill out rivets securing map pocket to front wall of forward seat box Remove pocket washers and retaining strips Deburr holes and clean up debris B Installation 1 Fold long outboard pocket edge around long A913 1 strip align holes and align holes with front of forward seat box Cleco in place 2 Pull material taut fold short inboard po...

Страница 330: ...ngle may be removed and shipped to RHC or a Kannad Service Center for reprogramming Kannad Aviation s Programming Data Sheet is available online at www robinsonheli com B Transmitter Removal 1 Release D693 4 strap assembly or B359 2 reusable ty rap 2 Release Velcro strap disconnect dongle and antenna wiring from transmitter at connectors and remove transmitter Installation 1 Connect dongle and ant...

Страница 331: ...00 grams If desired order one G654 15 decal blank maintenance log and attach to extinguisher to record weight checks Every 12 years Remove fire extinguisher from service Year of manufacture is labeled on bottom of extinguisher remove extinguisher from service at end of 12th year from labeled date B Bracket Removal 1 Unlatch fire extinguisher bracket and remove extinguisher 2 Remove hardware securi...

Страница 332: ...Intentionally Blank Page 25 16 Chapter 25 Furnishings APR 2019 ...

Страница 333: ...nd torque meter Each door contains an electric fan to aid with defogging A padded elbow rest is provided above the left side collective This allows the pilot to brace his elbow for stability while leaning out to see external loads The elbow rest is adjustable up and down via a friction knob A cabin interior hardpoint installation is for use with safety harnesses The cargo hook is suspended from a ...

Страница 334: ...nfigure helicopter for flight with hook removed per Part F as required C Installation 1 Turn battery switch off and pull out 10 amp HOOK RELEASE and 10 amp EXT LOAD if installed circuit breaker s on circuit breaker panel 2 Configure helicopter for flight with hook installed per Part F as required 3 Loosen jam nut and thread 528 029 00 cargo hook onto D676 3 cable assembly Verify threads protrude b...

Страница 335: ...ok and the helicopter is flying Every 100 hours of external load operations or annually whichever occurs first 1 Push in 10 amp HOOK RELEASE and 10 amp EXT LOAD if installed circuit breaker s on circuit breaker panel Turn battery switch on Refer to Figure 25 3 Verify proper function of electrical hook release Reset load beam by hand Verify lock indicator returns to locked position Turn battery swi...

Страница 336: ...40 7 installations with load cell harness assembly at connector on belly Install FTC 4 caps labeled FC 4 over open belly receptacle s verify cap security Cut and discard ty raps as required and remove harness assembly leave D676 3 control cable assembly looped to A215 149 o ring c Remove hardware securing D136 3 bumpers and D136 2 support to G137 1 hardpoint installation rod ends and remove bumper...

Страница 337: ...er 20 32 and torque stripe per Figure 5 1 c Remove FTC 4 cap labeled FC 4 from hook harness assembly receptacle on belly Connect G140 6 installations without load cell or G140 7 installations with load cell harness assembly to receptacle verify security Loop A215 149 o ring around harness and control cable assembly Install ty raps as required cinch ty raps until snug without over tightening and tr...

Страница 338: ...rip disconnect the electrical connectors located near the quick release pin before removing the left cyclic grip Reconnect the connectors when installing the left cyclic grip For removable collective stick a Removal Unplug push to start button cable from jack Unbutton boot and depress locking pins to disengage and remove collective stick b Installation Depress locking pins and insert collective st...

Страница 339: ...Intentionally Blank APR 2019 Chapter 25 Furnishings Page 25 23 ...

Страница 340: ...FIGURE 25 4 MECHANICAL RELEASE CONTROL RIGGING Shown with cover removed FIGURE 25 3 LOCK INDICATOR Page 25 24 Chapter 25 Furnishings APR 2019 ...

Страница 341: ... will begin to move and measure gap between fork and ball as shown 4 Adjust gap as required to obtain measurement between 0 15 0 25 inch To adjust gap a Disconnect cable assembly s ball from release lever assembly s fork b Remove cotter pin if installed castellated nut washers and bolt G132 1 or load cell G132 2 or G132 4 securing hook to hard point s D136 2 support Remove hook c Thread or unthrea...

Страница 342: ...emoved loop A215 149 o ring around harness and D676 3 control cable assembly Install ty raps as required cinch ty raps until snug without over tightening and trim tips flush with heads 2 Remove temporary thru bolt install load cell per 25 73 Part C steps 4 thru 10 Load Meter 1 Turn battery switch off pull out 10 amp HOOK RELEASE circuit breaker on circuit breaker panel 2 Install hardware securing ...

Страница 343: ...required and remove torquemeter and or MGT gage C Installation 1 Turn battery switch off and pull out 10 amp HOOK RELEASE circuit breaker on circuit breaker panel 2 Install hardware securing F600 2 torquemeter and T1221MK900C010 MGT gage to G138 4 face Connect G140 harness assembly to torquemeter and or MGT gage as required Verify security 3 Install hardware securing face with attached torquemeter...

Страница 344: ...y wiring from G140 9 harness assembly at connectors 3 Remove hardware securing fan assembly to door stiffener and remove fan C Installation Bubble Door WARNING Failure to install a ring in each door s two hinge pins may allow door to depart aircraft in flight 1 Turn battery switch off and pull out AUX PWR 10 amp circuit breaker on circuit breaker panel 2 Refer to 52 10 Align and insert door hinge ...

Страница 345: ...evise Weight and Balance Record in R66 Pilot s Operating Handbook POH Section 6 to incorporate the following data Right Door Subtract Weight Long Arm Long Moment Lat Arm Lat Moment Weigh door lb 49 50 in Weight x Long Arm 26 80 in Weight x Lat Arm Left Door Subtract Weight Long Arm Long Moment Lat Arm Lat Moment Weigh door lb 49 50 in Weight x Long Arm 26 80 in Weight x Lat Arm 2 Door s On Operati...

Страница 346: ...ections Every 100 hour annual inspection Inspect straps for security and any evidence of cracking or corrosion Inspect mirrors for cracks cleanliness and clarity D Configurations for Flight 1 Configuration for flight with skid mounted mirror s removed a Remove skid mounted mirror s including G138 support s per Part A b Reinstall screws in skid tube s to prevent debris and moisture from entering tu...

Страница 347: ...Removal Peel back headliner and remove hardware securing G949 2 ring to F087 1 frame remove ring B Installation Peel back headliner and install hardware securing G949 2 ring to F087 1 frame Standard torque fasteners per 20 32 and torque stripe per Figure 5 1 Position seam of grommet at top of hole in line with middle fastener 25 81 Arm Rest NOTE Flight with G135 7 support assembly 2454K71KNOB remo...

Страница 348: ...Intentionally Blank Page 25 32 Chapter 25 Furnishings APR 2019 ...

Страница 349: ...8 20 Fuel Quantity 28 7 28 21 Fuel Quantity Sender 28 7 28 22 Low Fuel Switch Assembly 28 10 28 23 Fuel Flow Meter Installation 28 11A 28 30 Fuel Valve 28 13 28 31 Fuel Valve Control Rigging 28 13 28 40 Fuel Flow Check 28 14 28 50 Aux Fuel System 28 17 28 51 Tank Assembly 28 18 28 52 Support Assembly 28 20 28 53 Bladder 28 21 28 54 Fuel Quantity Sender 28 25 28 55 Pump Assembly 28 25 ...

Страница 350: ...Intentionally Blank Page 28 ii Chapter 28 Fuel System JUL 2020 ...

Страница 351: ...nside an aluminum structure The filler cap is located under a cowl door The left and right side vent fittings are interconnected and vent through two risers within the mast fairing A fuel valve is located on the forward side of the firewall and is controlled by a push pull cable control at the base of the pilot s collective stick The engine incorporates a fuel pump assembly with an inlet filter A ...

Страница 352: ...Page 28 2 Chapter 28 Fuel System APR 2019 FIGURE 28 1 MAIN FUEL SYSTEM ...

Страница 353: ...ve cover Remove and discard o ring 5 Remove D277 8 clamp or cut and discard safety wire securing A729 tube to right rollover valve and pull tube off of valve Remove screws and washers securing valve to bladder and support Cut and discard ty rap securing 35486 hanger tab to G915 5 tab 6 Remove low fuel switch assembly per 28 22 Tape bladder openings 7 Disconnect D205 21 fuel outlet hose assembly fr...

Страница 354: ...lation CAUTION Avoid contaminating bladder assembly interior Cover arms with sleeves and use lint free gloves when working inside bladder 5 Remove tape from bladder assembly openings Insert a clean smooth blunt wooden dowel through bladder s fuel port opening and press on bladder lower surface to attach hook and loop tape Verify security 6 Install low fuel switch assembly per 28 22 7 Apply light c...

Страница 355: ...mbly per 53 23 as required 2 Refer to Figure 28 1 Remove D277 8 clamp s or cut and discard safety wire securing A729 tube to rollover valve and pull tube off of valve 3 Remove G254 2 fitting or G254 6 retainer Remove and discard MS29512 10 packing G254 2 fitting only and A215 015 o ring 4 Carefully remove B208 5 and B208 6 balls using a suction cup attached to a syringe Inspect condition of balls ...

Страница 356: ... to expose stem remove and discard o ring B Installation 1 Actuate and lock A761 2 or 1250H sump valve to expose stem install new o ring in stem seat 2 Refer to Figure 28 1 Lightly coat valve threads using B270 6 sealant Remove tape and install valve in bladder outlet Special torque A761 2 valve per 20 33 or standard torque 1250H valve per 20 32 and torque stripe per Figure 5 1 3 Secure A729 to va...

Страница 357: ... 04 harness assembly to F550 1 fuel quantity sender b Aux tank Disconnect G768 harness assembly from airframe harness and G759 cover assembly at connectors 4 Remove bolts securing fuel sender to cover assembly Carefully pull fuel sender lever through opening Tape bladder opening B Installation 1 Perform fuel sender check per Part C 2 Turn battery switch off and pull out 2 amp GAGES circuit breaker...

Страница 358: ...FIGURE 28 2 FUEL SENDER CHECK Page 28 8 Chapter 28 Fuel System JUL 2020 ...

Страница 359: ...ight coat A257 9 anti seize to threads and install screws securing G271 1 guard to cover assembly Verify security 7 Perform fuel indication check per Part D C Fuel Sender Check 1 Remove fuel sender per Part A 2 Simulate mounting position of appropriate F550 fuel quantity sender per Figure 28 2 Position float arm as shown and measure the resistance with a multimeter Verify resistance is within tole...

Страница 360: ...or 5 9 gallons 0 5 gallon small tank per 12 41 4 Refer to Figure 28 3 Push in 2 amp GAGES circuit breaker at panel and turn battery switch on Press QUANTITY button on aux fuel control panel for aux tank quantity displayed on fuel quantity gage Verify gage reads one half needle width to one one half needle widths below one quarter mark If fuel gage indication is correct proceed to step 6 5 If fuel ...

Страница 361: ...Intentionally Blank JUL 2020 Chapter 28 Fuel System Page 28 9B ...

Страница 362: ...ly through fuel cap opening avoiding fuel sender Install fuel cap and tape bladder opening C Installation 1 Lubricate new MS29512 05 packing with A257 6 grease and install packing over switch assembly threads 2 Refer to Figure 28 1 Remove fuel cap Tape A521 2 single or A521 4 dual switch assembly wiring to 4 ft length of lockwire insert other end of wire through fuel cap opening and through switch...

Страница 363: ...ert a clean non sparking rod through fuel cap opening and gently depress A521 switch assembly s float lower float if dual switch is installed verify LOW FUEL annunciator segment illuminates 5 Dual switch only Remove rod Service helicopter with additional 5 gallons fuel 12 gallons total per 12 41 Insert clean non sparking rod through opening and gently depress switch assembly s upper float verify 1...

Страница 364: ...8 33 for fuel flow meter installation electrical schematic C Removal Transducer 1 Remove engine cowling assembly per 53 21 2 Turn battery avionics switches off and pull out GPS 5 amp circuit breaker on panel Pull fuel shut off valve off 3 Disconnect airframe harness electrical connector from 660534HR 01 transducer assembly 4 Refer to Rolls Royce OMM Task 73 00 00 000 801 and observe precautions Pl...

Страница 365: ... fireshield 5 Remove caps and plugs from fittings Assemble engine washers G155 1 aft bracket engine nut new 2 AS4824N04 seals SS6565 8 4 reducer fitting new 2 AS4824N08 seals 660534HR 01 transducer assembly and 564601 tube assembly between fuel check valve and fuel control unit Install hardware securing G155 2 forward bracket to transducer and tighten screws install hardware securing G155 brackets...

Страница 366: ...security 5 Push in GPS circuit breaker 5 amp on panel Turn battery avionics switches on 6 Perform appropriate functional checks per Garmin GTN series or Avidyne IFD series moving map navigation display Pilot s Guide 7 Install aft left back rest assembly per 25 22 E Configuration Configure AIS 380 fuel flow adapter per Shadin Avionics M833811 01 Installation Manual Section 5 Make the following sele...

Страница 367: ...n and security Verify no damaged connectors Verify wiring neatness proper routing and installation and security Adapter Visually inspect adapter for any obvious damage verify proper installation and security Inspect wiring for loose chafed frayed or broken wires Verify no damaged connectors Verify wiring neatness proper routing and installation and security G Special Maintenance Transducer and Ada...

Страница 368: ...FIGURE 28 4 FUEL VALVE Page 28 12 Chapter 28 Fuel System JUL 2020 ...

Страница 369: ... nut securing A462 4 fitting and A522 11 fuel valve control inner wire to F670 1 fuel valve arm 2 Open baggage compartment door As required loosen hardware securing AN742 3 clamps and control housing to G915 3 bracket Position end of control housing flush to 0 25 inch at or beyond edge of G244 1 panel and install fasteners Verify security 3 Refer to detail in Figure 76 3 Push fuel valve into on po...

Страница 370: ...2 hose assembly from the engine fuel inlet fitting 6 Using a second suitable container push fuel valve into on position and drain fuel into second container for a few seconds to purge system of air Then fill the weighed container for 60 seconds Weigh and record weight of empty container 60 seconds of fuel flow in table below 7 Perform the following calculation Combined weight of empty container 60...

Страница 371: ...Intentionally Blank JUL 2020 Chapter 28 Fuel System Page 28 15 ...

Страница 372: ...FIGURE 28 5 AUX FUEL SYSTEM LARGE TANK SHOWN Page 28 16 Chapter 28 Fuel System JUL 2020 ...

Страница 373: ...is on the NO FLOW light indicates fuel is not transferring from auxiliary tank to the main tank either because the auxiliary tank is empty or the pump has failed It is normal for the light to illuminate for approximately five seconds when the pump is first switched on while the system is priming A time delay circuit automatically switches the pump off if the NO FLOW light is illuminated for more t...

Страница 374: ...rom airframe harness at connectors 4 Using a back up wrench disconnect D205 36 vent return and D205 36 pump hose assemblies from aux tank fittings in G759 1 cover assembly Install AN820 6 or AN929 6 caps included in MT183 1 kit on aux tank fittings Install AN806 6D plugs included in MT183 1 kit on hose fittings special torque plugs to 120 in lb and stow hoses in G769 1 bracket assembly 5 Remove B5...

Страница 375: ...aux tank fittings Using a back up wrench on fittings special torque hose nuts per 20 33 torque stripe per Figure 5 1 Verify security 5 Connect G768 4 harness assembly to airframe harness at connectors Verify security 6 As required revise Weight and Balance Record in R66 Pilot s Operating Handbook POH Section 6 to reflect aux tank assembly installation using the following data Add Item Weight Long ...

Страница 376: ...act Item Weight Long Arm Long Moment Lat Arm Lat Moment Large Tank Support Assy 3 0 lb 101 0 in 303 0 in lb 1 2 in 3 6 in lb Small Tank Support Assy 2 0 lb 96 8 in 193 6 in lb 0 4 in 0 8 in lb B Installation 1 Verify baggage compartment floor where G755 support assembly is to be installed is free of debris Position support assembly on floor 2 Install B526 6 screws securing support assembly to bulk...

Страница 377: ...cover assembly 5 Remove screws securing G758 1 cover to enclosure assembly Remove G762 12 hinge Guide cover clear of strap and remove cover 6 Detach bladder hook tape from enclosure loop tape and remove bladder Tape bladder openings B Installation 1 Fold forward aft and left sides of G756 bladder inward align bladder s G759 4 ring assembly with G754 enclosure assembly s servicing panel to clear st...

Страница 378: ...rain Verify security 7 Connect D205 drain hose assembly to drain fitting aligning hose 8 5 5 0 from parallel with edge of enclosure s G757 1 tray Using a back up wrench special torque hose nut per 20 33 and torque stripe per Figure 5 1 Secure hose near drain valve at tab Install MS336 7 9 ty rap securing scupper to hose Cinch ty rap until snug without overtightening and trim tip flush with head 8 ...

Страница 379: ...Intentionally Blank APR 2019 Chapter 28 Fuel System Page 28 23 ...

Страница 380: ...Page 28 24 Chapter 28 Fuel System APR 2019 FIGURE 28 6 AUX FUEL SYSTEM ELECTRICAL SCHEMATIC ...

Страница 381: ...sconnect D205 36 vent return and D205 36 pump hose assemblies from aux tank fittings in G759 1 cover assembly Temporarily cap and plug fittings AN820 6 and AN929 6 caps and AN806 6D plugs are included in MT183 1 kit 5 Refer to Figure 28 7 Remove screws securing G759 1 cover assembly and G756 bladder to G754 enclosure assembly Lift cover and inside bladder release clamp securing A729 73 tube to dra...

Страница 382: ...Page 28 26 Chapter 28 Fuel System JUL 2020 FIGURE 28 7 FUEL PUMP ...

Страница 383: ...nnect A729 73 tube to drain fitting and install D277 8 clamp verify security Connect A729 74 tube to G759 1 cover assembly install D277 8 clamp and ensure there is 1 00 3 00 inches between spirap and clamp verify security Install hardware securing pump connector to cover verify security 7 Install screws securing cover and bladder to G754 enclosure assembly verify security 8 Remove AN820 6 or AN929...

Страница 384: ...Intentionally Blank Page 28 28 Chapter 28 Fuel System JUL 2020 ...

Страница 385: ...CHAPTER 29 HYDRAULICS Section Title Page 29 00 Description 29 1 29 10 Hydraulic Pump 29 1 29 20 Hydraulic Reservoir 29 5 29 30 Hydraulic Servos 29 6 MAY 2015 Chapter 29 Hydraulics Page 29 i ...

Страница 386: ...Intentionally Blank Page 29 ii Chapter 29 Hydraulics MAY 2015 ...

Страница 387: ...and includes a filter pressure relief valve and pilot controlled pressure shut off valve A sight glass for pre flight fluid level checks is incorporated in the reservoir and accessible via a left side cowl door A vented filler cap is located on top of the reservoir The pressure shut off valve is solenoid actuated and controlled by the hydraulic switch on the pilot s cyclic The switch should be lef...

Страница 388: ...Page 29 2 Chapter 29 Hydraulics MAY 2015 FIGURE 29 1 HYDRAULIC FLIGHT CONTROL SYSTEM ...

Страница 389: ... secure Special torque nuts per 20 33 2 Install both MR rpm senders in pump bracket Adjust clearance between both senders and both yoke magnets to 0 040 0 020 inch and hand tighten sender jam nuts 3 Refer to Figure 12 4 Install F902 pressure line assembly special torque per 20 33 4 Install F902 suction line assembly and special torque per 20 33 5 Remove temporary air tight plug from reservoir and ...

Страница 390: ...Page 29 4 Chapter 29 Hydraulics JUL 2020 FIGURE 29 3 HYDRAULIC SERVO RIGGING FIGURE 29 2 HYDRAULIC SYSTEM SCHEMATIC ...

Страница 391: ...r LED and line and hose fittings from removed reservoir to replacement reservoir B Installation 1 Note alignment of tee fittings and sight gage LED on removed reservoir Transfer LED and line and hose fittings from removed reservoir to replacement reservoir Special torque fittings per 20 33 2 Install reservoir on gearbox and secure with three screws 3 Install pressure and suction lines repositionin...

Страница 392: ...securing C343 8 tube s lower rod end to F339 1 jackshaft weldment 5 Disconnect D205 hose assemblies from servo unions and tees Cap and plug fittings 6 Remove hardware securing servo to G201 1 frame weldment and remove servo 7 Aft Servo Measure and record center to center dimension between aft servo s lower rod end and C343 8 tube s lower rod end Loosen palnut and nut securing C343 8 tube to aft se...

Страница 393: ...o piston to dimension recorded during servo removal then tighten jam nut and palnut finger tight 2 Aft Servo Lightly coat servo s lower rod end threads with B270 21 protectant and install C343 8 tube Adjust tube on servo s rod end and tube s rod end to the center to center dimension between rod ends recorded during servo removal and with rod ends 90 to each other Tighten jam nuts and palnuts finge...

Страница 394: ...gs per 20 33 and torque stripe per Figure 5 1 Special torque hose B nuts per 20 33 and torque stripe per Figure 5 1 10 Bleed hydraulic system per 12 34 11 Perform the following measurements on all servos just installed a Measure and record dimension between clevis hole center top of servo piston b Apply cyclic and collective frictions With collective full down and hydraulics unpressurized position...

Страница 395: ...upper push pull tube per 29 30 Part A steps 1 thru 3 2 Remove clevis scissor and D200 3 washer from servo as applicable 3 Visually inspect threaded bore in piston with borescope Replace servo if corrosion is detected 4 Assemble servo and connect to upper push pull tube per 29 30 Part B steps 1 4 5 6 8 11 and 12 ...

Страница 396: ...Intentionally Blank Page 29 10 Chapter 29 Hydraulics JUL 2020 ...

Страница 397: ...es 32 5 32 30 Skid Tubes 32 7 32 31 Skid Shoes 32 8 32 32 Skid Extension Replacement 32 8 32 33 Ground Handling Wheel Support Replacement 32 8 32 40 Fairing Assemblies 32 9 32 50 Maintenance 32 9 32 60 Pop Out Floats Installation 32 11 32 61 Cylinder Assembly 32 11 32 62 Lever Rigging and Shear Rivet Replacement 32 17 32 63 Float Installation 32 19 32 64 System Maintenance 32 22 ...

Страница 398: ...Intentionally Blank Page 32 ii Chapter 32 Landing Gear R66 Maintenance Manual SEP 2012 ...

Страница 399: ... Remove fairing assemblies per 32 40 3 Refer to Figure 32 1 If installed remove hardware securing A936 3 ground wire assembly to aft right landing gear attachment 4 Using putty knife or plastic scraper cut sealant securing four cross tube rain caps to landing gear assembly and remove caps Remove sealant residue from caps cross tubes and strut assemblies Clean surfaces with solvent 5 Hoist helicopt...

Страница 400: ...FIGURE 32 1 LANDING GEAR ATTACHMENT Page 32 2 Chapter 32 Landing Gear MAY 2015 ...

Страница 401: ...o condenser support Verify security 3 Insert hardware thru access hole on aft left seat box forward wall and thru shackle Align mounting bolt with forward left landing gear attachment Install hardware special torque bolt per 20 33 torque stripe per Figure 5 1 4 Insert hardware thru right side access hole on baggage compartment aft wall and aft right landing gear attachment Install hardware special...

Страница 402: ...igital milliohm meter Model 310 BK Precision or similar d Attach negative black leads to battery ground strap attach positive red leads to the following ground locations and check readings i Tailcone forward bay strobe light ground stud ii Horizontal stabilizer tail light ground stud iii Main gearbox chip detector housing or MR temperature switch screw iv Left and right skid tube ground handling s...

Страница 403: ...Intentionally Blank APR 2017 Chapter 32 Landing Gear Page 32 3B ...

Страница 404: ...FIGURE 32 2 CROSS TUBE REMOVAL Page 32 4 Chapter 32 Landing Gear APR 2017 ...

Страница 405: ...es Using brass drift tap on strut assembly collars to separate struts from cross tube Do not tap on jack tabs C Installation Refer to R66 Illustrated Parts Catalog IPC Figure 32 1 NOTE When installing A936 3 ground wire assembly verify finish is removed from surface under wire terminal 1 Refer to Figure 32 2 Lightly coat mating surfaces of cross tube with zinc chromate or epoxy primer using approv...

Страница 406: ...FIGURE 32 3 SKID TUBES AND FAIRINGS Strut and skid tube angles exaggerated for clarity Page 32 6 Chapter 32 Landing Gear R66 Maintenance Manual SEP 2012 ...

Страница 407: ...mum length circumference scratch c 0 500 inch maximum width flat spot 4 Measure the thickness of skid tube s skid shoes five per skid Replace a skid shoe per Section 32 31 if damage exceeds 0 050 inch minimum thickness Repeat steps on opposite skid tube B Removal 1 Jack or hoist helicopter per Sections 7 10 or 7 20 Raise skids above ground approximately 4 inches 2 Refer to Figure 32 3 Remove hardw...

Страница 408: ... Remove skid extension 3 Clean interior of skid tube as practical Install new skid extension and align fastener holes 4 Install new A142 1 screws to secure aft skid shoe to skid tube Standard torque screws per Section 20 32 5 Install skid tube per Section 32 30 6 Fill gap in side of skid extension using B270 1 sealant Mix sealant according to manufacturer s instructions 32 33 Ground Handling Wheel...

Страница 409: ... fairing as required reinstall per preceding steps 32 50 Maintenance 1 Refer to Figure 32 3 Verify drain holes in bottom of skid tubes are free of obstructions two per skid between two forward skid shoes and aft of skid shoe at forward strut assembly 2 Refinish landing gear to prevent corrosion per Chapter 20 3 Inspect skid tubes and skid shoes per 32 30 especially following touch down autorotatio...

Страница 410: ...FIGURE 32 4 POP OUT FLOATS INSTALLATION Page 32 10 Chapter 32 Landing Gear APR 2019 ...

Страница 411: ...linder valve punctures the metal sealing disk and 4945 psig nominal at 20º C of helium is released into the inflation manifold to inflate both floats The manifold consists of hoses fittings and a check valve at each of the six float chambers per float Each float chamber has a topping valve for manual inflation and a pressure relief valve to vent excess internal pressure A modified aux stabilizer i...

Страница 412: ...FIGURE 32 5 POP OUT FLOATS CYLINDER ASSEMBLY Page 32 12 Chapter 32 Landing Gear R66 Maintenance Manual SEP 2012 ...

Страница 413: ...refully remove cylinder B Depressurization CAUTION Use appropriate eye and hearing protection Do not service cylinder assembly while cylinder is installed in helicopter 1 Remove cylinder per Section 32 61 Part A Verify MT545 1 pin assembly and MT546 1 diffuser are properly installed 2 Refer to Figure 32 5 Remove D760 7 cap etched with FILL PORT from valve assembly A loud pop may be heard when cap ...

Страница 414: ...ed 50ºC 122ºF or pressure to exceed 5500 psig If limits are approached stop fill and allow cylinder to cool and pressure to drop before continuing Placing cylinder in a water bath and using slow to moderate fill rates is recommended If using water bath keep water level below valve assembly to avoid water contamination of valve 1 Evaluate cylinder life and hydrostatic test status 2 Refer to Figure ...

Страница 415: ... cabin structure in three locations Carefully position cylinder in D669 6 cradle assembly 4 Engage D676 2 cable assembly ball in D760 1 trigger do not kink cable Install MS3367 4 9 ty rap as shown Cinch ty rap until snug without over tightening and trim tip flush with head Install hardware securing D761 1 support to valve 5 Verify cable housing protrudes through clamps on support flush to 0 200 in...

Страница 416: ...Page 32 16 Chapter 32 Landing Gear R66 Maintenance Manual SEP 2012 FIGURE 32 6 POP OUT FLOATS LEVER RIGGING AND SHEAR RIVET REPLACEMENT ...

Страница 417: ...ed raise collective full up push in and rotate D680 1 lever assembly safety to READY position squeeze lever to remove cable slack and verify 1 25 1 30 in between tip of lever and collective stick as shown As required reposition D676 2 cable assembly housing at lever to obtain dimension 3 Push in and rotate lever safety to LOCKED position Simultaneously squeeze lever and verify no preload in cable ...

Страница 418: ...Page 32 18 Chapter 32 Landing Gear R66 Maintenance Manual SEP 2012 FIGURE 32 7 POP OUT FLOATS FLOAT INSTALLATION ...

Страница 419: ... Use care when removing C944 retainer strips from girts and when separating girts from skid tube and skid extension Repeat steps for opposite float B Installation 1 Refer to Figure 32 7 Verify outboard bolt heads securing struts to skids are covered with B270 1 sealant Apply additional sealant as required 2 Position deflated float over skid tube and skid extension Align holes in C944 retainer stri...

Страница 420: ...Page 32 20 Chapter 32 Landing Gear R66 Maintenance Manual SEP 2012 FIGURE 32 8 POP OUT FLOATS FLOAT PACKING ...

Страница 421: ...th the assistance of six or seven people 7 Refer to Figure 32 8 Detail D Align hoses and valve cover flaps Roll float from outboard edge toward skid tube as tightly as possible Hold float on top of skid 8 Apply A257 7 lubricant to mating surfaces of float cover and outboard girt snaps Button snaps and secure hook and loop fasteners 9 Refer to Figure 32 8 Detail E Verify lacing cords are installed ...

Страница 422: ...se valves 4 Inflate floats with filtered oil free dry air to 2 0 psig via topping valves 5 Allow float air temperature to stabilize for 5 minutes minimum then record OAT and pressure in each float chamber 6 One to two hours after initial pressure check again record OAT and pressure in each float chamber Allowable chamber pressure drop from initial measurement is 0 2 psig adjusted for any temperatu...

Страница 423: ...rivet Time for floats to attain full shape without wrinkles should be three seconds or less CAUTION Floats inflate rapidly and with a loud noise Keep area clear during inflation and inform all nearby personnel Remove or close all doors prior to inflation Open doors interfere with float inflation and may be damaged 4 Allow float temperatures to stabilize for at least five minutes then record OAT an...

Страница 424: ...ure drop from initial measurement is 0 20 psi adjusted for any temperature change For example float chamber pressure will decrease 0 6 psig if temperature drops 10 degrees C 8 If leaks are detected repair float with supplied repair kit then perform leak check per Section 32 64 Part A on repaired float chamber 9 Connect D674 1 hose assembly to valve fitting Orient line as required to maintain minim...

Страница 425: ...Title Page 33 00 Description 33 1 33 10 Exterior Lights 33 1 33 11 Strobe Light s 33 1 33 12 Navigation Lights 33 2 33 13 Landing Lights 33 3 33 20 Interior Lights 33 3 33 21 Panel Light 33 3 MAY 2015 Chapter 33 Lights Page 33 i ...

Страница 426: ...Intentionally Blank Page 33 ii Chapter 33 Lights MAY 2015 ...

Страница 427: ...ding lights are installed in the nose One wide angle and one narrow beam light are used to increase lighted area One landing light switch controls both lights and is located on the cyclic center post NOTE Continuous operation of landing and position lights in flight is recommended to promote collision avoidance An optional flashing light may be mounted on the tailcone in addition to the standard a...

Страница 428: ...rdware securing light assembly gasket and ground wire to chin Cut and discard ty rap securing excess wire to light assembly pull out light assembly and disconnect light assembly harness from airframe harness at connector b Tail Light Remove screws securing retainer lens gasket and light assembly to stabilizer mount Pull out light assembly and disconnect light assembly harness from airframe harness...

Страница 429: ...erify function Turn battery switch and landing light switch off 33 20 Interior Lights 33 21 Panel Light A LED Assembly Replacement 1 Turn battery switch off Pull out LTS circuit breaker 5 amp at panel 2 Remove hardware securing G196 light assembly to windshield stiffener Remove two cap screws securing cover and LED assembly to housing Disconnect LED assembly wires from airframe harness and remove ...

Страница 430: ...Intentionally Blank Page 33 4 Chapter 33 Lights MAY 2015 ...

Страница 431: ...52 13 Gas Springs 52 7 52 20 Door Vent Replacement 52 7 52 21 Weather Seal Door Vent Replacement 52 7 52 22 Door Vent Hinge Replacement 52 8 52 23 Pivot Friction Adjustment 52 8 52 30 Windshield Installation 52 11 52 31 Standard Acrylic Windshield Installation 52 11 52 32 Impact Resistant Polycarbonate Windshield Installation 52 14 JUL 2020 Chapter 52 Doors and Windows Page 52 i ...

Страница 432: ...Intentionally Blank Page 52 ii Chapter 52 Doors and Windows JUL 2020 ...

Страница 433: ...efer to Figures 52 1 and 52 2 To disconnect door from gas spring mechanism a Forward Doors Pull D573 4 rod up and off of arm assembly ball joint b Aft Doors Insert flat tip screwdriver and pry up spring clip locking C394 1 gas spring to channel ball joint Pull gas spring up and off of ball joint 2 Remove rings from door hinge pins lift pins up from door frame hinge assemblies and remove door 3 Adj...

Страница 434: ...FIGURE 52 1 DOOR ASSEMBLY Page 52 2 Chapter 52 Doors and Windows JUL 2020 ...

Страница 435: ...r seals sit approximately even against door frame recess 5 Using soft pencil and a straight edge draw cross hairs through centers of door upper hinge assembly pre drilled holes Hold fitted door against frame insert new door mounted hinge assembly in frame mounted hinge assembly and transfer cross hairs onto hinge Remove hinge and door 6 Drill two 0 170 inch diameter holes at cross hair intersectio...

Страница 436: ...in locked position Apply thin coat B270 10 adhesive on screw threads install hardware and tighten screw 5 Bond hole plug in place using B270 9 adhesive 52 12 Weather Seal Door Assembly Replacement 1 Remove damaged weather seal using plastic wedge or putty knife Remove hardened adhesive using approved solvent per 20 70 or 60 grit sandpaper as required 2 Refer to Figure 52 1 Measure and trim continu...

Страница 437: ...Intentionally Blank 25 OCT 2010 R66 Maintenance Manual Chapter 52 Doors and Windows Page 52 5 ...

Страница 438: ...FIGURE 52 2 GAS SPRINGS AND DOOR VENTS Page 52 6 Chapter 52 Doors and Windows R66 Maintenance Manual 25 OCT 2010 ...

Страница 439: ...ndpaper 3 Hold fitted door vent in recess and match drill hinge four 0 098 inch diameter holes Smooth hole edges clean up debris Prepare surfaces for clamping using approved solvents per Section 20 70 Install rivets securing door to hinge 4 Extend pivot arm to approximately 1 85 inch between center of pins Match drill pivot arm assembly angle two 0 098 inch diameter holes Smooth hole edges clean u...

Страница 440: ...ole edges clean up debris Prepare surfaces for clamping using approved solvents per Section 20 70 4 Refer to Section 52 20 Verify proper vent door fit install rivets securing hinge to door assembly and door vent Prepare surfaces and touch up rivet heads and hinge using approved materials per Section 20 70 52 23 Pivot Friction Adjustment To increase pivot arm assembly friction tighten nut securing ...

Страница 441: ...Intentionally Blank JUL 2020 Chapter 52 Doors and Windows Page 52 9 ...

Страница 442: ...Page 52 10 Chapter 52 Doors and Windows JUL 2020 FIGURE 52 3 WINDSHIELD INSPECTION ACRYLIC WINDSHIELD SHOWN ...

Страница 443: ...er 52 10 Part B Remove hardware securing C228 4 upper hinge assembly to door frame and remove hinge NOTE If windshield is to be reinstalled prior to removal tape protective paper or film to the inside and outside of the windshield to prevent damage 2 Remove hardware securing C238 27 or C238 28 side retainer to door frame and remove retainer 3 Install upper hinge assembly and install door assemblie...

Страница 444: ...367 lower retainers Run a bead of B270 26 sealant along entire edge of tape line With a second person inside cabin to tighten nuts latch forward doors Install hardware securing lower retainers C366 8 retainer and C366 5 bracket to cabin Remove tape and wipe off excess sealant with cheesecloth wet with lacolene 7 Remove F238 4 upper retainer Run a bead of B270 26 sealant along entire edge of tape l...

Страница 445: ...tisfied with alignment lay out masking tape on windshield for trimming WARNING Review appropriate Safety Data Sheet SDS when working in proximity to hazardous materials Specific recommendations for use of personal protective equipment are located in the SDS 5 A band saw with a blade containing at least 24 teeth per inch is recommended for initial trimming Tape cardboard to band saw table to preven...

Страница 446: ...Inspection Inspect both windshields for cracks and crazing adjacent to retainers per Figure 52 3 Also inspect areas adjacent to fasteners and stainless steel straps for cracks and crazing If cracks exceed these limits replace damaged windshield per 52 31 Part F Inspect windshields for any significant discoloration or cloudiness Minor defects or imperfections that do not impair pilot visibility or ...

Страница 447: ...co G367 ties straps tabs and retainers to frames Also cleco G367 ties straps and tabs to windshield at center bow if drilled 3 Install C228 4 upper door hinge assembly Install forward door assemblies for cabin structure support during windshield installation 4 If windshield is drilled and has hardware G367 ties straps pads and tabs installed a With a second person inside cabin to tighten nuts latc...

Страница 448: ... 20 33 Wipe off excess sealant with cheesecloth wet with lacolene 7 At lower retainers a Remove F367 lower retainers Remove G367 straps and expand pilot holes to 0 169 0 175 inch diameter holes thru windshield Finish holes with reamer deburr back side of holes using plastic razor Clean up debris b Apply B270 26 sealant to G367 12 tabs and position on windshield Run a bead of B270 26 sealant along ...

Страница 449: ...rding to manufacturer s instruction 13 Remove protective paper or film from inside and outside of the windshield 14 Repeat steps to install opposite side windshield as required F Replacement 1 Perform 52 31 Part F steps 1 thru 4 WARNING Review appropriate Safety Data Sheet SDS when working in proximity to hazardous materials Specific recommendations for use of personal protective equipment are loc...

Страница 450: ...Intentionally Blank Page 52 18 Chapter 52 Doors and Windows JUL 2020 ...

Страница 451: ...2 Mast Fairing 53 3 53 23 Tailcone Cowling 53 4 53 24 Access and Inspection Panels 53 4 53 30 Frame Assemblies 53 5 53 31 Lower Frames 53 5 53 32 Hydraulic Servo Support Frame 53 9 53 33 Upper Frame 53 10 53 40 Tailcone Assembly 53 13 53 41 Inspection and Repair 53 15 53 50 Empennage Assembly 53 17 53 51 Vertical Stabilizer 53 18 53 52 Horizontal Stabilizer 53 19 53 53 Tail Rotor Guard 53 21 53 54...

Страница 452: ...Intentionally Blank Page 53 ii Chapter 53 Fuselage APR 2017 ...

Страница 453: ...ess panel under the left front seat or in the main baggage compartment depending on aircraft configuration The engine is located aft of the main baggage compartment The engine compartment is isolated from the rest of the airframe by stainless steel firewalls in front of and above the engine 53 10 Cabin Assembly The cabin assembly is a non field replaceable assembly 53 11 Repair 1 Vertical firewall...

Страница 454: ...FIGURE 53 1 FAIRING COWLINGS AND PANELS Page 53 2 Chapter 53 Fuselage R66 Maintenance Manual 25 OCT 2010 ...

Страница 455: ...039 ring is centered on exhaust weldment within 0 1 inch Remove and reinstall replace ring as required 53 22 Mast Fairing A Opening and Closing 1 Refer to Figure 53 1 Remove right side screws securing F261 1 mast fairing assembly at aft vertical seam 2 Remove right side screws securing fairing to ribs Keep fairing from springing open and minimize strain on nutplates by holding fairing closed until...

Страница 456: ... pitot line leak test per 95 10 53 23 Tailcone Cowling A Removal and Installation 1 Refer to Figure 53 1 Thru left access door disconnect ELT antenna lead from antenna mounted to F706 1 tailcone cowling assembly as required 2 Remove screws securing cowling to fuselage and remove cowling 3 Reinstall cowling and install screws securing cowling to fuselage 4 Connect ELT antenna lead to cowling thru l...

Страница 457: ...uired Cut and discard ty raps as required mark wires and disconnect wires at plastic connectors to liberate frame 4 Using plastic scraper remove sealant around frame weldment s at firewalls 5 Support tailcone until frames are reinstalled a F046 1 LH only Remove hardware securing frame to F574 5 block access bolt thru G246 1 brace inside baggage compartment Remove hardware securing shackle and fram...

Страница 458: ...FIGURE 53 2 LOWER FRAMES Page 53 6 Chapter 53 Fuselage JUL 2020 ...

Страница 459: ...1 support weldment is approximately symmetrical with minimal preload Adjust rod end extension on both sides as required per 5 33 and Figures 5 1 5 2 ensure rod extension is no more than 1 10 inches Install hardware securing weldment to lower frames standard torque bolts per 20 32 and torque stripe per Figure 5 1 Remove tailcone support 4 Seal around frame weldment s at firewalls using B270 1 seala...

Страница 460: ...FIGURE 53 3 HYDRAULIC SERVO SUPPORT FRAME Page 53 8 Chapter 53 Fuselage JUL 2020 ...

Страница 461: ...s and hardware Lift frame off of gearbox over mast assembly B Installation 1 Refer to Figure 53 3 Lower G201 1 servo support frame over mast assembly onto main rotor gearbox Install gearbox mounting bolts mounts and hardware Install nuts finger tight 2 Remove tags and install hardware securing D212 servo assemblies to frame forward plates and aft bracket Standard torque bolts per Section 20 32 and...

Страница 462: ... 19 hoseassemblyandF724 1 lineassemblyfromF823 1 thermostat assembly Plug hose and line and cap fittings Remove hardware securing F651 1 oil filter assembly to frame 12 Remove hardware securing F231 8 braces to fuel bladder support and to frame 13 Remove hardware securing rotor brake cable assembly to frame Remove hardware securing B157 1 pulley mount to frame 14 Remove ELT transmitter per Section...

Страница 463: ... fuel bladder support and to frame 7 Install hardware securing F651 1 oil filter assembly to frame Standard torque hardware per 20 32 and torque stripe per Figure 5 1 Remove caps and plugs and connect D205 19 hose assembly and F724 1 line assembly to F823 1 thermostat assembly Standard torque hose assembly nuts per 20 32 special torque line assembly nuts per 20 33 torque stripe per Figure 5 1 8 In...

Страница 464: ...Page 53 12 Chapter 53 Fuselage MAY 2015 FIGURE 53 4 TAILCONE ASSEMBLY ...

Страница 465: ...ly on F020 1 upper frame assembly do not pinch wiring between tailcone bulkhead and frames Install hardware securing tailcone to frames standard torque bolts per Section 20 32 and torque stripe per Figure 5 1 3 Install hardware securing D224 tail rotor drive shaft yoke to C947 3 intermediate plate assembly Shim tail rotor driveline per 65 30 Standard torque bolts per 20 32 and torque stripe per Fi...

Страница 466: ...FIGURE 53 5 TAILCONE INSPECTION AND REPAIR Page 53 14 Chapter 53 Fuselage MAY 2015 ...

Страница 467: ...xceeds limits return tailcone assembly to RHC for repair If damage is within limits blend out scratches with a 0 10 inch minimum blend radius Refinish skins using approved materials per Section 20 70 B Dents 1 Refer to Figure 53 5 Smooth round bottom dents with 0 125 inch minimum radius without sharp nicks or cracks are acceptable when damage does not exceed the following limits a 0 030 inch maxim...

Страница 468: ...FIGURE 53 6 EMPENNAGE TAILCONE CASTING Page 53 16 Chapter 53 Fuselage R66 Maintenance Manual 25 OCT 2010 ...

Страница 469: ... required to secure wires and connectors together Cinch ty raps until snug without over tightening and trim tips flush with heads 3 Test and verify correct function of position and TR chip light circuits 4 Install tail rotor guard assembly per 53 53 C Repair A single dent on the C044 1 stabilizer leading edge outboard of the vertical stabilizers is permitted provided 1 Dent is no more than 0 050 i...

Страница 470: ...ilizer Removal 1 Remove tail rotor guard assembly per 53 53 2 Remove aux stabilizer assembly per 53 52 and tail skid per 53 54 as required 3 Refer to Figure 53 6 Remove fastener securing C554 clips to upper horizontal stabilizer trailing edge 4 Support C043 1 lower vertical stabilizer Remove four bolts threaded and spacers securing C043 1 stabilizer to upper horizontal stabilizer and remove C043 1...

Страница 471: ... 51 3 If C044 1 stabilizer was replaced match drill C554 clips 0 144 inch diameter hole through trailing edge of horizontal stabilizer Deburr hole and install fastener 4 Connect position light at connectors Install hardware securing forward clamp to upper horizontal stabilizer Install MS3367 4 9 or 5 9 ty raps as required to secure position light and gearbox chip detector wires and connectors toge...

Страница 472: ...FIGURE 53 7 EMPENNAGE TAIL ROTOR GUARD Page 53 20 Chapter 53 Fuselage MAY 2015 ...

Страница 473: ...izer if not previously accomplished Insert D079 1 guard assembly aft through blocks 2 Lightly coat retaining hardware and mating surfaces of D082 1 tube assembly and D079 1 guard assembly with approved primer per 20 70 prior to installation 3 Install D081 1 spacer inside tube While wet with primer slide guard onto tube and install hardware Standard torque bolts per 20 32 and torque stripe per Figu...

Страница 474: ...moved B Installation 1 Refer to Figure 53 7 Install C470 3 spacer inside C470 1 tail skid Install tail skid and two C470 2 blocks inside C043 1 lower vertical stabilizer Install D081 4 block assembly and install hardware securing block assembly to stabilizer Standard torque screw per 20 32 and torque stripe per Figure 5 1 2 Install D081 2 block and hardware securing block to stabilizer Verify D081...

Страница 475: ...al and Shim Calculations 62 11 62 32 Adjusting Hinge Friction 62 15 62 33 Drilling Nuts and Bolts 62 17 62 34 Static Balance 62 17B 62 40 Inspection of Main Rotor Blades 62 18 62 41 Scratches and Corrosion 62 19 62 42 Dents 62 20 62 43 Spar Damage 62 21A 62 44 Root Fitting Damage 62 21B 62 45 Nicks and Notches 62 23 62 46 Voids and Debonds 62 25 62 50 Repair of Main Rotor Blades 62 27 62 51 Sealin...

Страница 476: ...Intentionally Blank Page 62 ii Chapter 62 Main Rotor JUL 2020 ...

Страница 477: ...he spindle tusk contacts an aluminum droop stop attached to the main rotor shaft to minimize teetering when blades are at rest or turning at low RPM 62 10 Main Rotor Blades WARNING Due to potentially destructive results use of blade tape anti erosion tape is prohibited A Removal Refer to Figure 62 1 Four people will be required to remove the blades One person must support the blade approximately 2...

Страница 478: ...FIGURE 62 2 TEETER HINGE HUB INSTALLATION FIGURE 62 3 CONING HINGE BLADE INSTALLATION Page 62 2 Chapter 62 Main Rotor R66 Maintenance Manual 25 OCT 2010 ...

Страница 479: ...r to R66 Illustrated Parts Catalog IPC Figures 62 1 62 3 and 62 5 1 Verify correct teeter hinge friction per Section 62 32 step 4 2 If previously installed information is unavailable perform coning hinge journal and shim calculation per Section 62 31 3 Refer to Figure 62 3 With rotor hub level insert journals into coning hinge bearings Install thrust washer on coning hinge bolt 4 Position blade in...

Страница 480: ...FIGURE 62 4 MEASURING BOLT STRETCH Shown on teeter hinge bolt Page 62 4 Chapter 62 Main Rotor R66 Maintenance Manual 25 OCT 2010 ...

Страница 481: ...ach bolts must be stretched from 0 020 0 022 inch 0 021 0 022 inch for new undrilled bolt to obtain proper clamping force Under stretching or over stretching can cause catastrophic failure of the bolts 10 Connect pitch link to pitch horn Standard torque per 20 32 install palnut and torque stripe per Figure 5 1 11 Repeat steps 1 thru 10 for remaining blade If installed main rotor blade pitch bearin...

Страница 482: ...TE C156 1 Black blade boots are standard C156 2 grey boots are optional for use in sub freezing temperatures 1 Visually inspect and verify boot is undamaged Carefully stretch new boot over spindle 2 Solvent clean surfaces clamped by boot inner lip Properly position boot inner lip install C165 1 inner clamp assembly and tighten clamp to 2 850 0 005 inch outside diameter Rotate spindle and verify ad...

Страница 483: ... per Section 20 70 Inspect journals and thrust washers for chipping of chrome plating corrosion and or wear grooves extending through chrome plating 0 0006 inch maximum wear Replace journal or thrust washer if any of these conditions exist 2 Line up mark on hub with chord arm on rotor shaft 3 Refer to Figure 62 2 Reinstall teeter hinge bolt thrust washers shims and journals exactly as removed If p...

Страница 484: ...FIGURE 62 6 MAIN ROTOR HUB BEARING INSTALLATION FIGURE 62 5 MAIN ROTOR HUB BEARING REMOVAL Page 62 8 Chapter 62 Main Rotor R66 Maintenance Manual 25 OCT 2010 ...

Страница 485: ...er and install wet 62 21 Bearing Replacement Refer to R66 Illustrated Parts Catalog IPC Figure 62 3 1 Remove main rotor hub per Section 62 20 2 If main rotor hub is to be reinstalled with same blades measure and record shim thicknesses and locations in hub 3 Refer to Figures 62 2 and 62 3 Measure and record hub width across widest point of teeter and coning hinge bearing faces total of three measu...

Страница 486: ... bearing flange contacts hub CAUTION Use MT643 1 support when installing coning hinge bearings Never install coning hinge bearings into unsupported hub 8 Seal between bearing flange and hub with epoxy primer Similarly seal between inboard edge of bearing and hub Do not allow primer to contaminate Teflon portion of bearing 9 Measure hub width across teeter and coning hinge bearing faces Compare wid...

Страница 487: ...fy no scoring scratches or other obvious damage Polish out fretting or corrosion to 0 002 inch maximum depth on inner and outer surfaces within 2 125 inches of bearing bores Polish out fretting or corrosion to 0 001 inch maximum depth on inside of bearing bores maximum bearing bore diameter is 1 5618 inches b Visually inspect all other areas of hub for obvious damage Polish out nicks scratches gou...

Страница 488: ...ent penetrant inspect hub per 20 42 5 Prime hub per 20 60 6 Install bearings per 62 21 steps 6 thru 8 7 Mask bearings and topcoat hub assembly per 20 60 8 When top coat has sufficiently cured remove masking Page 62 10B Chapter 62 Main Rotor JUL 2020 ...

Страница 489: ...rust washer and journal Subtract combined measured thickness of selected journal and shims inches Difference inches 4 Subtract measured length of C106 5 journal to be used on nut side inches Difference inches CAUTION Initial teeter hinge hardware stack up must be adjusted to 0 005 0 008 inch greater than calculated empty space A smaller initial stack up could damage thrust washers and hub bearings...

Страница 490: ... and thrust washer Deviate from initial trailing edge shim stack up as necessary to meet coning hinge axial play per Figure 62 8 and maintain friction requirements as follows It must be possible to manually cone each blade without teetering the hub when blades are held up off the droop stops and lifted at tip Increasing shim stack up or journal length decreases hinge friction C106 Journal Lengths ...

Страница 491: ...Intentionally Blank 25 OCT 2010 R66 Maintenance Manual Chapter 62 Main Rotor Page 62 13 ...

Страница 492: ...FIGURE 62 7 MEASURING TEETER HINGE FRICTION Page 62 14 Chapter 62 Main Rotor R66 Maintenance Manual 25 OCT 2010 ...

Страница 493: ...asher and C117 shims under nut 3 Refer to Table 62 1 Measure thickness of C117 shims under teeter hinge nut Change shims as necessary to adjust friction Reducing shim stack up by 0 003 0 005 inch will increase teeter friction Increasing shim stack up will reduce teeter friction 4 Reassemble teeter shims thrust washer and nut Repeat step 1 Torque teeter hinge bolt per Section 62 20 Part B steps 4 t...

Страница 494: ...FIGURE 62 8 MEASURING THRUST WASHER AND HUB BEARING GAP Page 62 16 Chapter 62 Main Rotor R66 Maintenance Manual 25 OCT 2010 ...

Страница 495: ...een blade s thrust washers and hub bearings NOTE When a shim is replaced with a shim of a different size it will be necessary to install a new nut and bolt Drilled holes in original bolts will not align at required bolt stretch 5 Replace coning hinge bolt with a new bolt 6 Install shims and new bolt and nut per 62 10 Part B steps 4 thru 6 7 Repeat steps 1 and 2 Drill new bolt and nut per 62 33 coa...

Страница 496: ...FIGURE 62 8A MT524 2 MAIN ROTOR STATIC BALANCE FIXTURE ASSEMBLY Page 62 17A Chapter 62 Main Rotor JUL 2020 ...

Страница 497: ... thrust washers and hub bearing faces per Figure 62 8 verify total axial clearance at each hinge is between 0 002 0 006 inch 3 Refer to Figure 62 8A Install MT524 2 main rotor static balancing fixture assembly in hub as shown Hoist main rotor assembly and position on MT009 9 base assembly 4 Refer to Figure 62 8B Verify blade pitch angles are approximately equal with pitch horns adjusted as shown I...

Страница 498: ...stem by adding C298 balance strips NAS1149F0332P washers and or NAS1149F0363P washers as required Final balance to be within one NAS1149F0332P washer 8 Apply light coat A257 9 anti seize to threads and install screws securing tip weights to blade special torque screws to 40 in lb Apply light coat A257 9 anti seize to threads and install screws securing tip cover to blade special torque screws to 4...

Страница 499: ...Intentionally Blank JUL 2020 Chapter 62 Main Rotor Page 62 17D ...

Страница 500: ...nd size of the voids that exceed the limits NOTE The inspection criteria in this section applies to blade damage that occurs after blade manufacturing including shipping and handling and time in service Damage after blade manufacturing usually exhibits paint scuffing scratches or freshly exposed metal in the form of scratches in the finish If a blade manufacturing irregularity is suspected contact...

Страница 501: ...nt of material removed 2 Use a straight edge and thickness gage to measure repaired areas less than 2 inches across in the blade skins and spar 62 41 Scratches and Corrosion A Skins and Doublers 1 Refer to 62 50 for repair procedures Polish out damage by hand with a 0 10 inch minimum blend radius 2 Refer to 62 40 for measuring damage and measuring material removed after repair Repair may not excee...

Страница 502: ...0 62 42 Dents CAUTION Tap test dented areas in honeycomb If any voids are found associated with dents contact RHC Customer Service Tap test voids debonds and dents in blades using an AN970 4 washer or 1965 or later U S quarter dollar coin in good condition CAUTION When dented areas are found inspect opposite side of the blade for a bulge Replace blade with a bulge greater than 0 010 inch opposite ...

Страница 503: ... length is 4 0 inches between RS 162 90 and RS 196 50 f Replace blade with any dent in 0 7 inch area immediately aft of skin to spar bond line g For dents in skins and or doublers inboard of RS 70 00 contact RHC for repair procedures 2 Refer to Part C for leading edge cap damage Refer to 62 50 for repair procedures for damage within limits B Trailing Edge Bond Joints 1 Refer to Figure 62 12 Verify...

Страница 504: ...y damage does not exceed the following limits a 0 020 inch maximum depth between RS 70 00 and RS 198 00 b Replace blade if erosion has reduced thickness at spar leading edge to 0 040 inch c Replace blade if erosion has cause ripples in or deformation to spar leading edge 2 Refer to 62 50 for repair procedures for damage within limits Blend out spar damage with a minimum 1 0 inch blend radius ...

Страница 505: ...ollowing limits a 0 040 inch maximum depth on outside diameter of flange b 0 002 inch maximum depth on area 0 35 inch outboard of flange c 0 060 inch maximum depth on other root fitting exposed areas 2 Refer to 62 50 for repair procedures for damage within limits Blend out root fitting damage with a minimum 1 0 inch blend radius ...

Страница 506: ...FIGURE 62 15 REPAIRS TO BLADE AND TRIM TAB TRAILING EDGES FIGURE 62 16 MINIMUM CHORD AFTER BLADE AND TRIM TAB TRAILING EDGE REPAIRS Page 62 22 Chapter 62 Main Rotor APR 2019 ...

Страница 507: ...pection criteria B Blade Tip 1 Refer to Figure 62 17 Using a fine toothed hand file file in spanwise or chordwise direction within limits indicated Remove file marks using 220 grit or finer aluminum oxide abrasive paper 2 File trailing edge to maintain square edge at skins perpendicular to chord line per Figure 62 15 Seal exposed trailing edge bond joint 3 Track and Balance Main Rotor per Chapter ...

Страница 508: ...FIGURE 62 17 BLADE TIP REPAIR LIMITS FIGURE 62 18 TIP CAP SPAR AND TRAILING EDGES VOID AND DEBOND LIMITS Page 62 24 Chapter 62 Main Rotor APR 2019 ...

Страница 509: ... doubler Verify no individual void larger than 0 10 square inch except at the doubler finger tips The finger tips may be debonded from the outboard tip to 1 0 inch inboard Voids that are separated by less than 0 25 inch shall be considered continuous b Non Critical Areas Area more than 50 inch spanwise or more than 30 inch chordwise from doubler edges Verify void does not exceed 2 0 inches chordwi...

Страница 510: ...FIGURE 62 20 HONEYCOMB VOID AND DEBOND LIMITS FIGURE 62 19 DOUBLERS VOID AND DEBOND LIMITS Page 62 26 Chapter 62 Main Rotor JUL 2020 ...

Страница 511: ...ge is removed 5 Measure reworked area and verify material removed and or new chord dimension is permissible per 62 40 6 Seal and fill per 62 51 as required Paint per 62 52 as required 7 Track and balance main rotor per Chapter 18 as required 62 51 Sealing Filling and Fairing 1 Clean area needing sealing filling and fairing with QSOL 220 2 a Apply B270 27 adhesive to seal all exposed bond joints ex...

Страница 512: ...r with 320 grit abrasive paper or very fine Scotch Brite and wipe down with a lint free cloth dampened with enamel cleaner prior to applying new coat NOTE Best results are achieved if primer is allowed to air dry for 12 hours prior to top coat application 4 Refer to Figure 62 21 Apply dark gray flat black white and or yellow Dupont Imron polyurethane enamel or equivalent see Approved Materials 20 ...

Страница 513: ...ated in the SDS CAUTION Do NOT use power tools or chemical paint strippers to remove blade paint 2 Remove any corrosion and loose paint from skins on upper or lower surface of blade aft of skin to spar bond joint by hand sanding in a spanwise direction using 220 grit aluminum oxide abrasive paper and minimum 0 1 inch blend radius finish sand with 320 grit aluminum oxide abrasive paper Remove only ...

Страница 514: ...oly sulfide refer to 20 79 and allow to cure 5 Prime remaining exposed metal with two coats of epoxy primer chromated epoxy preferred 6 Apply yellow paint topcoat within 2 48 hours of primer application For best performance allow paint to cure 48 hours before flight 7 Install tip covers and special torque screws to 40 in lb wet with A257 9 anti seize ensure cover edges are flush with blade profile...

Страница 515: ...eldment 63 1 63 11 Engine Driveline Forward Flex Plate Shimming 63 2 63 12 Clutch Assembly 63 5 63 20 Main Rotor Gearbox Assembly 63 6 63 21 Yoke and Seal Replacement 63 8 63 30 Rotor Brake 63 13 63 31 Pad Replacement 63 14 63 40 Rotor RPM 63 14 APR 2017 Chapter 63 Main Rotor Drive System Page 63 i ...

Страница 516: ...Intentionally Blank Page 63 ii Chapter 63 Main Rotor Drive System APR 2017 ...

Страница 517: ...mblies per 71 22 3 Refer to Figure 63 1 Remove hardware securing F453 1 box assembly to F234 1 firewall 4 Remove hardware securing forward A947 2 flex plate assembly to F910 1 main gearbox yoke and F642 engine shaft weldment forward flange noting hardware removed Remove flex plate and temporarily suppport forward portion of shaft weldment 5 Remove hardware securing shaft weldment to aft A947 2 fle...

Страница 518: ...complished remove hardware securing forward A947 2 flex plate assembly to F910 1 main gearbox yoke and F642 engine shaft weldment forward flange Remove flex plate and temporarily suppport forward portion of shaft weldment 3 Measure flex plate thickness at bonded washers 4 places to determine average thickness 1st place inch 2nd place inch 3rd place inch 4th place inch Total inch Total 4 inch Flex ...

Страница 519: ...quirements given in 20 33 Calculated Dimension Shim required between forward A947 2 flex plate and F910 1 main gearbox yoke Shim required between forward A947 2 flex plate and F642 engine shaft weldment forward flange 0 041 inch or greater negative number NAS1149F0432P washer between aft A947 2 flex plate assembly and F642 engine shaft weldment aft flange and or F018 1 clutch assembly yoke may be ...

Страница 520: ...Page 63 4 Chapter 63 Main Rotor Drive System JUL 2020 FIGURE 63 1 ENGINE DRIVELINE ...

Страница 521: ...50 C300 A1 Remove clutch assembly through main rotor gearbox compartment B Installation 1 Refer to Figure 63 1 Lubricate F018 1 clutch assembly splines using A257 1 9 or 12 2 Route clutch assembly through main rotor gearbox compartment insert clutch assembly in Rolls Royce engine model 250 C300 A1 and install spacer earlier R66s G732 cap and bolt at rear PTO pad Standard torque bolt per 20 32 and ...

Страница 522: ...205 19 and D205 20 hose assemblies from F006 1 main rotor gearbox and D500 3 oil pump Cap and plug fittings and hoses 8 Disconnect F059 01 cabin harness assembly plug from F049 01 gearbox harness assembly receptacle Remove hardware securing A936 3 ground wire assembly to F560 1 bulkhead assembly 9 Remove D277 8 clamp or cut and discard safety wire securing Tygon tube to G254 1 fuel vent assembly a...

Страница 523: ...r Figure 5 1 4 Remove hoisting equipment and lifting fixture or nylon rope 5 Install Tygon tube on G254 1 fuel vent assembly and install D277 8 clamp Verify security 6 Install hardware securing A936 3 ground wire assembly to F560 1 bulkhead assembly Connect F059 01 cabin harness assembly plug to F049 01 gearbox harness assembly receptacle 7 Remove caps and plugs and connect D205 19 and D205 20 hos...

Страница 524: ...r to Figure 63 2 Set rotor brake Remove and discard lockwire securing F904 1 plug to yoke and remove plug using a 3 4 inch hex bit socket Visually inspect forward C947 3 flex plate assembly and plug for damage Order replacement parts from RHC Customer Service if damage is found 5 Remove hardware securing F254 1 cover with C966 8 seal to F006 1 main rotor gearbox Remove cover 6 Using hydraulic pres...

Страница 525: ... Standard torque hardware per MM 20 32 and torque stripe per MM Figure 5 1 Ensure safety wire is not contacting flex plate 8 Install and shim intermediate C947 3 flex plate assembly per MM 65 30 9 Install hardware securing aft F305 5 inlet to scroll assembly Verify 0 10 inch minimum gap between fanwheel assembly and inlet 10 Install tailcone cowling assembly per 53 23 11 Set hall effect sender to ...

Страница 526: ...securing yoke to pinion then remove yoke 5 Remove rotor brake per 63 30 6 Remove F255 cover with C966 seal but do not remove shims under pinion bearing Remove F266 2 spacer 7 Using hydraulic press press old seal from cover D Engine Driven F910 1 Yoke Assembly and Seal Installation CAUTION Do not remove shims under pinion bearing Shims control bearing preload and gear backlash 1 Refer to Figure 63 ...

Страница 527: ...Intentionally Blank APR 2017 Chapter 63 Main Rotor Drive System Page 63 11 ...

Страница 528: ...FIGURE 63 3 ROTOR BRAKE Page 63 12 Chapter 63 Main Rotor Drive System APR 2017 ...

Страница 529: ...all yoke on pinion shaft Place a wood block between firewall and yoke flange to prevent yoke from rotating Install pinion retaining nut and washer and special torque nut per 20 33 Coat nut and exposed pinion splines with B270 21 protectant When dry torque stripe per Figure 5 1 5 Attach B774 3 spring to gearbox cartridge retaining screw and rotor brake assembly link Attach D126 2 cable assembly to ...

Страница 530: ...110 1 arm assembly to 2 G111 1 bars and B112 2 lever but do not torque 2 Lubricate spacers with A257 1 grease and install in new G109 1 arm assembly Install D774 4 spring and install hardware securing G109 1 arm assembly to 2 G111 1 bars and G113 1 2 links Standard torque all bolts and torque stripe per Figure 5 1 3 Install rotor brake per 63 30 63 40 Rotor RPM 1 Remove tailcone cowling assembly p...

Страница 531: ...11 Static Balance 64 5 64 20 Tail Rotor Blades 64 8 64 30 Tail Rotor Blade Inspection and Repair 64 11 64 31 Scratches and Corrosion 64 11 64 32 Dents 64 13 64 33 Erosion 64 14 64 34 Root Fitting Damage 64 14 64 35 Nicks and Notches 64 14 64 36 Painting 64 14 64 40 Tail Rotor Hub 64 17 64 41 Bearing Replacement 64 17 64 42 Inspection 64 17 ...

Страница 532: ...Intentionally Blank Page 64 ii Chapter 64 Tail Rotor APR 2019 ...

Страница 533: ... teetering stop is a urethane bumper attached to the output shaft 64 10 Tail Rotor Assembly A Removal 1 Refer to Figure 64 1 Tag each pitch link with corresponding blade serial number for reinstallation Remove hardware securing pitch links to tail rotor blades noting hardware removed NOTE Tail rotor pitch link to blade attach bolts may be different lengths and or have different washers installed u...

Страница 534: ...FIGURE 64 1 TAIL ROTOR INSTALLATION Page 64 2 Chapter 64 Tail Rotor APR 2019 ...

Страница 535: ...ynamic check 4 Fabricate a tracking aid using 1x12 inch aluminum sheet make a 90º bend 2 inches from one end With tail rotor horizontal tape tracking aid to tailcone near blade tip 5 Rotate tail rotor drive shaft and mark tracking aid where each blade tip drain hole passes Adjust teeter tail rotor until both blade tips pass the same point within 0 125 inch Special torque teeter hinge bolt per Sect...

Страница 536: ...FIGURE 64 2 CHORDWISE STATIC BALANCE Page 64 4 Chapter 64 Tail Rotor R66 Maintenance Manual 25 OCT 2010 ...

Страница 537: ...e blade falls trailing edge first the top blade is the light blade 3 To simulate pitch link attachment assemble hardware as shown and install in blade pitch horns Install standard washer nut and palnut on heavy blade fastener Standard torque hardware per 20 32 4 Chordwise balancing is achieved by varying NAS6604 bolt length and nut side washers on light blade fastener Select bolt length and washer...

Страница 538: ...FIGURE 64 3 SPANWISE STATIC BALANCE Page 64 6 Chapter 64 Tail Rotor JUL 2020 ...

Страница 539: ...quivalent balancing stand Hold tail rotor assembly horizontally then allow to fall The falling blade is the heavy blade the rising blade is the light blade 4 Spanwise balancing is achieved by varying nut side washer size on light blade outboard fastener Four washers are required under outboard fastener nuts place largest washers closest to hub assembly Select washers for balancing standard torque ...

Страница 540: ...o Figure 64 1 If removed apply light coat of approved primer per 20 70 to outer surface of C138 2 bushings while primer is wet press bushings flush with inboard side of hub inboard arm bushings will seat properly with fastener torque applied CAUTION F137 2 spacer creates blade precone angle and must be installed on the outboard side of blade on the blade outboard spanwise fitting 3 Install tail ro...

Страница 541: ...Intentionally Blank APR 2019 Chapter 64 Tail Rotor Page 64 9 ...

Страница 542: ...FIGURE 64 4 SCRATCHES AND CORROSION Page 64 10 Chapter 64 Tail Rotor APR 2019 ...

Страница 543: ... questions as to the possibility of a manufacturing irregularity contact RHC Technical Support CAUTION A blade may be repaired more than one time However in no case can more than the maximum material be removed or the maximum dent depth be exceeded in any one location Refer to 62 40 for measuring blade damage 64 31 Scratches and Corrosion 1 Refer to Figure 64 4 Verify damage does not exceed the fo...

Страница 544: ...FIGURE 64 5 DENTS Page 64 12 Chapter 64 Tail Rotor APR 2019 ...

Страница 545: ...n the limits of this section must be removed from service immediately and marked scrap A Skins 1 Refer to Figure 64 5 Smooth round bottom dents with 0 060 inch minimum radius may be repaired when damage does not exceed the following limits a 0 010 inch maximum depth between leading edge and 0 75 inch aft chordwise b 0 75 inch aft chordwise of leading edge i 0 090 inch maximum dent depth between RS...

Страница 546: ...or for repair procedures for damage within limits Blend out root fitting damage with a minimum 1 0 inch blend radius 64 35 Nicks and Notches A Trailing Edge 1 Verify damage does not exceed the following limits a 0 050 inch maximum in the extreme trailing edge 2 Refer to 62 50 main rotor for repair procedures for damage within limits Blend out nicks and notches in blade trailing edge for 1 0 inch m...

Страница 547: ...Intentionally Blank APR 2019 Chapter 64 Tail Rotor Page 64 15 ...

Страница 548: ...Page 64 16 Chapter 64 Tail Rotor APR 2019 FIGURE 64 7 ELASTOMERIC BEARING INSTALLATION FIGURE 64 6 ELASTOMERIC BEARING REMOVAL ...

Страница 549: ...ile primer is wet press bearing into hub using MT556 11 bearing removal and installation tools Wipe away excess primer 3 Repeat steps for second bearing as required 64 42 Inspection 1 Remove tail rotor blades per 64 20 and inspect blades per 64 30 2 Remove elastomeric bearings per 64 41 3 Clean G062 1 tail rotor hub using approved solvent per 20 70 4 Visually inspect for indications of damage wear...

Страница 550: ...Intentionally Blank Page 64 18 Chapter 64 Tail Rotor APR 2019 ...

Страница 551: ... 00 Description 65 1 65 10 Tail Rotor Drive Fan Shaft 65 1 65 20 Tail Rotor Drive Shaft Assembly 65 3 65 21 Runout 65 5 65 22 Damper Assembly 65 7 65 30 Tail Rotor Driveline Intermediate Flex Plate Shimming 65 8 65 40 Tail Rotor Gearbox Assembly 65 10 65 41 Output Shaft Seal Replacement 65 11 65 42 Input Shaft Seal Replacement 65 12 ...

Страница 552: ...Intentionally Blank Page 65 ii Chapter 65 Tail Rotor Drive System R66 Maintenance Manual SEP 2012 ...

Страница 553: ...ove hardware securing intermediate C947 3 flex plate assembly to F196 1 tail rotor fan shaft aft flange and D224 tail rotor drive shaft assembly forward yoke noting hardware removed Remove flex plate and temporarily support aft portion of fan shaft 4 Remove hardware securing fan shaft to forward C947 3 flex plate assembly 5 Remove hardware securing fan shaft to G174 1 fanwheel assembly Carefully p...

Страница 554: ...FIGURE 65 1 TAIL ROTOR DRIVELINE Page 65 2 Chapter 65 Tail Rotor Drive System MAY 2015 ...

Страница 555: ...cone Support drive shaft as required 2 Install hardware securing drive shaft to aft C947 3 plate assembly as removed and remove support Standard torque fasteners per 20 32 and torque stripe per Figure 5 1 Install A558 2 cover 3 Refer to Figure 65 3 Remove forward A231 tailcone plug assembly Estimate longitudinal gap or interference between C041 12 damper assembly arm and D072 1 bulkhead assembly a...

Страница 556: ...FIGURE 65 2 RUNOUT Page 65 4 Chapter 65 Tail Rotor Drive System MAY 2015 ...

Страница 557: ...ft when pressing dial indicator firmly against inspection hole edges Have a second person rotate rotor system by turning tail rotor hub 4 Rotate rotor system slowly smoothly and for several revolutions until the technician is able to determine the average indicated movement Maximum runout is 0 025 inch 5 Repeat steps at each inspection hole Record values as required recommended during 100 hour or ...

Страница 558: ...FIGURE 65 4 DAMPER ASSEMBLY Page 65 6 Chapter 65 Tail Rotor Drive System MAY 2015 ...

Страница 559: ...d torque stripe per Figure 5 1 3 Attach a calibrated spring scale to Point A Holding link verify force required to rotate arm about Point B is 3 5 5 8 lb Adjust as required per Part C 4 Attach a calibrated spring scale to Point B Holding bearing assembly verify force required to rotate link about point C is 2 1 3 6 lb Adjust as required per Part C C Friction Adjustment CAUTION Do not adjust damper...

Страница 560: ... fan shaft aft flange arms and D224 tail rotor drive shaft assembly forward yoke flange arms at 3 o clock and 9 o clock positions horizontal Measure gap between arms to determine average gap 3 o clock position inch 9 o clock position inch Total inch Total 2 inch Average gap between flange arms b Rotate D224 tail rotor drive shaft assembly 180º and repeat step a 3 o clock position inch 9 o clock po...

Страница 561: ...ft forward yoke 0 017 or greater negative number NAS1149F0432P washer between forward C947 3 flex plate assembly and F908 1 yoke assembly and or F196 1 fan shaft forward flange may be relocated under nut as required to achieve 0 016 0 016 inch calculated dimension Relocate washers as required and repeat steps 3 thru 6 0 016 0 016 in None None 0 017 0 047 in NAS1149F0432P washer None 0 048 0 079 in...

Страница 562: ...move gearbox B Installation 1 Position tail rotor gearbox assembly on tailcone casting and install mounting hardware Special torque screws per 20 33 and torque stripe per Figure 5 1 2 Connect chip detector wiring at plastic connector and install ty raps as required Cinch ty raps until snug without over tightening and trim tips flush with heads 3 Install hardware securing gearbox input yoke to aft ...

Страница 563: ...g Clean and dry cap especially seal seating surface and o ring groove 6 Verify open face of seal points toward gearbox and press new seal into cap bore 0 160 inches from external surface Lightly coat new o ring with A257 22 oil and install in cap 7 Lightly coat output shaft seal seating area with A257 22 lubricant and slide cap onto shaft Install hardware securing cap to gearbox and special torque...

Страница 564: ... A966 3 seal and C215 140 o ring CAUTION Do not remove C141 2 washer between cap and bearing 4 Using hydraulic press press old seal from cap Remove and discard o ring Clean and dry cap especially seal seating surface and o ring groove 5 Verify open face of seal points toward gearbox and press new seal into cap bore 0 25 inch from external surface Lightly coat new o ring with A257 22 oil and instal...

Страница 565: ...ive Stick Assembly 67 6 67 22 Collective Friction 67 8 67 30 Jackshaft and Strut Assembly 67 8 67 31 Jackshaft 67 8 67 40 Swashplate 67 9 67 41 Swashplate Tilting Friction Adjustment 67 11 67 42 Upper and Lower Scissor Assemblies 67 11 67 50 Tail Rotor Controls 67 13 67 51 Pedals 67 13 67 52 Pitch Control 67 14 67 60 Bellcranks 67 15 67 61 C317 5 or C317 9 Bellcrank 67 15 67 62 C317 7 Bellcrank 67...

Страница 566: ...Intentionally Blank Page 67 ii Chapter 67 Flight Controls MAY 2015 ...

Страница 567: ...WARNING Assembly of flight controls is critical and requires inspection by a qualified person If a second person is not available the installer must take a 5 minute break prior to inspecting flight control connections he has assembled 67 10 Cyclic Controls Refer to R66 Illustrated Parts Catalog IPC Chapter 67 67 11 Cyclic Control Assembly A Removal 1 Refer to Section 6 70 Remove F794 1 forward and...

Страница 568: ...FIGURE 67 1 MAIN ROTOR FLIGHT CONTROLS Page 67 2 Chapter 67 Flight Controls R66 Maintenance Manual MAR 2012 ...

Страница 569: ...d push pull tube assembly aft through belly B Installation 1 Refer to Figure 67 1 Verify center to center distance between rod end and spherical bearings in G205 5 fork is 5 40 0 03 inches adjust as required Standard torque jam nut and palnut per Section 20 32 Install C175 5 cyclic pivot assembly torque tube yoke bellcranks fork and push pull tube assemblies thru aft belly 2 Connect G205 1 fork as...

Страница 570: ...67 12 Cyclic Grip Assembly A Removal NOTE This may be accomplished without removal of complete cyclic assembly from rotorcraft 1 Remove forward belly panel 2 Refer to Figure 67 1 Disconnect wiring connectors attached to wiring exiting base of D320 8 cyclic stick Using pin extractor remove pins from housings wires 112 138 355 may remain installed and retain housings Remove lacing tape from both end...

Страница 571: ...en placed full up Install circular plug 4 Temporarily attach grip assembly wiring to safety wire or lacing exiting atop cyclic stick Carefully pull wires thru cyclic stick Install grommet included with grip assembly wiring into cyclic stick wiring entrance hole Remove safety wire or lacing 5 Position protective sleeving on wiring exiting cyclic stick bottom to cover maximum amount of wiring possib...

Страница 572: ...pply collective friction 2 Refer to Figure 6 8 Remove F445 1 forward tunnel cover F680 3 pilot s collective cover F680 1 co pilot s collective cover F463 1 mid tunnel cover and F461 1 collective cross tube cover 3 Pivot pilot s seat bottom to the open position Remove bolt securing inboard end of collective stick to pilot s seat structure Refer to Figure 76 1 Disconnect throttle control inner wire ...

Страница 573: ...e stripe per Figure 5 1 6 Refer to Figure 6 8 Slide F680 3 collective cover over center collective stick aft of friction assembly 7 Insert A130 4 spacer into lower end of A333 1 collective travel stop Position spacer and stop in F348 1 anchor Install NAS1149F0432P and 0463P washers on spacer on either side of stop as required to obtain 0 001 0 035 inch axial play and align stop with collective Sec...

Страница 574: ...ft to G201 1 frame 3 Remove jackshaft B Installation 1 Ensure A105 6 journal is installed in jackshaft aft support on G201 1 frame Position F339 1 jackshaft on G201 1 frame and install bolts Standard torque bolts per 20 32 install palnuts and torque stripe per Figure 5 1 2 Insert bolt forward thru forward jackshaft arm and connect to upper end of F121 7 push pull tube Install A115 1 spacer A214 3 ...

Страница 575: ...ree lugs on lower non rotating swashplate Connect aft push pull tube to right side of aft single lug on lower swashplate Standard torque bolts per 20 32 Install palnuts and standard torque per 20 32 2 Verify swashplate tilting friction per 67 41 adjust as required 3 Slide swashplate boot over main rotor drive shaft and set in place 4 Install C203 yokes on C251 main rotor drive shaft upper flange u...

Страница 576: ... 20 32 and torque stripe per Figure 5 1 11 Connect upper A205 fork rod end and lower rod end of C258 pitch link to interrupter side swashplate ear and standard torque bolt per 20 32 Install palnut standard torque per 20 32 and torque stripe per Figure 5 1 12 Position swashplate boot on rotating swashplate with inner lip contacting C203 yoke Secure with ty raps 13 Attach two A255 3 counterweights a...

Страница 577: ...ness increases tilting friction while increasing spacer stack thickness decreases tilting friction Install and special torque per 20 33 all inner screws on lower swashplate and at least two screws thru retainers in upper swashplate prior to measuring tilting friction 5 Connect both forward push pull tubes to lower swashplate and standard torque per 20 32 Install palnut special torque per 20 33 and...

Страница 578: ...Page 67 12 Chapter 67 Flight Controls MAY 2015 FIGURE 67 3 TAIL ROTOR FLIGHT CONTROLS ...

Страница 579: ...r and lower portion of blocks DO NOT mix them or alignment problems may develop on installation 5 Remove bolts securing A318 1 and 2 bearing block halves together and remove lower bearing blocks 6 Remove pedal assemblies one at a time by lifting one end and lowering other into chin Remove pedals thru pilot side opening NOTE On reassembly the right pedal assembly is mounted forward in the bearing b...

Страница 580: ...shaft 2 With pitch control s input stud thru short arm of A120 5 bellcrank assembly position bellcrank on tail rotor gearbox and install NAS6604 25 bolt one AN960 416L washer under bolt head two MS20002 4 washers one on each side of bearing and MS21042 L4 nut Tighten but don t torque at this time 3 Measure vertical gap between A120 5 bellcrank arm and flange on pitch control stud Install sufficien...

Страница 581: ...assembly flange holes and install hardware Standard torque nut and palnut per 20 32 and torque stripe per Figure 5 1 2 Position support with attached bellcrank in helicopter and install hardware securing support to side panels Verify security 3 Verify C343 11 push pull tube s rod end center to center dimension is 5 82 0 03 inches and C343 13 push pull tube s rod end center to center dimension is 5...

Страница 582: ...in hole aft and an A141 3 washer against outboard face of each journal install bellcrank on F334 1 support assembly and retain with NAS6604 67 bolt 2 Install two NAS1149F0463P and one NAS1149F0432P washer followed by MS21042L4 nut on NAS6604 67 bolt Standard torque bolt per 20 32 Install palnut special torque per 20 33 and torque stripe per Figure 5 1 3 Connect F121 9 push pull tube assembly to C3...

Страница 583: ... in helicopter with longer arm pointing up 3 On inboard end of C494 2 shaft install two NAS1149F0463P washers followed by MS17825 4 castellated nut Tighten nut until it aligns with hole in shaft and install new MS16562 14 spring pin 4 On outboard end of shaft install C130 34 spacer and MS21042L4 nut Special torque nut to 90 in lb Install palnut and special torque per 20 33 Torque stripe inboard an...

Страница 584: ...9F0432P washer 2 Install bellcrank with straight side aft on F020 1 frame s boss and secure to frame with an NAS1149F0432P washer and MS21042L4 nut Standard torque bolt per 20 32 Install palnut special torque per 20 33 and torque stripe per Figure 5 1 67 65 A120 5 Bellcrank A Removal 1 Remove hardware securing C121 17 push pull tube assembly to A120 5 bellcrank assembly 2 Disconnect bellcrank pivo...

Страница 585: ...ce Maintenance Facility 71 7 71 12 Preparing Engine for Helicopter Installation 71 7B 71 20 Induction 71 11 71 21 Air Filter Assembly 71 11 71 22 Cage Assembly 71 17 71 23 Engine Inlet Bellmouth 71 17 71 30 Exhaust Weldment 71 19 71 40 Accessories 71 20 71 41 Starter Generator 71 20 71 42 Generator Control Unit GCU 71 20 71 43 Engine Monitoring Unit EMU 71 21 ...

Страница 586: ...Intentionally Blank Page 71 ii Chapter 71 Powerplant JUL 2020 ...

Страница 587: ...gh efficiency filter includes a sight gage inside the upper left cowl door with provides an indication of filter dirt load NOTE The high efficiency filter is recommended for operating in dusty conditions The filter may not filter fine sand or dust resulting in reduced engine life If the air filter becomes blocked spring loaded doors at the front of the filter housing open allowing unfiltered air t...

Страница 588: ...FIGURE 71 1 ENGINE RIGHT SIDE Page 71 2 Chapter 71 Powerplant JUL 2020 ...

Страница 589: ... on inducer bleed port and tape box assembly to protect openings from contaminants 5 Remove hardware securing G391 1 customer air line assembly clamps Loosen line assembly B nut from G391 5 line assembly union and disconnect B nut from engine compressor union Cap fitting and plug line 6 Drain engine oil per 12 60 drain engine oil per RR300 Operation and Maintenance Manual OMM Refer to Figure 79 3 ...

Страница 590: ...1 support weldment Cut and discard safety wire and remove two bolts one per side securing side engine mounts to F046 lower frames 12 Carefully remove engine verify F579 1 bellmouth is clear of firewall and loose wires cables fittings and line assemblies are clear of engine during separation Install bellmouth cover 13 Prepare engine for Rolls Royce maintenance facility per 71 11 as required Page 71...

Страница 591: ...Intentionally Blank JUL 2020 Chapter 71 Powerplant Page 71 3B ...

Страница 592: ...FIGURE 71 2 ENGINE LEFT SIDE Page 71 4 Chapter 71 Powerplant JUL 2020 ...

Страница 593: ... safety wire will be installed in step 7 b Verify 0 2 inch minimum clearance between F642 shaft weldment and firewall grommet To adjust clearance i Remove two bolts securing support weldment rod ends to engine bottom mount and remove support weldment ii Adjust rod end extension on both sides as required per 5 33 and Figures 5 1 5 2 ensure rod extension is no more than 1 10 inches iii Repeat steps ...

Страница 594: ...tting per RR300 OMM Remove plug and connect B283 12 fuel hose assembly B nut to inlet fitting Special torque B nut per 20 33 and torque stripe per Figure 5 1 Push fuel shut off valve ON 15 Connect cabin electrical harness plug to N2 speed sensor connect cabin harness TMP torquemeter oil pressure and MOP main oil pressure plugs to engine senders Connect cabin harness to engine electrical harness at...

Страница 595: ...b Remove hardware securing harness wire terminal to igniton exiter box stud c Cut and discard ty raps as required and disconnect G426 1 fuel differential pressure switch assembly wire from harness at connectors Cut and discard stand off ty raps at switch wire and F741 1 line assembly d Remove hardware securing 2 MS21919WCH4 clamps to bottom of engine gearbox e Disconnect harness plugs from anti ic...

Страница 596: ... securing F593 3 plate to bottom of engine gearbox and remove plate 10 Remove bolt spacer if installed and G732 cap securing F018 1 clutch assembly in engine gearbox and remove clutch assembly 11 Remove AN815 8D union from engine gearbox TANK VENT port AN815 8D union or CV26 77 check valve early R66s from OIL OUTLET port and AN815 10D union from OIL INLET port Remove D745 3 pressure switch assembl...

Страница 597: ...arbox TANK VENT port Special torque union per 20 33 and torque stripe per Figure 5 1 6 Inspect F018 1 clutch assembly splines and verify no evidence of galling Also verify end of thread insert is 0 090 0 110 inch inboard from tip of splined end of clutch housing F018 1 Rev A thru C only contact RHC Technical Support if thread insert position is incorrect Lubricate clutch splines using B270 21 prot...

Страница 598: ...x special torque nuts per 20 33 and torque stripe per Figure 5 1 b Install MS21919WCH8 clamp around harness assembly and install clamp on F577 3 bracket assembly Install and tighten hardware Install bracket on right side of engine gearbox special torque nuts per 20 33 and torque stripe per Figure 5 1 c Connect harness to D745 3 pressure switch assembly at connectors Verify security Install 2 MS336...

Страница 599: ...gure 71 5 Verify F169 2 exhaust base and engine exhaust collector mating surfaces are clean and dry and lay 0 25 inch bead 7020 3 ceramic putty on top of exhaust collector flange Position F169 2 base F577 5 bracket earlier R66s and F173 2 shield if installed on exhaust collector and install hardware Verify security Remove excess putty Install exhaust protective cover 17 Refer to Figure 76 1 Instal...

Страница 600: ...FIGURE 71 3 INDUCTION STANDARD FILTER SHOWN Page 71 10 Chapter 71 Powerplant JUL 2020 ...

Страница 601: ...am filter is installed over the G057 1 cage assembly refer to 71 22 and secured with locking cords Filter should be removed cleaned with water when visibly dirty replace filter if foam is visibly damaged or deteriorated The optional G058 1 inlet barrier filter cage assembly is a separate installation with additional parts that secure the filters to the G057 1 cage assembly and that secure the asse...

Страница 602: ...Page 71 12 Chapter 71 Powerplant APR 2019 FIGURE 71 4 INDUCTION INLET BARRIER FILTER SHOWN ...

Страница 603: ...mbly release latch and move strap assembly aside 3 Remove 146150 101 filter from G058 1 cage assembly brackets handle filter by the potting to avoid damaging pleated media 4 Repeat steps 2 and 3 for other filter C Installation Standard Filter 1 Refer to Figure 71 3 Remove temporary cover Pull F771 1 filter assembly aft over G057 1 cage assembly and tighten cords as required Verify security 2 Insta...

Страница 604: ...t Barrier Filter 1 Visually inspect each filter assembly for obvious damage replace filter s as required per Parts B and C 2 To clean and dry each filter assembly a Remove debris as practical from dirty side of filter assembly using a soft bristle brush CAUTION Use only ZOK 27 cleaner to clean filter media CAUTION Do not use steam a high pressure washer or compressed air to clean filter assemblies...

Страница 605: ...ilter Visually inspect filter pleats for straightness Visually inspect filter media for small ruptures tears or holes Visually inspect potting compound for cracks gouges or gaps between filter and compound Replace filter s as required per Parts B and C CAUTION Verify filter media is completely dry before applying oil Use only approved oil never put an un oiled filter in service 5 Apply 4 5 oz tota...

Страница 606: ...oors are opened individually then simultaneously Turn battery switch off If bypass switch functions properly replace F771 1 filter assembly per Parts B and C If pilot reports a failed power assurance check refer to 5 43 replace F771 1 filter assembly per Parts B and C Inlet Barrier Filter If pilot reports AIR FILTER caution segment illuminates during engine operation when engine is shut down verif...

Страница 607: ...65 10 71 23 Engine Inlet Bellmouth A Removal 1 Remove engine per 71 10 2 Refer to Figure 71 3 Remove F579 1 bellmouth cover and loosen B277 36 clamps securing bellmouth to engine front support Remove bellmouth and clamps 3 Remove hardware securing F597 1 seal and F580 1 inlet to engine front support Remove seal and inlet Install cover over front support B Installation 1 Refer to Figure 71 3 Remove...

Страница 608: ...FIGURE 71 5 EXHAUST Page 71 18 Chapter 71 Powerplant JUL 2020 ...

Страница 609: ... 3 Verify base and engine exhaust collector mating surfaces are clean and dry and lay 0 25 inch bead 7020 3 ceramic putty on top of exhaust collector flange 2 Position F169 2 base F577 5 bracket earlier R66s and F173 2 shield if installed on exhaust collector and install hardware Verify security Remove excess putty 3 Position F169 1 exhaust weldment on base and install fasteners securing exhaust w...

Страница 610: ...orque stripe per Figure 5 1 3 Install engine cowling assembly per 53 21 71 42 Generator Control Unit GCU A Removal 1 Open baggage compartment door Remove hardware securing G248 1 cover battery compartment to inner compartment and remove cover 2 Disconnect F049 GCU electrical harness plug from GCU Remove mounting hardware and remove GCU Cap receptacles B Installation 1 Open baggage compartment door...

Страница 611: ...warning segment illuminates and is solid indicating normal EMU operation See R66 Pilot s Operating Handbook Section 7 for complete description Turn battery switch off 4 Install hardware securing F003 4 RH seat back assembly to cabin C Downloading EMU Data NOTE An EMU USB receptacle is located inside the aft right seat baggage compartment on the underside of the aft ledge Use a flashlight and mirro...

Страница 612: ... battery switch off and connect battery ground cable to battery negative terminal 6 While observing the built in indicator light on the EMU turn battery switch on and verify light illuminates but does not flash Steady illumination of built in indicator light means normal EMU operation A slow flashing 0 5 hz flashing light or no illumination indicates EMU or monitored sensor failure perform RR300 O...

Страница 613: ...CHAPTER 75 ENGINE AIR SYSTEMS Section Title Page 75 00 Description 75 1 75 10 Engine Anti Ice 75 1 25 OCT 2010 R66 Maintenance Manual Chapter 75 Engine Air Systems Page 75 i ...

Страница 614: ...Intentionally Blank Page 75 ii Chapter 75 Engine Air Systems R66 Maintenance Manual 25 OCT 2010 ...

Страница 615: ... Operating Handbook The engine anti ice system includes an air valve a solenoid valve and a pressure switch The air valve is mounted on top of the compressor scroll the solenoid valve and pressure switch are mounted on top of the compressor When anti ice is switched ON the solenoid valve de energizes the pressure activated air valve opens the pressure switch closes which illuminates the green anti...

Страница 616: ...Intentionally Blank Page 75 2 Chapter 75 Engine Air Systems R66 Maintenance Manual 25 OCT 2010 ...

Страница 617: ...TER 76 ENGINE CONTROLS Section Title Page 76 00 Description 76 1 76 10 Fuel Control Unit FCU 76 1 76 11 FCU Throttle Control Rigging 76 3 76 12 FCU Fuel Cutoff Control Rigging 76 3 76 20 Power Turbine Governor PTG 76 5 76 21 PTG Control Rigging 76 5 76 22 PTG Rigging Check 76 7 ...

Страница 618: ...Intentionally Blank Page 76 ii Chapter 76 Engine Controls R66 Maintenance Manual 25 OCT 2010 ...

Страница 619: ...eep switch up or down will change rotor RPM approximately one percent per two seconds The governor controls RPM under normal conditions It may not prevent over or under speed conditions generated by aggressive flight maneuvers or rapid power changes Other engine controls include a push pull fuel cutoff control on the console face a start button on the pilot s collective a key type igniter switch a...

Страница 620: ...Page 76 2 Chapter 76 Engine Controls JUL 2020 FIGURE 76 1 FUEL CONTROL UNIT ...

Страница 621: ... idle stop Verify sufficient inner wire beyond aft edge of fitting and special torque fitting nut per Section 20 33 8 Rotate twist grip open verify FCU throttle lever contacts maximum throttle stop and 0 030 0 050 inch gap between F328 1 connecting rod and throttle stop washer Reposition fitting on wire as required until proper rod to washer gap and FCU throttle lever contacts maximum throttle sto...

Страница 622: ...FIGURE 76 2 POWER TURBINE GOVERNOR Page 76 4 Chapter 76 Engine Controls R66 Maintenance Manual 25 OCT 2010 ...

Страница 623: ...ual OMM 2 Perform PTG control rigging per Section 76 21 76 21 PTG Control Rigging 1 Remove engine cowling assembly per Section 53 21 Detach center back rest assembly hook and loop tape Velcro at bottom slide back rest assembly up and out of keyhole slots Remove F474 2 middle seat cover see Section 6 70 2 Refer to Figure 76 2 Verify PTG input lever rigging angle is 93 0 7 5 As required remove hardw...

Страница 624: ...FIGURE 76 3 PTG BEEP ACTUATOR ASSEMBLY Page 76 6 Chapter 76 Engine Controls R66 Maintenance Manual 25 OCT 2010 ...

Страница 625: ...embly in keyhole slots and slide down press firmly on back rest assembly hook and loop tape at bottom Verify security 76 22 PTG Rigging Check 1 Turn BATTERY switch ON 2 Refer to Figure 76 2 With collective stick full down beep collective toggle switch to full down Verify PTG pointer indicates between 42 5 and 47 5 on PTG protractor Turn BATTERY switch OFF 3 Adjust PTG control rigging as required p...

Страница 626: ...Intentionally Blank Page 76 8 Chapter 76 Engine Controls R66 Maintenance Manual 25 OCT 2010 ...

Страница 627: ...eel Assemblies 79 3 79 11 Fanwheel to Inlet Gaps 79 3 79 20 Oil Tank Assembly 79 5 79 21 Oil Temperature Sender 79 6 79 22 Sight Gage 79 7 79 30 Engine Oil Cooler 79 7 79 40 Engine Oil Filter 79 7 79 50 Engine Oil Line Assemblies and Fittings 79 8 APR 2017 Chapter 79 Engine Oil System Page 79 i ...

Страница 628: ...Intentionally Blank Page 79 ii Chapter 79 Engine Oil System APR 2017 ...

Страница 629: ...to the engine accessory gearbox which is vented to the exhaust pipe The engine oil cooler has an internal thermostat thermostat initial closure 70 C full closure 81 C and pressure relief valve The thermostat maintains normal system operating pressure by allowing cool oil to bypass the heat exchanger and return to the oil tank Higher than normal system pressure will open a pressure relief valve Whe...

Страница 630: ...Page 79 2 Chapter 79 Engine Oil System APR 2019 FIGURE 79 2 SCROLL AND FANWHEEL ASSEMBLIES ...

Страница 631: ...assembly inside F236 1 scroll assembly accordingly Position F305 5 inlets on scroll and install hardware Verify security 2 Lower scroll with fanwheel inside through frame and install hardware securing scroll to F306 1 box assembly Verify security Seal gaps joints using A701 1 aluminum tape 3 Install F196 1 fan shaft per 65 10 79 11 Fanwheel to Inlet Gaps A Measuring Gap 1 Remove tailcone cowling a...

Страница 632: ...FIGURE 79 3 ENGINE OIL SYSTEM Page 79 4 Chapter 79 Engine Oil System APR 2017 ...

Страница 633: ...install hardware securing inlets to scroll assembly Verify security Install hardware securing fan shaft to plate assemblies standard torque hardware per 20 32 and torque stripe per Figure 5 1 7 Measure fanwheel to inlet gaps per Part A Repeat procedure as required for minimum 0 10 inch gap at forward and aft inlets 79 20 Oil Tank Assembly A Removal 1 Drain engine oil per 12 60 2 Remove tailcone co...

Страница 634: ... 9 Air conditioned ships Torque check nuts at firewall per 20 33 Remove caps and connect G794 2 G794 3 hose assemblies to G810 1 G811 1 line assemblies Using backup wrench special torque hose nuts per 20 33 Charge system per 12 81 10 Install tailcone cowling assembly per 53 23 79 21 Oil Temperature Sender A Removal 1 Drain engine oil per 12 60 2 Remove tailcone cowling assembly per 53 23 3 Refer t...

Страница 635: ...ox assembly 3 Support oil cooler without damaging oil cooler fins Disconnect F723 2 and F723 4 line assemblies from oil cooler and associated components cap fittings B Installation 1 Refer to Figure 79 3 Install hardware securing F649 1 oil cooler to F309 1 box assembly 2 Torque check associated oil cooler and engine unions per 20 33 3 Remove caps and connect F723 2 and F723 4 line assemblies to o...

Страница 636: ...gs Remove line B Installation 1 Refer to Figure 79 3 Torque check associated oil cooler and engine unions per 20 33 2 Remove caps and connect F723 line assembly to associated components Using backup wrench special torque line nuts per 20 33 3 Install hardware securing line assembly clamps Verify security 4 Torque stripe fittings per Figure 5 1 5 Service engine oil per 12 60 Page 79 8 Chapter 79 En...

Страница 637: ...nstallation 90 13 90 151 C831 12 13 14 GTN XXX Series GPS NAV COM Installation 90 13 90 152 G060 4 Garmin G500H Upper Console Assembly 90 13 90 155 F075 8 EFIS Installation 90 14 90 156 F817 9 Garmin G500H GDU 1060 Display R66 Police Installation 90 14 90 157 F818 11 G070 Console GTN 6XX series GPS NAV COM Installation 90 14 90 158 G070 7 8 Instrument High Upper Console Assembly 90 14 90 160 F079 ...

Страница 638: ...Intentionally Blank Page 90 ii Chapter 90 Police Version JUL 2020 ...

Страница 639: ...ations One configuration uses a modified cyclic control without a left side grip because the flat screen monitor would interfere The second configuration uses the standard cyclic control with a left side grip An additional circuit breaker panel on the ledge just forward of the pilot s seat contains all circuit breakers for police equipment Depending on installed police options the outboard section...

Страница 640: ...FIGURE 90 1 POLICE VERSION Page 90 2 Chapter 90 Police Version JUL 2020 ...

Страница 641: ... parked The infrared camera system consists of a gyro stabilized gimbal mounted infrared video camera in the chin and a power junction box in the main baggage compartment behind the interior wall The camera is operated by the observer in the left front seat via a handheld controller A tray and strap forward of the circuit breaker panel are provided for controller stowage when not in use A flat scr...

Страница 642: ...d on the aircraft belly near the left rear landing gear strut The PA system control panel is located in the avionics stack and allows the pilot or observer to select PA radio yelp or siren for broadcast through the speaker A multi band FM transceiver may be mounted either next to the LCD monitor or in the main avionics stack The FM transceiver band s are selectable from the audio control panel s T...

Страница 643: ...for cyclic control and grip assembly maintenance procedures A Schematic Refer to Figure 90 3 for C058 11 grip assembly wiring schematic 90 40 C430 2 Five Point Harness Installation Optional Refer to Figure 90 1 The C430 2 five point harness installation was optional equipment for earlier Police helicopters and now is optional for all R66 Turbines see 6 10 for version descriptions Refer to 25 10 fo...

Страница 644: ...0 Transceiver 1 Refer to Figure 90 1 Turn battery avionics switches off and pull out 7 5 amp circuit breaker at panel 2 Remove screws securing D413 2 cover to D413 1 box assembly 3 Disconnect D613 4 harness assembly from C813 2 transceiver 4 Release slotted turnlock fasteners securing transceiver to box assembly and remove transceiver C813 4 Technisonic TDFM 9000 Transceiver 1 Refer to Figure 90 1...

Страница 645: ...off and pull out 10 amp circuit breaker at panel 2 Position C813 4 transceiver in avionics tray and engage slotted turnlock fasteners Verify security 3 Push in 10 amp circuit breaker at panel Turn battery avionics switches on 4 Perform appropriate functional checks per Technisonic Industries Limited Installation and Operating Instructions supplied with unit Turn battery avionics switches off C813 ...

Страница 646: ...quired Perform ground checks per last two steps of Part D 90 70 C823 16 Audio Control Installation A Removal 1 Refer to Figure 90 1 Turn battery switch off Pull out associated circuit breaker 2 Release four slot head fasteners securing C823 16 audio control to radio tray and remove audio control B Installation 1 Refer to Figure 90 1 Turn battery switch off pull out associated circuit breaker 2 Pos...

Страница 647: ...and blower openings to prevent contamination 5 Remove hardware securing blower to D651 1 bracket and remove blower B Installation 1 Refer to Figure 90 1 Turn battery switch off pull out associated circuit breaker 2 Without pinching wiring position TB1 1 5D blower on D651 1 bracket and install hardware Verify security 3 Remove tape and push hose onto blower Verify security 4 Connect blower wiring t...

Страница 648: ...ted hardware 90 110 F014 5 Landing Gear Installation Refer to Figure 90 1 The F014 5 extended landing gear installation provides clearance for the F081 searchlight installation F239 5 and 6 forward struts extended gear are approximately 2 inches taller than F239 3 and 4 forward struts standard gear Refer to Chapter 32 for landing gear maintenance procedures and for extended gear minimum tail skid ...

Страница 649: ...ter Calculate weight and balance prior to flight with camera removed to assure aft CG limit is not exceeded 1 Refer to Figure 90 1 Turn battery switch off pull out associated circuit breaker 2 Position gimbal assembly s D349 3 plate between D349 1 supports and install fasters Standard torque nuts per Section 20 32 and torque stripe per Figure 5 1 Verify security 3 Connect cables to gimbal assembly...

Страница 650: ...trol unit to D428 16 brackets and G429 10 support and remove control unit F Electronics Control Unit Installation 1 Refer to Figure 90 1 Turn battery switch off pull out associated circuit breaker 2 Remove G428 1 wall assembly per 90 220 if not previously accomplished 3 Position 19206 2XX electronics control unit on G429 1 support assemblies Align control unit D428 16 brackets and G429 10 support ...

Страница 651: ...rmin GDU 620 display per 95 72 2 Remove C813 4 transceiver per 90 60 3 Remove perimeter screws securing instrument face to console 4 Disconnect instrument pitot static lines Plug lines 5 Remove screws securing console assembly to keel panels and hinge console aft B Securing Console 1 Hinge console assembly forward and install screws securing console to keel panels 2 Position instrument face in hel...

Страница 652: ...e 1 Remove C813 5 transceiver per 90 60 2 Remove GTN 650Xi GPS NAV COM per 97 15 3 Remove perimeter screws securing instrument face to console 4 Disconnect instrument pitot static lines Plug lines 5 Remove hardware securing console assembly to keel panels and lower console Disconnect airframe harnesses from console harnesses and remove console B Installing Upper Console 1 Connect airframe harnesse...

Страница 653: ... two bolts to 60 in lb install 0 032 inch diameter lockwire and safety bolts together Verify speaker security 3 Slide wire receptacles on speaker electrical turrets Slide nipples over connections 4 Install 0 032 inch diameter lockwire inside of cone and prepare safety Position speaker horn drilled hole on top on speaker and install and tighten cone Thread safety through hole and safety cone to bra...

Страница 654: ...tment door 4 Connect airframe wiring to amplifier at connectors Verify security Install aft left back rest per 25 22 CAUTION Hearing loss can result if personnel do not wear appropriate hearing protection when in close proximity to an operating PA Siren 5 Push in associated circuit breaker Turn battery switch on Wearing appropriate hearing protection perform appropriate post installation function ...

Страница 655: ...move nut washer searchlight and spacer washer B D432 1 or 3 Gimbal Assembly Installation 1 Refer to Figure 90 1 Turn battery switch off pull out associated circuit breaker 2 Install spacer washer shoulder facing up 024711 31 searchlight assembly flat washer and nut 3 Align the searchlight canister with the helicopter fore to aft axis Have a second person support the searchlight assembly and preven...

Страница 656: ...iscard ty raps as required securing XM DVR PRO converter output cable and input wiring to harness Disconnect output cable from UDVP PRO DVR Disconnect input wiring from harness at connectors 3 Remove F680 3 collective cover assembly Remove hardware securing converter to F370 1 panel and remove converter D Converter Installation 1 Refer to Figure 90 1 Turn battery switch off pull out associated cir...

Страница 657: ... from V R1041 RH monitor 3 Remove hardware securing MS21919WDG8 clamp to monitor 4 Support monitor Remove A483 1 knob with associated hardware and DK 225 knob with associated hardware securing monitor to D409 8 pivot assembly Remove monitor 5 Remove screws securing D763 3 visor assembly to monitor G416 4 Monitor Installation 1 Turn battery switch off and pull out MONITOR 2 amp circuit breaker at p...

Страница 658: ... at panel 2 Position DVI 10LDB_RH monitor on G417 1 pivot assembly and G417 4 tray assembly and install screws Verify security 3 Connect G458 harness assembly cables to monitor 4 Push in 2 amp circuit breaker at panel Turn battery avionics switches on Perform appropriate post installation function checks Turn battery avionics switches off G416 5 Monitor Installation 1 Turn battery switch off and p...

Страница 659: ...t and wing head fasteners securing G428 1 wall assembly to G238 1 bulkhead and G428 2 angles Carefully remove wall B Installation 1 Refer to Figure 90 1 Open baggage compartment door Verify no foreign objects aft of wall mounting points Verify proper installation and security of equipment 2 Align G428 1 wall assembly quarter turn slot and wing head fasteners with receptacles on G238 1 bulkhead and...

Страница 660: ... breaker 2 Remove G428 1 wall assembly per 90 220 3 Remove screws securing two cable backshells to 4107 0003 10 receiver Disconnect all cables from receiver 4 Remove screws securing receiver to G429 3 and G429 4 support assemblies and remove receiver D Receiver Installation 1 Refer to Figure 90 1 Turn battery switch off pull out associated circuit breaker 2 Remove G428 1 wall assembly per Section ...

Страница 661: ...fully plug in install Technisonic A711L series audio control in appropriate location in avionics tray 3 Tighten radio key securing audio control to tray Verify equipment security 4 Push in ICS 3 amp circuit breakers at panel Turn battery avionics switches on 5 Perform appropriate functional checks per Technisonic Industries Limited Installation and Operating Instructions Turn battery avionics swit...

Страница 662: ...ync3D Computer 1 Turn battery switch off and pull out VIEWSYNC 5 amp circuit breaker at panel 2 Remove G428 1 wall assembly per 90 220 3 Disconnect cables from Viewsync3D computer 4 Remove hardware securing computer to isolator mounting tray and remove computer UC 5300 6000 Computer 1 Turn battery switch off and pull out GPS MAP 5 amp circuit breaker at panel 2 Remove G428 1 wall assembly per 90 2...

Страница 663: ...lator mounting tray and install hardware Verify security 3 Connect cables to computer 4 Install G428 1 wall assembly per MM 90 220 5 Push in GPS MAP 5 amp circuit breakers at panel Turn battery avionics switches on 6 Perform appropriate functional checks per Aerocomputers Airborne Systems UC 5300 6000 Operating Instructions Turn battery avionics switches off IMU Sensor if installed 1 Turn battery ...

Страница 664: ...na to cabin and remove antenna Installation 1 Turn battery switch off and pull out GPS MAP 5 amp circuit breaker at panel 2 Position antenna on cabin and install hardware Verify security Connect antenna cable 3 Position G796 1 duct assembly on cabin and install hardware Verify security 4 Perform ground checks per Part D IMU Sensor steps 6 and 7 F Scheduled Maintenance and Inspections On condition ...

Страница 665: ...emove contents from G749 2 console assembly Latch tray 2 Remove screws securing console assembly to F377 1 support assembly and remove console B Installation 1 Refer to Figure 90 1 Unlatch G750 1 tray and remove contents from G749 2 console assembly Latch tray 2 Position console on F377 1 support assembly and install screws Verify security ...

Страница 666: ...Intentionally Blank Page 90 28 Chapter 90 Police Version JUL 2020 ...

Страница 667: ...90 280 Wiring Schematics JUL 2020 Chapter 90 Police Version Page 90 29 FIGURE 90 2 CO60 3 INTERIOR LIGHT INSTALLATION WIRING SCHEMATIC ...

Страница 668: ...Intentionally Blank Page 90 30 Chapter 90 Police Version JUL 2020 ...

Страница 669: ...90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 31 FIGURE 90 3 C058 11 GRIP ASSEMBLY WIRING SCHEMATIC ...

Страница 670: ...Intentionally Blank Page 90 32 Chapter 90 Police Version JUL 2020 ...

Страница 671: ...FIGURE 90 4 C813 2 TRANSCEIVER INSTALLATION WIRING SCHEMATIC 90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 33 ...

Страница 672: ...Intentionally Blank Page 90 34 Chapter 90 Police Version JUL 2020 ...

Страница 673: ...FIGURE 90 5 C813 4 TRANSCEIVER INSTALLATION WIRING SCHEMATIC 90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 35 ...

Страница 674: ...Intentionally Blank Page 90 36 Chapter 90 Police Version JUL 2020 ...

Страница 675: ...90 280 Wiring Schematics continued FIGURE 90 6 C813 5 TRANSCEIVER INSTALLATION WIRING SCHEMATIC JUL 2020 Chapter 90 Police Version Page 90 37 ...

Страница 676: ...Intentionally Blank Page 90 38 Chapter 90 Police Version JUL 2020 ...

Страница 677: ...JUL 2020 Chapter 90 Police Version Page 90 39 90 280 Wiring Schematics continued FIGURE 90 7 C823 16 AUDIO CONTROL INSTALLATION WIRING SCHEMATIC ...

Страница 678: ...Page 90 40 Chapter 90 Police Version JUL 2020 Intentionally Blank ...

Страница 679: ...90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 41 FIGURE 90 8 F051 1 CAMERA SYSTEM INSTALLATION WIRING SCHEMATIC ...

Страница 680: ...Intentionally Blank Page 90 42 Chapter 90 Police Version JUL 2020 ...

Страница 681: ...90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 43 FIGURE 90 9 F079 1 PA SIREN SYSTEM INSTALLATION WIRING SCHEMATIC ...

Страница 682: ...Intentionally Blank Page 90 44 Chapter 90 Police Version JUL 2020 ...

Страница 683: ...JUL 2020 Chapter 90 Police Version Page 90 45 90 280 Wiring Schematics continued FIGURE 90 10 F081 1 SEARCHLIGHT INSTALLATION WIRING SCHEMATIC ...

Страница 684: ...Page 90 46 Chapter 90 Police Version JUL 2020 90 280 Wiring Schematics continued FIGURE 90 11 F081 2 AND F081 3 SEARCHLIGHT INSTALLATION WIRING SCHEMATIC ...

Страница 685: ...90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 47 FIGURE 90 12 G415 1 AND G416 1 MONITOR INSTALLATION WIRING SCHEMATIC ...

Страница 686: ...Intentionally Blank Page 90 48 Chapter 90 Police Version JUL 2020 ...

Страница 687: ...90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 49 FIGURE 90 13 G415 1 AND G416 4 AND MONITOR INSTALLATION WIRING SCHEMATIC ...

Страница 688: ...Intentionally Blank Page 90 50 Chapter 90 Police Version JUL 2020 ...

Страница 689: ...90 280 Wiring Schematics continued JUL 2020 Chapter 90 Police Version Page 90 51 FIGURE 90 14 G416 5 MONITOR INSTALLATION WIRING SCHEMATIC ...

Страница 690: ...Intentionally Blank Page 90 52 Chapter 90 Police Version JUL 2020 ...

Страница 691: ...FIGURE 90 15 G437 1 LOJACK INSTALLATION WIRING SCHEMATIC JUL 2020 Chapter 90 Police Version Page 90 53 90 280 Wiring Schematics continued ...

Страница 692: ...Intentionally Blank Page 90 54 Chapter 90 Police Version JUL 2020 ...

Страница 693: ...JUL 2020 Chapter 90 Police Version Page 90 55 FIGURE 90 16 G445 AND G467 AUX ELECTRICAL AND CB WIRING INSTALLATION WIRING SCHEMATIC 90 280 Wiring Schematics continued ...

Страница 694: ...Intentionally Blank Page 90 56 Chapter 90 Police Version JUL 2020 ...

Страница 695: ...JUL 2020 Chapter 90 Police Version Page 90 57 90 280 Wiring Schematics continued FIGURE 90 17 C460 1 AND C460 2 AUDIO CONTROL INSTALLATION WIRING SCHEMATIC ...

Страница 696: ...Page 90 58 Chapter 90 Police Version JUL 2020 90 280 Wiring Schematics continued FIGURE 90 18 G608 GPS MAPPING AND MDT INSTALLATION WIRING SCHEMATIC ...

Страница 697: ...92 90 F075 1 EFIS Installation 92 12 92 100 F082 21 Fairing Installation 92 12 92 110 F461 4 Cover Assembly 92 12 92 120 G197 13 Window 92 12 92 130 G425 1 Wall Installation 92 13 92 140 G445 2 Aux Circuit Breaker Panel Installation 92 13 92 150 G448 Aft Monitors Installation 92 14 92 151 G448 1 10 inch Monitor 92 15 92 152 G448 1 Five inch Left Hand Monitor 92 16 92 153 G448 2 Five inch Right Han...

Страница 698: ...ion 92 38 92 230 G490 1 Talent Light Installation 92 39 92 231 D553 1 Forward Talent Light Assembly 92 39 92 232 ILED MA Aft Talent Light 92 40 92 240 G491 TV Receiver Provision Installation 92 40 92 241 Distribution Amp 92 41 92 242 Digital TV Receiver 92 42 92 250 G492 1 Audio System Installation 92 43 92 251 Forward Audio Panels 92 44 92 252 Aft Console Audio Panels 92 45 92 253 Digital Router ...

Страница 699: ...dio controller are located on each side of the instrument console A ten inch monitor is mounted on an arm assembly in front of the left aft passenger and controls are located in the equipment console Each monitor allows for independent monitoring and transmitting of video from cameras R66 ENG is equipped with a microwave system which provides live broadcasting capability Other features include a v...

Страница 700: ...Page 92 2 Chapter 92 ENG Version JUL 2020 FIGURE 92 1 ENG VERSION ...

Страница 701: ...reaker at panel 2 Connect G459 harness assembly to A824 18 transceiver and verify security Install transceiver in upper console radio tray 3 Tighten radio key securing transceiver to tray Verify equipment security 4 Push in FM1 10 amp circuit breaker at panel Turn battery avionics switches on 5 Perform appropriate functional checks per Kenwood TK 7180 TK 8180 FM Transceiver Instruction Manual Turn...

Страница 702: ...s 92 40 C720 1 Support Installation A Removal Refer to Figure 92 1 Remove hardware securing C719 1 support to C242 skid tube and remove support B Installation Install hardware securing C719 1 support to C242 skid tube special torque bolt per 20 33 and torque stripe per Figure 5 1 92 50 HD Micro Camera Installations A Description The micro camera system consists of three small cameras and their con...

Страница 703: ...ndshield bow Verify security 4 Connect CV505 345 10FTCBLE cable and G459 2798 wire to camera at connectors Verify security 5 Push in MICRO CAMS circuit breaker 2 amp at panel Turn battery news equipment switches on 6 Perform appropriate functional checks per Marshall Electronics CV345 Operation Manual Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspect...

Страница 704: ...y 3 Connect CV505 345 10FTCBLE cable and G459 756 wire to camera at connectors Verify security 4 Install ILED MA aft talent light per 92 232 5 Push in MICRO CAMS circuit breaker 2 amp at panel Turn battery news equipment switches on 6 Perform appropriate functional checks per Marshall Electronics CV345 Operation Manual Turn battery news equipment switches off C Special Inspections 1 Refer to Figur...

Страница 705: ...Intentionally Blank JUL 2020 Chapter 92 ENG Version Page 92 7 ...

Страница 706: ... connectors disconnect CV200 M MB camera cable from C023 wires at connectors 3 Supporting camera remove screws securing D368 11 clamp to stabilizer and remove camera and clamp Carefully remove grommet from outboard side of stabilizer and pull camera cable through hole in stabilizer Remove grommet and clamp B Installation 1 Refer to Figure 92 1 Turn battery news equipment switches off and pull out ...

Страница 707: ...el Turn battery news equipment switches on 6 Perform appropriate functional checks per Marshall Electronics CV200 M MB Operation Manual Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect CV200 M MB micro camera for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps 5 and 6 D Special Inspe...

Страница 708: ...stall screws securing support to G472 face Verify security 4 Install screws securing face to G471 panels Verify security 5 Push in MICRO CAMS circuit breaker 2 amp at panel Turn battery news equipment switches on 6 Perform appropriate functional checks per Marshall Electronics CV200 MB M or CV345 CS CSB Operation Manual Turn battery news equipment switches off C Scheduled Inspections Every 100 hou...

Страница 709: ...d forward on the landing gear skids For ground handling using MT950 towcart install wheels at forward supports and use cart at aft cross tube as indicated on cart instructions online at www robinsonheli com For ground handling without towcart wheels may be installed at all four support locations B Maintenance Procedures Refer to Chapter 32 for landing gear assembly maintenance procedures identical...

Страница 710: ...s F082 21 fairing installation replaces F082 1 fairing installation B Maintenance Procedures Refer to 32 40 fairing assemblies for maintenance procedures 92 110 F461 4 Cover Assembly Refer to Figure 92 1 Refer to R66 Illustrated Parts Catalog Chapter 6 for access and inspection panel locations F461 4 cover assembly replaces F461 1 cover assembly 92 120 G197 13 Window A Description Refer to Figure ...

Страница 711: ...uipment has a dedicated circuit breaker panel with a second news master switch allowing the pilot to easily remove power for the majority of ENG equipment simultaneously B Schematic Refer to Figure 92 5 for G445 2 aux circuit breaker panel installation wiring diagram C Access 1 Turn battery news equipment switches off 2 Remove screws securing G445 2 aux circuit breaker panel to ledge Carefully lif...

Страница 712: ...apped around the seat back cross tube to hold the monitor in the operating position Detaching the tether will cause the monitor to return to the stowed position Verify monitor locks in position after detaching tether NOTE Monitor must be stowed below 500 ft AGL If not stowed the monitor is a potential source of head injury in an accident The main rear LCD monitor may be switched between three inpu...

Страница 713: ...ty 4 Push in 10 MON 2 amp circuit breaker at panel Turn battery news equipment switches on 5 Perform appropriate functional checks per Transvideo operator s guide Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect HD10CINEROB monitor for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps ...

Страница 714: ... MONS 2 amp circuit breaker at panel Turn battery news equipment switches on 5 Perform appropriate functional checks per TVLogic VRM 056W Operation Manual Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect VFM 056W monitor for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps 4 and 5 D S...

Страница 715: ...ecurity 4 Push in 5 MONS 2 amp circuit breaker at panel Turn battery news equipment switches on 5 Perform appropriate functional checks per TVLogic VRM 056W Operation Manual Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect VFM 056W monitor for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part ...

Страница 716: ...and pull out 7 MON 2 amp circuit breaker at panel 2 Install screws securing BVB07 monitor s to G474 bracket assembly Verify security 3 Connect G459 harness assembly to monitor verify security 4 Push in 7 MON 2 amp circuit breaker at panel Turn battery news equipment switches on 5 Perform appropriate functional checks per Boland Communications BVB07 User Manual Turn battery news equipment switches ...

Страница 717: ... CAMERA 10 amp circuit breaker at panel 2 Remove screws securing G427 fairings to chin and remove fairings 3 Disconnect E195 2 and E204 6 cable assemblies from E801 1 gimbal assembly 4 Have a second person support gimbal assembly Remove screws securing D374 3 spacer and gimbal assembly to D385 4 mount assembly and remove spacer and gimbal 5 Configure helicopter for flight with gimbal assembly remo...

Страница 718: ...ed positions via Pan Tilt knobs 3 Roll Mode Switch Momentary Toggle Changes modes by moving switch in direction of desired mode Mode selected is illuminated A mode Inertial Mode Gimbal Roll is controlled via joystick rotational motions about Z axis and ROLL TRIM knob B mode Position Mode Gimbal position is controlled via ROLL POSITION knob 4 Panel Lights Dimmer Knob Adjust the illumination level o...

Страница 719: ...ystick moves CW Roll Axis moves CW 13 DIG EXT Switch Two position toggle Controls the digital zoom function Feature not active in some cameras 2x Activate digital zoom 1x Deactivate digital zoom 14 Zoom Rate Knob Controls magnitude of the zoom rocker switch CCW Decrease zoom rocker response CW Increase zoom rocker response 15 Joystick Polarity Knob Four position Controls polarity of joystick comma...

Страница 720: ...nction in the monitor Only available in some models Corresponding LED light on switch test box WA5 should light up when activated 20 Zoom Rocker Switch Controls Camera Zoom T Zoom in W Zoom Wide 21 Ikegami RM 11 Camera Controller Test the following items Mode BARS Display color bar on screen CAL Display gray scale Gain up toggle image appears brighter in each incremental toggle down toggle image a...

Страница 721: ...shade color 28 Remote Video Switcher Toggle Momentary toggle Switches output of main video switcher between Gimbal camera and Micro camera Corresponding LED light on switch test box WA5 should light up when activated 29 VTR Start Stop Toggle Two position toggle Toggle to start and stop recording of the video recorder Operates on selected video recorders only Corresponding LED light on switch test ...

Страница 722: ...mbly connectors to prevent moisture or debris from contacting connector sockets pins secure with ty raps Stow and secure cables with ty raps to surrounding structure Verify security c Verify cable assembly clearance to tail rotor pedal controls thru full range of travel d Install screws securing D050 13 cover to chin Verify security e Revise Weight and Balance Record in R66 Pilot s Operating Handb...

Страница 723: ...nel Turn battery news equipment switches on 4 Perform appropriate function checks per 92 171 Part C C Scheduled Inspections Every 100 hour or annual inspection inspect E002 2 laptop assembly for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps 3 and 4 D Special Inspections 1 Refer to Figure 92 1 Turn battery news equipment switches off Open ci...

Страница 724: ...y security 4 Connect G459 harness assembly and E195 2 E199 3 and E204 6 cable assemblies to aux box Verify security 5 Install baggage compartment wall per 92 130 6 Push in GIMBAL CAMERA 10 amp circuit breaker at panel Turn battery news equipment switches on 7 Perform appropriate function checks per 92 171 Part C C Scheduled Inspections Every 100 hour or annual inspection inspect E003 7 aux box ass...

Страница 725: ...es stowed Refer to 92 184 Part E for maintenance procedures B Schematic Refer to Figure 92 9 for G456 1 microwave system installation wiring diagram 92 181 D588 5 Controller Assembly A Removal 1 Refer to Figure 92 1 Turn battery news equipment switches off and pull out MWAVE XMIT 5 amp circuit breaker at panel 2 Disconnect G459 harness assembly from D588 5 controller assembly 3 Remove screws secur...

Страница 726: ...ections 1 Refer to Figure 92 1 Turn battery news equipment switches off Open circuit breaker panel 2 As required remove D588 5 controller assembly per Part A Inspect condition of and verify no obvious damage to controller circuit breaker and wiring Verify no loose chafed or broken wires or terminals Verify no evidence of arcing Verify equipment security 3 Secure circuit breaker panel Install contr...

Страница 727: ...MIT 5 amp circuit breaker at panel Turn battery news equipment switches on 5 Perform appropriate post installation function checks Turn battery switch off C Scheduled Inspections Every 100 hour or annual inspection inspect ARC CM TX RX CR 01 controller for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps 4 and 5 D Special Inspections 1 Refer t...

Страница 728: ... securing N 4 BK clamps to angles Verify security 5 Connect G459 harness assembly to transmitter Verify security 6 Install baggage compartment wall per 92 130 7 Push in MWAVE XMIT 5 amp circuit breaker at panel Turn battery news equipment switches on 8 Perform appropriate post installation function checks Turn battery switch off C Scheduled Inspections Every 100 hour or annual inspection inspect C...

Страница 729: ...s Verify security 4 Have a second person support pod antenna Install screws and washers securing pod antenna to D586 brackets Verify security 5 Connect G459 harness assembly to pod antenna and amp assembly Verify security 6 Push in MWAVE XMIT 5 amp circuit breaker at panel Turn battery news equipment switches on 7 Perform appropriate post installation function checks Turn battery switch off C Sche...

Страница 730: ...e Record in R66 Pilot s Operating Handbook POH Section 6 to incorporate the following data Subtract Weight Long Arm Long Moment Lat Arm Lat Moment 18 1 lb 80 7 in 1460 7 in lb 0 in 0 in lb 2 Configuration for Flight with Pod Antenna Installed a Remove and discard ty raps and plastic bags securing cable assemblies together and ty raps and bags protecting connectors b Install hardware securing D586 ...

Страница 731: ...Intentionally Blank JUL 2020 Chapter 92 ENG Version Page 92 31B ...

Страница 732: ...switches on 5 Perform appropriate post installation function checks Turn battery switch off C Scheduled Inspections Every 100 hour or annual inspection inspect GPS 1270FW antenna for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps 4 and 5 D Special Inspections 1 Refer to Figure 92 1 Turn battery news equipment switches off Open circuit breake...

Страница 733: ...it breaker at panel 2 Remove paint primer from between cabin skin and B322 12 plate and between cabin skin and CI 105 16 transponder antenna to ensure electrical ground 3 Install hardware securing B322 12 doubler and transponder antenna to mounting plate to aft cowling Verify security 4 Apply small bead of B270 1 sealant 0 1 inch max in height around antenna exterior only where it attaches to aft ...

Страница 734: ... plastic scraper remove B270 1 sealant from around CI 273 TV tuner antenna where it attaches to cabin skin 3 Remove screws securing B322 11 plate to cabin skin and remove plate with antenna attached Disconnect antenna cable from antenna at connectors 4 Disassemble antenna from plate as required C Installation 1 Refer to Figure 92 1 Turn battery news equipment switches off and pull out TV TUNER 2 a...

Страница 735: ...t A if removed 92 193 G457 3 Antenna Installation Scanner A Schematic Refer to Figure 92 11 for G489 scanner installation wiring diagram B Removal 1 Refer to Figure 92 1 Turn battery news equipment switches off and pull out SCANNER 2 amp circuit breaker at panel 2 Remove G13000 audio system router per 92 253 3 Disconnect antenna cable from CI 285 antenna at connectors 4 Supporting antenna and B322...

Страница 736: ... per Part A Inspect condition of and verify no obvious damage to antenna circuit breaker and wiring Verify no loose chafed or broken wires or terminals Verify no evidence of arcing Verify equipment security 3 Secure circuit breaker panel Install antenna per Part A if removed 92 200 G470 1 Aft Console Installation The G470 1 aft console installation is a sheet metal console installed in place of th...

Страница 737: ...arness assembly to transceiver s 5 Push in FM2 10 amp and FM3 10 amp circuit breakers at panel Turn battery news equipment switches on 6 Perform appropriate functional checks per Kenwood TK 7180 TK 8180 VHF FM UHF FM Transceiver Instruction Manual Turn battery new equipment switches off E Scheduled Inspections Every 100 hour or annual inspection inspect A824 transceiver s for proper installation r...

Страница 738: ...lies to face and scanner Verify security 3 Connect G459 harness assembly to scanner Verify security 4 Install screws securing G472 face to G471 panels 5 Push in SCANNER 2 amp circuit breaker at panel Turn battery news equipment switches on 6 Perform appropriate functional checks per Uniden Scanners User s Guide Turn battery new equipment switches off E Scheduled Inspections Every 100 hour or annua...

Страница 739: ... wiring diagram 92 231 D553 1 Forward Talent Light Assembly A Lamp Replacement 1 Refer to Figure 92 1 Turn battery news equipment switches off and pull out TALENT LTS 3 amp circuit breaker at panel 2 Supporting D553 1 light assembly remove hardware securing light assembly to D566 10 bracket 3 Holding light assembly vertically unscrew D553 3 housing from D566 9 cap and remove housing and D566 5 len...

Страница 740: ...securing light to stud Verify security 3 Plug in mini USB cable to light 4 Push in TALENT LTS 3 amp circuit breaker at panel Turn battery news equipment switches on Verify talent light switches on and off using switch C Scheduled Inspections Every 100 hour or annual inspection inspect ILED MA light for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part ...

Страница 741: ...TV TUNER 2 amp circuit breaker at panel Turn battery news equipment switches on 6 Perform appropriate functional checks per TV receiver manufacturer s instructions manufacturer s may vary due to regional requirements Turn battery new equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect 11 911 102 distribution amp s for proper installation refer to R66 Illustra...

Страница 742: ...ker at panel Turn battery news equipment switches on 6 Perform appropriate functional checks per TV receiver manufacturer s instructions manufacturer s may vary due to regional requirements Turn battery new equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect CTDVBT 288X digital TV receiver s for proper installation refer to R66 Illustrated Parts Catalog Chapt...

Страница 743: ...igger switch is the intercom key The second detent transmits on the 1 VHF communications radio regardless of audio panel configuration The audio panel transmit thumb button transmits on the panel selected audio component A toggle switch to the left of the pilot s audio panel may be used to bypass the audio system and connect the pilot directly to Com 1 This mode is automatically engaged in the eve...

Страница 744: ...ush in 7 MONS 2 amp and AUDIO PANEL 5 amp circuit breakers at panel 6 Perform appropriate functional checks per Geneva Aviation user guide Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect G11431 00102 1 audio panel s for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps 5 and 6 D Speci...

Страница 745: ...udio panel s Verify security 4 Position audio panel s in console and install face screws securing audio panel s to D344 4 angle assemblies Verify security 5 Push in AUDIO PANEL 5 amp circuit breaker at panel 6 Perform appropriate functional checks per Geneva Aviation user guide Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect G11431 00102...

Страница 746: ...sembly to router Verify security 4 Push in AUDIO PANEL 5 amp circuit breaker at panel 5 Perform appropriate functional checks per Geneva Aviation user guide Turn battery news equipment switches off C Scheduled Inspections Every 100 hour or annual inspection inspect G13000 router for proper installation refer to R66 Illustrated Parts Catalog Chapter 92 proper operation per Part B steps 4 and 5 D Sp...

Страница 747: ...mponent s disconnect G459 harness assembly from video router or video switch as required and remove component D Installation 1 Refer to Figure 92 1 Turn battery news equipment switches off and pull out VID SW 2 amp circuit breaker at panel 2 Connect G459 harness assembly to BENXT430X video router or RH AB video switch as required 3 Install screws securing video router or video switch to G470 1 con...

Страница 748: ... in monitor and controls B Schematic Refer to Figure 92 16 for G496 1 DVR installation wiring diagram C Removal 1 Refer to Figure 92 1 Turn battery news equipment switches off and pull out DVR 2 amp circuit breaker at panel 2 Disconnect G459 harness assembly from ODYSSEY7Q or ODYSSEY7QPLUS monitor recorder 3 Supporting monitor recorder remove hardware securing monitor recorder to G474 3 bar and re...

Страница 749: ...anel Install monitor recorder per Part A if removed 92 280 Aux Electrical System Installation An additional circuit breaker panel on the ledge just forward of the pilot s seat contains all circuit breakers for ENG equipment The forward row of circuit breakers is a 28 volt bus and the aft row is a 14 volt bus A 28 to 14 volt converter powers the 14 volt bus The news equipment master switch on the l...

Страница 750: ...Intentionally Blank Page 92 50 Chapter 92 ENG Version JUL 2020 ...

Страница 751: ...92 290 Wiring Diagrams FIGURE 92 3 A826 18 TRANSCEIVER INSTALLATION FM1 WIRING DIAGRAM JUL 2020 Chapter 92 ENG Version Page 92 51 ...

Страница 752: ...92 290 Wiring Diagrams continued FIGURE 92 4 D097 HD MICRO CAMERA INSTALLATION WIRING DIAGRAM Page 92 52 Chapter 92 ENG Version JUL 2020 ...

Страница 753: ...92 290 Wiring Diagrams continued FIGURE 92 5 G445 2 AUX CIRCUIT BREAKER PANEL INSTALLATION WIRING DIAGRAM JUL 2020 Chapter 92 ENG Version Page 92 53 ...

Страница 754: ...92 290 Wiring Diagrams continued FIGURE 92 6 G448 AFT MONITORS INSTALLATION WIRING DIAGRAM Page 92 54 Chapter 92 ENG Version JUL 2020 ...

Страница 755: ...92 290 Wiring Diagrams continued FIGURE 92 7 G449 FORWARD MONITORS INSTALLATION WIRING DIAGRAM JUL 2020 Chapter 92 ENG Version Page 92 55 ...

Страница 756: ...Intentionally Blank Page 92 56 Chapter 92 ENG Version JUL 2020 ...

Страница 757: ...JUL 2020 Chapter 92 ENG Version Page 92 57 FIGURE 92 8 G454 1 CAMERA SYSTEM INSTALLATION WIRING DIAGRAM 92 280 Wiring Diagrams continued ...

Страница 758: ...Intentionally Blank Page 92 58 Chapter 92 ENG Version JUL 2020 ...

Страница 759: ...92 290 Wiring Diagrams continued FIGURE 92 9 G456 1 MICROWAVE SYSTEM INSTALLATION WIRING DIAGRAM JUL 2020 Chapter 92 ENG Version Page 92 59 ...

Страница 760: ...92 290 Wiring Diagrams continued FIGURE 92 10 G487 1 FM TRANSCEIVERS INSTALLATION WIRING DIAGRAM Page 92 60 Chapter 92 ENG Version JUL 2020 ...

Страница 761: ...92 290 Wiring Diagrams continued FIGURE 92 11 G489 SCANNER INSTALLATION WIRING DIAGRAM JUL 2020 Chapter 92 ENG Version Page 92 61 ...

Страница 762: ...92 290 Wiring Diagrams continued FIGURE 92 12 G490 1 TALENT LIGHT INSTALLATION WIRING DIAGRAM Page 92 62 Chapter 92 ENG Version JUL 2020 ...

Страница 763: ...92 290 Wiring Diagrams continued FIGURE 92 13 G491 TV RECEIVER PROVISION INSTALLATION WIRING DIAGRAM JUL 2020 Chapter 92 ENG Version Page 92 63 ...

Страница 764: ...Intentionally Blank Page 92 64 Chapter 92 ENG Version JUL 2020 ...

Страница 765: ...JUL 2020 Chapter 92 ENG Version Page 92 65 92 280 Wiring Diagrams continued FIGURE 92 14 G492 1 AUDIO SYSTEM INSTALLATION WIRING DIAGRAM ...

Страница 766: ...Intentionally Blank Page 92 66 Chapter 92 ENG Version JUL 2020 ...

Страница 767: ...92 290 Wiring Diagrams continued FIGURE 92 15 G493 1 VIDEO COMPONENTS INSTALLATION WIRING DIAGRAM JUL 2020 Chapter 92 ENG Version Page 92 67 ...

Страница 768: ...92 290 Wiring Diagrams continued FIGURE 92 16 G496 1 DVR INSTALLATION WIRING DIAGRAM Page 92 68 Chapter 92 ENG Version JUL 2020 ...

Страница 769: ...5 31 N1 Tachometer 95 14 95 32 Measured Gas Turbine Temperature MGT Gage 95 15 95 33 Engine Oil Pressure Gage 95 16 95 34 Engine Oil Temperature Gage 95 16 95 35 Fuel Quantity Gage 95 17 95 40 Additional Standard Indicating Equipment 95 18 95 41 Clock 95 18 95 42 Ammeter 95 19 95 43 Outside Air Temperature OAT Gage Voltmeter 95 20 95 44 Hourmeters 95 21 95 50 Console Assemblies 95 22 95 60 Instrum...

Страница 770: ...Intentionally Blank Page 95 ii Chapter 95 Instrument System JUL 2020 ...

Страница 771: ...n service For instrument panels with electronic flight displays a P N D327 light filter may be used to reduce reflections in the windshield at night The light filter is installed by clipping it to the front of the display Filter use is at pilot discretion The pitot static system supplies air pressure to operate the airspeed indicator altimeter and vertical speed indicator The pitot tube is located...

Страница 772: ...FIGURE 95 1 PITOT STATIC SYSTEM INSTALLATION Page 95 2 Chapter 95 Instrument System APR 2017 ...

Страница 773: ...ak s Retest after any repairs 6 Remove tape from pitot tube drain hole and verify airspeed indicator has returned to zero 7 Remove test equipment B Static System Leak Test CAUTION Airspeed indicator altimeter and vertical speed indicator may be damaged if suction to static line is applied or removed rapidly 1 Refer to Figures 95 1 and 95 2 Set altimeter to location elevation 2 Temporarily seal lef...

Страница 774: ...Page 95 4 Chapter 95 Instrument System APR 2017 FIGURE 95 2 PITOT STATIC SYSTEM INSTALLATION ...

Страница 775: ... pitot static system schematic C Removal CAUTION Protect instrumentation using foam padding or equivalent Handle instruments like eggs 1 Turn battery switch off and pull out applicable circuit breaker s 2 Remove perimeter screws securing face to console and pull face aft 3 Remove screws securing instrument to face 4 Disconnect wiring as applicable 5 Disconnect pitot static lines and cap plug instr...

Страница 776: ...Perform appropriate function checks per 5 40 E Scheduled Maintenance and Inspections Refer to 5 45 100 Hour Annual Inspection F Special Maintenance and Inspections 1 If vertical speed indicator displays climb indication but does not return to zero in level flight or if indication is erratic a Inspect static system for water or obstructions and remove water or obstructions if found b Perform pitot ...

Страница 777: ...pper console and inspect pitot line for kinks or bends d Perform pitot static system checks as required per 95 10 e Perform appropriate function checks per 5 40 If indicator still displays no indication remove indicator per Part C and return to RHC for inspection f Install airworthy indicator per Part D 2 If airspeed indicator displays erratic indication a Inspect pitot static system connection s ...

Страница 778: ... circuit whenever the rotors are turning even if the avionics bus is not powered The bypass circuit is disconnected from the tachometer bus when the annunciator test button is depressed Pressing the test button while the helicopter is running will confirm that the tachometers are receiving power from the avionics bus NOTE Do not use magnetized tools CAUTION Protect instrumentation using foam paddi...

Страница 779: ... N2 2 amp and R 2 amp circuit breakers on circuit breaker panel Turn battery switch on open throttle and beep actuator to minimum RPM setting Close throttle and turn battery switch off 4 a Start engine and run up helicopter per R66 Pilot s Operating Handbook POH Section 4 establish stable idle and record dual tachometer s N2 indication Also record RPM displayed on balancer b Multiply dual tachomet...

Страница 780: ...ng instrument face perimeter screws and pulling face aft 8 Shut down helicopter per R66 POH Section 4 9 Install perimeter screws securing face to console Verify security E Scheduled Maintenance and Inspections Refer to 5 45 100 Hour Annual Inspection Refer to 4 22 for recommended replacement time between overhauls F Special Maintenance and Inspections 1 Perform accuracy check and needle synchroniz...

Страница 781: ...cial Maintenance and Inspections 1 If altimeter displays no indication a Inspect static lines for obstructions and remove obstructions if found b Perform pitot static system checks as required per 95 10 c Perform appropriate function checks per 5 40 If altimeter still displays no indication remove altimeter per Part C and return to RHC for inspection d Install airworthy altimeter per Part D 2 If a...

Страница 782: ...spect wiring for loose chafed frayed or broken wires Verify no damaged connectors Verify wiring neatness proper routing and installation and security 2 Perform appropriate function checks per 5 40 If accuracy of torquemeter is suspected remove torquemeter per Part C and check calibration per Figure 95 3A 3 Install airworthy torquemeter per Part D Page 95 12 Chapter 95 Instrument System APR 2017 FI...

Страница 783: ... to B339 2 mount Verify security 3 Install hardware securing mount to windshield bow Verify security 4 Using the airport compass rose align the helicopter skids on the rose lines and record the indicated compass headings at 30 increments Adjust compass compensator magnets as required until the maximum error at any heading is 5 or less with all avionics operating all exterior lights on and dimmer f...

Страница 784: ...nd disconnect wiring 4 Remove screws securing instrument cluster to G051 shell assembly s face plate and remove instrument cluster D Installation 1 Turn battery switch off and pull out applicable circuit breaker s 2 Remove screws securing upper console to lower console and tilt upper console aft 3 Position G144 6 instrument cluster on G051 shell assembly s face plate and install screws Verify secu...

Страница 785: ... per Part D 95 32 Measured Gas Turbine Temperature MGT Gage A Description The measured gas temperature MGT gage connects to the engine s thermocouple harness via different size connectors to ensure correct polarity Refer to RR300 Series Operation and Maintenance Manual OMM for periodic calibration requirements B Schematic Refer to Figure 98 1 for electrical schematic C Removal Remove G144 6 instru...

Страница 786: ...nce and Inspections Perform special maintenance and inspections per 95 31 Part F 95 34 Engine Oil Temperature Gage A Description The engine oil temperature gage is electronic The oil temperature sensor is a transducer mounted on the inboard wall of the oil tank B Schematic Refer to Figure 98 1 for electrical schematic C Removal Remove G144 6 instrument cluster per 95 31 Part C D Installation Insta...

Страница 787: ...gure 98 1 for electrical schematic C Removal Remove G144 6 instrument cluster per 95 31 Part C D Installation Install G144 6 instrument cluster per 95 31 Part D E Scheduled Maintenance and Inspections Refer to 5 45 100 Hour Annual Inspection F Special Maintenance and Inspections Perform special maintenance and inspections per 95 31 Part F APR 2017 Chapter 95 Instrument System Page 95 17 ...

Страница 788: ...nnectors Verify security 2 Install screws securing clock to face Verify security 3 Install perimeter screws securing face to console and verify security or tilt console forward and install screws securing upper console to lower console and verify security as required E Scheduled Maintenance and Inspections Refer to 5 45 100 Hour Annual Inspection F Special Maintenance and Inspections 1 Check AGC 3...

Страница 789: ...stallation 1 Connect console wiring to ammeter wiring at connectors Verify security 2 Install screws securing ammeter to face Verify security 3 Install perimeter screws securing face to console and verify security or tilt console forward and install screws securing upper console to lower console and verify security as required E Scheduled Maintenance and Inspections Refer to 5 45 100 Hour Annual I...

Страница 790: ...g at connectors and remove gage D Installation 1 Connect console wiring to OAT gage wiring at connectors Verify security 2 Install screws securing OAT gage to face Verify security 3 Install perimeter screws securing face to console and verify security or tilt console forward and install screws securing upper console to lower console and verify security as required E Scheduled Maintenance and Inspe...

Страница 791: ...face to lower console and supporting hourmeter remove face 2 Disconnect airframe wiring from hourmeter and remove hourmeter D Installation Collective Activated Hourmeter 1 Connect airframe wiring to hourmeter wiring at connectors Verify security 2 Install screws securing hourmeter faceplate and carpet to F353 2 panel Verify security Console Hourmeter 1 Connect airframe wiring to hourmeter F859 205...

Страница 792: ...n upper instrument console not required if control panel is located at top of avionics stack 4 Remove perimeter screws securing instrument face to console 5 Disconnect instrument pitot static lines Plug lines 6 Remove screws securing console assembly to forward keel panels and lower panel Remove console and disconnect console harness from airframe harness C Installing Console 1 Connect console ass...

Страница 793: ...Intentionally Blank APR 2019 Chapter 95 Instrument System Page 95 23 ...

Страница 794: ...Page 95 24 Chapter 95 Instrument System APR 2019 FIGURE 95 4 GARMIN G500H UPPER CONSOLE WITH GDU 1060 FIGURE 95 5 GARMIN G500H UPPER CONSOLE PITOT STATIC SCHEMATIC ...

Страница 795: ...for GDU 1060 installation electrical schematic Refer to Figures 95 3 95 5 for Garmin G500H upper console pitot static schematic C Removal 1 Turn battery avionics switches off and pull out EFIS circuit breaker 5 amp on circuit breaker panel 2 Remove screws securing GDU to console face 3 Pull out and support display unplug console harness connectors and remove display D Installation 1 Turn battery a...

Страница 796: ...ns for Continued Airworthiness NOTE All factory installed Garmin units are on condition and do not require scheduled periodic maintenance Units feature a BIT Built In Test function during each initial power up that will detect internal failure s and alert pilot NOTE Refer to 97 60 for avionics software information FIGURE 95 6 GARMIN G500H UPPER CONSOLE WITH GDU 620 ...

Страница 797: ...nuedAirworthiness A Description The GDU 620 integrates with the Garmin G500H Electronic Flight Instrument System EFIS The GDU 620 electronically displays primary flight instrumentation via a primary flight display PFD and moving map weather traffic terrain and other functionality via a multifunction display MFD on dual 6 5 inch displays Refer to 97 10 for Garmin G500H EFIS system components B Sche...

Страница 798: ...FIGURE 95 8 EIGHT INSTRUMENT CONSOLE WITH ASPEN PFD PITOT STATIC SCHEMATIC FIGURE 95 7 EIGHT INSTRUMENT CONSOLE WITH ASPEN PFD Page 95 28 Chapter 95 Instrument System APR 2019 ...

Страница 799: ... display to a Horizontal Situation Indicator HSI Primary GPS position data is provided by GTN series GPS Heading and outside air temperature data is received from the Aspen remote sensor module RSM The RSM provides backup GPS position data if primary GPS fails The Aspen MFD Multifunction Display is an LCD unit with displays for moving map navigation data terrain and traffic Terrain and traffic may...

Страница 800: ...FIGURE 95 11 EIGHT INSTRUMENT CONSOLE WITH ASPEN PFD AND MFD PITOT STATIC SCHEMATIC FIGURE 95 10 EIGHT INSTRUMENT CONSOLE WITH ASPEN PFD AND MFD Page 95 30 Chapter 95 Instrument System APR 2019 ...

Страница 801: ...ngs at display and in aircraft to prevent contamination 4 Loosen screws securing airframe wiring harness connector s to display s unplug connector s and remove display s D Installation 1 Turn battery switch off and pull out EFIS circuit breaker 7 5 amp on circuit breaker panel 2 Plug airframe wiring harness connector s into Aspen PFD MFD display s and tighten screws Verify security 3 PFD only Remo...

Страница 802: ...e to tailcone Verify security 4 Apply small bead B270 1 sealant 0 1 inch max in height around antenna at corners where it attaches to tailcone and allow to dry 5 Connect antenna cable at connectors secure to frame using ty raps Verify security 6 Perform ground checks per Part D steps 5 and 6 F Scheduled Maintenance and Inspections Maintenance is on condition Contact Aspen Avionics at www aspenavio...

Страница 803: ...2 Lithium Ion Battery Installation 96 7 96 20 External Power 96 9 96 30 Starter and Ignition System 96 9 96 40 Lighting System 96 10 96 50 Annunciator Panel 96 10 96 60 Low Rotor RPM Warning Unit Adjustment 96 12 96 70 Audio System 96 12 96 80 Engine Monitoring Unit EMU 96 13 96 90 Emergency Locator Transmitter ELT 96 14 96 100 Electrical Load Analysis 96 15 96 110 Audio Alerts 96 18 ...

Страница 804: ...Intentionally Blank Page 96 ii Chapter 96 Electrical System JUL 2020 ...

Страница 805: ...he battery relay to allow the tachometers and clock to receive battery power with the battery switch OFF The avionics switch controls power to avionics This allows avionics to be switched OFF via a single switch Having sensitive electrical equipment off when the generator is switched ON protects against voltage spikes An ammeter indicates total generator output A digital voltmeter which reads main...

Страница 806: ...FIGURE 96 1A B237 7 LEAD ACID BATTERY INSTALLATION Page 96 2 Chapter 96 Electrical System APR 2019 ...

Страница 807: ...ve ground cable A Disconnecting and Removing Battery 1 Turn battery switch off Open baggage compartment door Remove auxiliary fuel tank per 28 51 if installed 2 Refer to Figure 96 1A 96 1B Remove G248 8 cover assembly 3 Remove hardware securing negative ground cable to battery negative terminal B237 7 battery or G131 5 terminal assembly B237 8 battery 4 Remove hardware securing positive cable to b...

Страница 808: ...Page 96 4 Chapter 96 Electrical System APR 2019 FIGURE 96 1B B237 8 LEAD ACID BATTERY INSTALLATION ...

Страница 809: ... battery routing negative ground cable as shown Special torque bolt per battery decal and torque stripe per Figure 5 1 6 Install G248 8 cover assembly verify security Install auxiliary fuel tank per 28 51 as required Close baggage compartment door 7 a If B237 7 battery was removed and B237 8 battery was installed Revise Weight and Balance Record in R66 Pilot s Operating Handbook POH Section 6 to i...

Страница 810: ...Intentionally Blank Page 96 4B Chapter 96 Electrical System APR 2019 ...

Страница 811: ...Intentionally Blank JUL 2020 Chapter 96 Electrical System Page 96 5 ...

Страница 812: ...FIGURE 96 2 LITHIUM ION BATTERY INSTALLATION Page 96 6 Chapter 96 Electrical System JUL 2020 ...

Страница 813: ...ble 9 volt batteries mounted under the co pilot s seat will supply backup power to the EMU and MGT gage Though not critical for flight safety power to these units ensures the recording of a gas temperature exceedence were one to occur during engine start NOTE Refer to True Blue Power Installation Manual and Operating Instructions for battery maintenance procedures CAUTION To minimize risk of elect...

Страница 814: ... positive terminal and install battery hardware Special torque terminal bolt as noted on battery label and torque stripe per Figure 5 1 Slide nipple over terminal 7 Install negative ground cable to battery negative terminal and install battery hardware Special torque terminal bolt as noted on battery label and torque stripe per Figure 5 1 8 Install G248 8 cover assembly and install hardware Verify...

Страница 815: ...a diode provides polarity protection 96 30 Starter and Ignition System A single starter generator is used for engine starting and electrical power generation A generator control unit GCU controls starter generator function During a start the GCU latches the starter on until N1 reaches 58 percent RPM Therefore the pilot is not required to hold the start button down throughout the start sequence Abo...

Страница 816: ...e at pilot discretion 96 50 Annunciator Panel The annunciator panel consists of illuminated segments located at the top of the main instrument panel If a caution or warning condition occurs the appropriate segment s illuminate indicating the nature of the problem The CHIP segments are illuminated by magnetic chip devices in each gearbox which collect metallic particles in order to complete an elec...

Страница 817: ...right aft seatback assembly 2 Disconnect EMU from airframe electrical harness 3 Using an insulated jumper connect airframe wire 2044 pin 13 on airframe connector to EMU to a convenient airframe ground 4 Turn battery switch on Depress push to test switch adjacent to annunciator panel and observe EMU annunciator segment response a If EMU annunciator segment illuminates Turn battery switch off and di...

Страница 818: ...rom a 3 8 inch diameter hole in the left vertical panel exterior Adjust screw on back of warning unit 2 turns equals approximately 1 change 96 70 Audio System A five place audio system is standard An audio control panel allows control of communication radios intercom and stereo capable auxiliary audio e g music input The system has four modes of operation In normal mode all occupants hear incoming...

Страница 819: ... after the aircraft battery is switched ON Once initialization is complete steady illumination of the annunciator means normal EMU operation A slowly flashing indication once every two seconds is given if the EMU detects a fault in its senders or circuitry A fast flashing indication four times per second is given if the EMU has detected an exceedance A fault or exceedance indication should be inve...

Страница 820: ...ld always be in this position for flight The remote switch annunciator is a three position switch with indicator light This switch should be in the ARMED position for flight With both switches set to armed the ELT will begin transmitting when subjected to a high G load When the unit is transmitting the red indicator light illuminates Moving the remote switch to ON activates the transmitter Use the...

Страница 821: ... SENDER 1 0 025 0 025 0 025 0 025 LOW RPM UNIT W HORN 1 0 045 0 160 0 045 0 160 AA12S 600 AUDIO PANEL 1 1 000 1 000 1 000 1 000 N2 GOVERNOR SYSTEM 1 0 000 0 0871 0 000 0 0871 N2 GOV ACTUATOR 12V 1 0 150 N2 GOV RELAY 12V 1 0 010 ANTI ICE SOLENOID 1 0 670 0 670 0 670 0 670 HEATED PITOT 1 4 000 4 000 4 000 4 000 ENGINE HOUR METER 2 0 015 0 015 0 030 0 030 HYD CONTROL SOLENOID 1 0 800 0 000 0 800 ENGI...

Страница 822: ... 670 3 000 SUBTOTAL LIGHTS BUS 5 961 15 591 COMPONENT QTY CONTINUOUS AMPS EACH INTERMITTENT AMPS EACH CONTINUOUS TOTAL INTERMITTENT TOTAL AVIONICS BUS KY196A COM 1 1 000 5 000 1 000 5 0002 GNC 420W GPS COM 1 1 215 4 200 1 215 1 2152 GNS 530AW GPS COM NAV 1 1 415 4 400 1 415 1 4152 GTX 330 XPDR 1 1 640 9 090 1 640 9 090 BLIND ENCODER 1 0 600 0 600 0 600 0 600 AM FM CD RCVR 1 1 500 1 500 1 500 1 500...

Страница 823: ...EQUIPMENT TACH RELAY 1 0 060 0 060 0 060 0 060 CLOCK DIGITAL 1 0 003 0 003 0 003 0 003 BATTERY RELAY 1 0 250 6 000 0 250 6 000 START GEN RELAY 1 0 250 6 000 0 250 6 000 GEN LT RELAY 1 0 010 0 010 0 010 0 010 GEN CONTROL UNIT 1 0 2004 2 0005 0 200 2 000 IGNITION EXCITER 1 1 500 0 000 1 500 EXTERNAL PWR RELAY2 1 0 250 6 000 BAGGAGE COMPARTMENT LT2 1 0 020 0 020 SIGHT GLASS LED2 2 0 020 0 020 LATCHIN...

Страница 824: ...5 For high engine torque MGT a beeping tone indicates torque above 100 or MGT above 782 C 5 minute limits High torque is indicated by four beeps per second increasing to 12 beeps per second if torque exceeds 108 High MGT is indicated by 12 beeps per second The beep tone will also come on during start if MGT exceeds 860 C indicating an abnormally hot start Test buttons on the instrument panel permi...

Страница 825: ...tion 97 9 97 30 Garmin GTX 33 Transponder Installation 97 12 97 40 Garmin GDL 69A XM Receiver Installation 97 15 97 50 Avionics for R66 S N 293 520 522 Subsequent 97 17 97 51 Cyclic Grip Assembly 97 17 97 52 Aspen EFD Electronic Flight Instrument System EFIS Installations 97 17 97 53 Garmin GTR 225B COM Radio Installation 97 18 97 54 Garmin GDL 88 ADS B In Receiver Installation 97 20 97 55 Garmin ...

Страница 826: ...Intentionally Blank Page 97 ii Chapter 97 Avionics APR 2019 ...

Страница 827: ...e Air Temperature OAT sensor The GDC 74H computer provides pressure altitude airspeed vertical speed and OAT information to the G500H EFIS system The GDC 74H computer communicates with the GDU display and GRS 77H AHRS using an ARINC 429 digital interface B Schematic Refer to Figure 98 10 for GDC 74H Air Data Computer Installation electrical schematic C Removal 1 Turn battery avionics switches off ...

Страница 828: ...nd hinge left seat back E Scheduled Maintenance and Inspections Refer to Garmin G500H EFIS Maintenance Manual Section 5 Periodic Maintenance NOTE All factory installed Garmin units are on condition and do not require scheduled periodic maintenance Units feature a BIT Built In Test function during each initial power up that will detect internal failure s and alert pilot NOTE Refer to 97 60 for avio...

Страница 829: ...r panel 2 Hinge left seat forward and remove F950 3 cover assembly 3 Disconnect airframe harness from GRS 77H AHRS at connectors 4 Loosen thumbscrews securing AHRS to F950 1 support assembly Carefully remove AHRS from under left seat D Installation 1 Turn battery avionics switches off and pull out EFIS 5 amp circuit breaker on circuit breaker panel 2 Place GRS 77H AHRS on F950 1 support assembly a...

Страница 830: ...ify no loose chafed or broken wires or terminals Verify no evidence of arcing Verify equipment security 3 Secure circuit breaker panel Perform ground checks per Part D steps 4 thru 6 97 14 LRU Installation GMU 44 Magnetometer A Description The GMU 44 magnetometer senses the earth s magnetic field Data is sent to the GRS 77H AHRS for processing to determine aircraft magnetic heading This unit recei...

Страница 831: ...ance and Inspections Refer to Garmin G500H EFIS Maintenance Manual Section 5 Periodic Maintenance NOTE All factory installed Garmin units are on condition and do not require scheduled periodic maintenance Units feature a BIT Built In Test function during each initial power up that will detect internal failure s and alert pilot NOTE Refer to 97 60 for avionics software information F Special Mainten...

Страница 832: ...Installation electrical schematic C Removal 1 Turn battery avionics switches off and pull out GPS 1 5 amp and GPS 2 5 amp circuit breakers as required on circuit breaker panel 2 Loosen radio key securing GTN 600 700 series GPS s to tray in upper console 3 Carefully unplug remove GPS s from tray D Installation 1 Turn battery avionics switches off and pull out GPS 1 5 amp and GPS 2 5 amp circuit bre...

Страница 833: ...ve antenna Installation 1 Turn battery avionics switches off and pull out GPS 1 5 amp and GPS 2 5 amp circuit breakers as required on circuit breaker panel 2 a For GPS antenna i Remove paint primer from antenna mating surfaces to ensure electrical ground ii As required apply light coat B270 13 sealant to screw threads and install screws securing antenna to tailcone As required seal around screw he...

Страница 834: ...ernal failure s and alert pilot NOTE Refer to 97 60 for avionics software information G Special Maintenance and Inspections 1 Turn battery avionics switches off Open circuit breaker panel and upper console 2 Inspect condition of and verify no obvious damage to GPS s copper bus bars circuit breaker and wiring Verify no loose chafed or broken wires or terminals Verify no evidence of arcing Verify eq...

Страница 835: ...r In Console Installation Supporting RAD 40 indicator remove hardware securing B421 1 visor assembly A590 4 cover plate and indicator to instrument face 4 Disconnect console harness from indicator and carefully remove indicator ATG 410 Tone Generator 1 Turn battery avionics switches off and pull out RADAR ALT 2 amp circuit breaker on circuit breaker panel Open instrument console or remove Garmin G...

Страница 836: ...switches off and pull out RADAR ALT 2 amp circuit breaker on circuit breaker panel 2 Connect console harness to ATG 410 tone generator 3 Position tone generator on keel panel and install screws Verify security 4 Close instrument console or install Garmin GDU 620 Display per 95 70 5 Push in RADAR ALT 2 amp circuit breaker on circuit breaker panel Turn battery avionics switches on 6 Perform appropri...

Страница 837: ...ircuit breaker panel Turn battery avionics switches on 5 Perform appropriate functional checks per Freeflight Systems Instructions for Continued Airworthiness Turn battery avionics switches off F Scheduled Maintenance and Inspections Refer to Freeflight Systems Instructions for Continued Airworthiness G Special Maintenance and Inspections 1 Turn battery avionics switches off Open circuit breaker p...

Страница 838: ...ardware securing F640 face assembly to avionics panel and remove face 3 Loosen screw and swing handle across GTX 33 transponder to unlock Carefully unplug remove transponder from tray D Installation 1 Turn battery avionics switches off and pull out XPDR 5 amp circuit breaker on circuit breaker panel 2 Carefully plug in install GTX 33 transponder in appropriate location in avionics tray 3 Swing han...

Страница 839: ...R 5 amp circuit breaker on circuit breaker panel 2 Remove paint primer from between cabin skin and B322 plate doubler to ensure electrical ground 3 Install hardware securing transponder antenna to plate doubler Verify security Apply small bead B270 1 sealant 0 1 inch max in height around antenna at corners where it attaches to plate doubler and allow to dry 4 Connect antenna cable to antenna and i...

Страница 840: ...er panel 2 Remove GTX 33 transponder per Part C Inspect condition of and verify no obvious damage to transponder radio tray copper bus bars circuit breaker and wiring Verify no loose chafed or broken wires or terminals Verify no evidence of arcing 3 Secure circuit breaker panel Install transponder per Part D Page 97 14 Chapter 97 Avionics APR 2019 ...

Страница 841: ...ull out XM 2 amp circuit breaker on circuit breaker panel 2 Remove hardware securing F640 face assembly to avionics panel and remove face 3 Loosen screw and swing handle across GDL 69A receiver to unlock Carefully unplug remove receiver from tray D Installation 1 Turn battery avionics switches off and pull out XM 5 amp circuit breaker on circuit breaker panel 2 Carefully plug in install GDL 69A re...

Страница 842: ...all bead B270 1 sealant 0 1 inch max in height around antenna at corners where it attaches to cowling and allow to dry 3 Connect antenna cable to antenna Verify security 4 Perform ground checks per Part D steps 4 and 5 F Scheduled Maintenance and Inspections NOTE All factory installed Garmin units are on condition and do not require scheduled periodic maintenance Units feature a BIT Built In Test ...

Страница 843: ... Rotate grip about weldment to desired angle Special torque cap screws to 40 in lb C Removal and Installation Refer to 67 12 for cyclic grip assembly removal and installation procedures D Schematic Refer to Figure 98 1 for F024 electrical system schematic 97 52 Aspen EFD Electronic Flight Instrument System EFIS Installations Refer to 95 73 for Aspen EFD EFIS Installations A Schematic Refer to Figu...

Страница 844: ...io 5 amp circuit breaker on circuit breaker panel 2 Loosen radio key securing C802 2 COM radio to avionics tray 3 Carefully unplug remove radio from tray D Installation 1 Turn battery switch off and pull out COM radio 5 amp circuit breaker on circuit breaker panel 2 Carefully plug in install C802 2 COM radio in appropriate location in avionics tray 3 Tighten radio key securing radio to tray Verify...

Страница 845: ...fy security 4 Apply small bead B270 1 sealant 0 1 inch max in height around antenna at corners where it attaches to tailcone and allow to dry 5 Connect antenna cable to antenna Verify security 6 Perform ground checks per Part D steps 4 and 5 F Scheduled Maintenance and Inspections NOTE All factory installed Garmin units are on condition and do not require scheduled periodic maintenance Units featu...

Страница 846: ...layed on the primary GPS screen Refer to 97 16 B Schematic Refer to Figure 98 10 for C803 2 ADS B Installation electrical schematic C Removal 1 Turn battery switch off and pull out XPDR 5 amp circuit breaker on circuit breaker panel 2 Under left front seat disconnect airframe harness from GDL 88 receiver at connectors 3 Remove screws securing GDL 88 receiver to C904 1 mount assembly and remove GDL...

Страница 847: ...ly Apply small bead B270 1 sealant around antenna at corners where it attaches to belly and allow to dry 4 Connect antenna cable to antenna Verify security 5 Perform ground checks per Part D steps 4 and 5 F Scheduled Maintenance and Inspections NOTE All factory installed Garmin units are on condition and do not require scheduled periodic maintenance Units feature a BIT Built In Test function durin...

Страница 848: ...ntered by the pilot using transponder controls ADS B data is transmitted via the transponder s Extended Squitter ES on frequency 1090 MHz The ADS B In system receives data via a receiver on frequencies 978 MHz and 1090 MHz Received data is displayed on the primary GPS screen ADS B Out equipment transponder and primary GPS or ADS B Out and ADS B In equipment transponder primary GPS and receiver mus...

Страница 849: ...amp circuit breaker on circuit breaker panel 2 Using plastic scraper remove B270 1 sealant from around transponder antenna at corners where it attaches to B322 11 mounting plate 3 Remove screws securing mounting plate to cabin skin and disconnect antenna cable from antenna Remove hardware securing mounting plate to antenna and remove antenna Installation 1 Turn battery switch off and pull out XPDR...

Страница 850: ...ify no evidence of arcing Verify equipment security 3 Secure circuit breaker panel and upper console Perform ground checks per Part D steps 4 and 5 97 56 Garmin GTN 600 700 series GPS Installation NOTE Refer to Garmin GTN 600 700 series Maintenance Manual and Instructions for Continued Airworthiness A Description of New Features The new C831 GPS Garmin GTN 600 700 series includes similar navigatio...

Страница 851: ...amp circuit breakers as required on circuit breaker panel Turn battery avionics switches on 5 Perform appropriate functional checks per Garmin GTN 600 700 series Pilot s Guide Turn battery avionics switches off E Antenna Refer to 6 80 for antenna locations and R66 Illustrated Parts Catalog IPC Chapter 6 NOTE Antenna installation depends on number COM installations and additional equipment installe...

Страница 852: ...and 5 F Scheduled Maintenance and Inspections NOTE All factory installed Garmin units are on condition and do not require scheduled periodic maintenance Units feature a BIT Built In Test function during each initial power up that will detect internal failure s and alert pilot NOTE Refer to 97 60 for avionics software information G Special Maintenance and Inspections 1 Turn battery avionics switche...

Страница 853: ...from separate locations around the listener and some control functions via voice command when a momentary pushbutton switch is depressed on the pilot s cyclic grip B Schematic Refer to Figure 98 14 for F060 Intercom System Installation Garmin GMA 350H Audio Control electrical schematic C Removal 1 Turn battery switch off pull out ICS 5 amp circuit breaker on circuit breaker panel 2 Loosen radio ke...

Страница 854: ...primer from antenna mating surfaces to ensure electrical ground 3 Apply light coat B270 11 adhesive to screw threads and install screws securing CI 102 marker beacon antenna to F794 forward belly panel Verify security 4 Connect F850 210 antenna cable to antenna Install screws securing forward belly panel to belly Verify security 5 Apply small bead B270 1 sealant 0 1 inch max in height around anten...

Страница 855: ... installation in Robinson helicopters Software updates should not be attempted without a thorough understanding of approval status and compatibility Technical support from either RHC or the avionics manufacturer will likely be required In some cases updating software for one item of avionics may require additional avionics to be updated to assure compatibility As long as RHC installed equipment is...

Страница 856: ...Intentionally Blank Page 97 30 Chapter 97 Avionics APR 2019 ...

Страница 857: ...s GPS Installation G500H EFIS 98 23 98 13A Avidyne IFD 4XX 5XX series GPS Installation 98 24A 98 13B Garmin 500 Series GPS Installation 98 24C 98 13C Garmin 500 Series GPS Installation 98 24D 98 14 Radar Altimeter Installation 98 25 98 15 Garmin GTX 3X5 Transponder Installation 98 27 98 16 Garmin GTX 33 328 330 ES Transponder Installation 98 29 98 17 Garmin GDL 69A XM Receiver Installation 98 31 9...

Страница 858: ...on Battery Installation 98 47 98 27 Heated Seats Installation 98 51 98 28 Cargo Hook Installation 98 53 98 29 External Load Controls 98 55 98 30 Copilot Instruments Installation 98 57 98 31 Bubble Door Fans Installation 98 59 98 32 Dual Low Fuel Warning Light Installation 98 61 98 33 Fuel Flow Meter Installation 98 61 ...

Страница 859: ...JUL 2020 Chapter 98 Wiring Diagrams Page 98 1 FIGURE 98 1 R66 ELECTRICAL SYSTEM REVISION V ...

Страница 860: ...Page 98 2 Chapter 98 Wiring Diagrams JUL 2020 Intentionally Blank ...

Страница 861: ...JUL 2020 Chapter 98 Wiring Diagrams Page 98 2A FIGURE 98 2A R66 ELECTRICAL SYSTEM F024 2 REVISION R ...

Страница 862: ...Page 98 2B Chapter 98 Wiring Diagrams JUL 2020 FIGURE 98 2B R66 ELECTRICAL SYSTEM F024 1 REVISION J ...

Страница 863: ...APR 2017 Chapter 98 Wiring Schematics Page 98 3 FIGURE 98 3 AIR CONDITIONING INSTALLATION ...

Страница 864: ...Page 98 4 Chapter 98 Wiring Schematics APR 2017 Intentionally Blank ...

Страница 865: ...FIGURE 98 4 ADF INSTALLATION APR 2017 Chapter 98 Wiring Diagrams Page 98 5 ...

Страница 866: ...Intentionally Blank Page 98 6 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 867: ...APR 2017 Chapter 98 Wiring Schematics Page 98 7 FIGURE 98 5 STANDARD AUDIO INSTALLATION NAT AA12S 600 AUDIO CONTROL ...

Страница 868: ...Page 98 8 Chapter 98 Wiring Schematics APR 2017 Intentionally Blank ...

Страница 869: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 9 FIGURE 98 6 DUAL AUDIO CONTROL INSTALLATION ...

Страница 870: ...Intentionally Blank Page 98 10 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 871: ...FIGURE 98 7 PA SIREN INSTALLATION APR 2017 Chapter 98 Wiring Diagrams Page 98 11 ...

Страница 872: ...Intentionally Blank Page 98 12 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 873: ...JUL 2020 Chapter 98 Wiring Schematics Page 98 13 FIGURE 98 8A AUTOPILOT INSTALLATION ...

Страница 874: ...Page 98 14 Chapter 98 Wiring Schematics JUL 2020 FIGURE 98 8B AUTOPILOT INSTALLATION ...

Страница 875: ...FIGURE 98 9 GARMIN GDU 1060 INSTALLATION APR 2019 Chapter 98 Wiring Diagrams Page 98 15 ...

Страница 876: ...Page 98 16 Chapter 98 Wiring Diagrams APR 2019 FIGURE 98 9A GARMIN GDU 620 INSTALLATION ...

Страница 877: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 17 FIGURE 98 10 GARMIN GSU 75 ADAHRS INSTALLATION ...

Страница 878: ...Intentionally Blank Page 98 18 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 879: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 19 FIGURE 98 11 GARMIN GDC 74H AIR DATA COMPUTER INSTALLATION ...

Страница 880: ...Intentionally Blank Page 98 20 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 881: ...FIGURE 98 12 GARMIN GRS 77H AHRS INSTALLATION APR 2017 Chapter 98 Wiring Diagrams Page 98 21 ...

Страница 882: ...Intentionally Blank Page 98 22 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 883: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 23 FIGURE 98 13 GARMIN GTN 6XX 7XX SERIES GPS INSTALLATION G500H EFIS ...

Страница 884: ...Intentionally Blank Page 98 24 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 885: ...JUL 2020 Chapter 98 Wiring Schematics Page 98 24A FIGURE 98 13A AVYIDYNE IFD 4XX 5XX SERIES INSTALLATION ...

Страница 886: ...Page 98 24B Chapter 98 Wiring Schematics JUL 2020 Intentionally Blank ...

Страница 887: ...JUL 2020 Chapter 98 Wiring Schematics Page 98 24C FIGURE 98 13B GARMIN 500 SERIES GPS INSTALLATION ...

Страница 888: ...Page 98 24D Chapter 98 Wiring Schematics JUL 2020 FIGURE 98 13C GARMIN 500 SERIES GPS INSTALLATION ...

Страница 889: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 25 FIGURE 98 14 RADAR ALTIMETER INSTALLATION ...

Страница 890: ...Intentionally Blank Page 98 26 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 891: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 27 FIGURE 98 15 GARMIN GTX 3X5 TRANSPONDER INSTALLATION ...

Страница 892: ...Intentionally Blank Page 98 28 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 893: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 29 FIGURE 98 16 GARMIN GTX 33 328 330 ES TRANSPONDER INSTALLATION ...

Страница 894: ...Intentionally Blank Page 98 30 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 895: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 31 FIGURE 98 17 GARMIN GDL 69A XM RECEIVER INSTALLATION ...

Страница 896: ...Intentionally Blank Page 98 32 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 897: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 33 FIGURE 98 18 ASPEN EFD1000H DISPLAY INSTALLATION ...

Страница 898: ...Intentionally Blank Page 98 34 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 899: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 35 FIGURE 98 19 ASPEN EFD500H DISPLAY INSTALLATION ...

Страница 900: ...Intentionally Blank Page 98 36 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 901: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 37 FIGURE 98 20 GARMIN GTR 225B COM GNC 255B NAV COM RADIO INSTALLATION ...

Страница 902: ...Intentionally Blank Page 98 38 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 903: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 39 FIGURE 98 21 GARMIN GTR 225B COM RADIO INSTALLATION ...

Страница 904: ...Intentionally Blank Page 98 40 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 905: ...FIGURE 98 22 GARMIN GDL 88 ADS B IN RECEIVER INSTALLATION APR 2017 Chapter 98 Wiring Diagrams Page 98 41 ...

Страница 906: ...Intentionally Blank Page 98 42 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 907: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 43 FIGURE 98 23 GARMIN GTN 6XX 7XX SERIES GPS INSTALLATION PILOT SIDE CONSOLE ...

Страница 908: ...Intentionally Blank Page 98 44 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 909: ...JUL 2020 Chapter 98 Wiring Schematics Page 98 45 FIGURE 98 24 F060 INTERCOM SYSTEM INSTALLATION GARMIN GMA 350HC AUDIO CONTROL ...

Страница 910: ...Page 98 45A Chapter 98 Wiring Schematics JUL 2020 Intentionally Blank ...

Страница 911: ...FIGURE 98 25A F060 4 5 6 7 INTERCOM SYSTEM INSTALLATION GARMIN GMA 350HC AUDIO CONTROL JUL 2020 Chapter 98 Wiring Schematics Page 98 45B ...

Страница 912: ...Page 98 46 Chapter 98 Wiring Schematics JUL 2020 FIGURE 98 25B F060 1 2 INTERCOM SYSTEM INSTALLATION GARMIN GMA 350H AUDIO CONTROL ...

Страница 913: ...APR 2017 Chapter 98 Wiring Diagrams Page 98 47 FIGURE 98 26 LITHIUM ION BATTERY INSTALLATION ...

Страница 914: ...Intentionally Blank Page 98 48 Chapter 98 Wiring Diagrams APR 2017 ...

Страница 915: ...APR 2019 Chapter 98 Wiring Diagrams Page 98 49 FIGURE 98 27 HEATED SEATS INSTALLATION ...

Страница 916: ...Intentionally Blank Page 98 50 Chapter 98 Wiring Diagrams APR 2019 ...

Страница 917: ...FIGURE 98 28 CARGO HOOK INSTALLATION APR 2019 Chapter 98 Wiring Diagrams Page 98 51 ...

Страница 918: ...Intentionally Blank Page 98 52 Chapter 98 Wiring Diagrams APR 2019 ...

Страница 919: ...FIGURE 98 29 EXTERNAL LOAD CONTROLS APR 2019 Chapter 98 Wiring Diagrams Page 98 53 ...

Страница 920: ...Intentionally Blank Page 98 54 Chapter 98 Wiring Diagrams APR 2019 ...

Страница 921: ...FIGURE 98 30 COPILOT INSTRUMENTS INSTALLATION APR 2019 Chapter 98 Wiring Diagrams Page 98 55 ...

Страница 922: ...Intentionally Blank Page 98 56 Chapter 98 Wiring Diagrams APR 2019 ...

Страница 923: ...FIGURE 98 31 BUBBLE DOOR FANS INSTALLATION APR 2019 Chapter 98 Wiring Diagrams Page 98 57 ...

Страница 924: ...Intentionally Blank Page 98 58 Chapter 98 Wiring Diagrams APR 2019 ...

Страница 925: ...FIGURE 98 32 DUAL LOW FUEL WARNING LIGHT INSTALLATION APR 2019 Chapter 98 Wiring Diagrams Page 98 59 ...

Страница 926: ...Intentionally Blank Page 98 60 Chapter 98 Wiring Diagrams APR 2019 ...

Страница 927: ...FIGURE 98 33 FUEL FLOW METER INSTALLATION JUL 2020 Chapter 98 Wiring Diagrams Page 98 61 ...

Страница 928: ...Intentionally Blank Page 98 62 Chapter 98 Wiring Diagrams JUL 2020 ...

Страница 929: ...CHAPTER 99 SPECIAL TOOLS Section Title Page 99 10 Special Tools 99 1 99 20 Illustrations and Tasks 99 2 APR 2017 Chapter 99 Special Tools Page 99 i ...

Страница 930: ...Intentionally Blank Page 99 ii Chapter 99 Special Tools APR 2017 ...

Страница 931: ... The following is a list of Robinson R66 special tools R66 special tools are to be used in conjunction with the applicable instructions for continued airworthiness for their designated maintenance task APR 2017 Chapter 99 Special Tools Page 99 1 ...

Страница 932: ...n Assembly MM 12 11 2 MT122 6 Micrometer Assembly Main Rotor Hub Bolt Stretch MM 62 10 3 MT146 4 Blocks Swashplate Rigging set of 2 MM 18 30 4 MT147 1 Bleed Tool Main Rotor Blade Spindle MM 12 51 5 MT179 4 Balancing Bar Tail Rotor Assembly Static Balance MM 64 11 6 MT260 6 Tail Rotor Drive Shaft Runout Attachments Kit MM 65 21 7 MT329 6 Plug Main Rotor Hub Bearing Installation MM 62 21 ...

Страница 933: ... 4 or 7 Teeter Moment Tool MM 62 32 3 MT357 2 0 375 inch diameter Reamer Various 4 MT357 3 0 156 inch diameter Cobalt Steel Drill MM 62 33 5 MT357 4 Hex Driver Snap On Part No FABL8 MM 65 40 6 MT357 5 Torque Adapter Snap On Part No FRDH101 MM 65 40 7 MT359 1 Spring Scale 0 30 lb MM 62 32 67 22 67 41 Ream bore after installation of A139 1 bearing to 0 376 0 375 inch diameter FIGURE 99 2 SPECIAL TOO...

Страница 934: ...draulic Test Pump U S Canada Mexico 110 V MM 12 33 2 MT384 2 Hydraulic Test Pump Outside North America 220 V MM 12 33 3 MT525 7 Main Rotor Blade Rigging Fixture MM 18 40 4 MT525 9 Tail Rotor Blade Rigging Fixture MM 18 60 5 MT526 8 Bender Assembly Trim Tab Main Rotor Blade aluminum MM 18 13 6 MT527 1 Helicopter Lifting Fixture MM 7 20 7 MT548 8 Fitting engine hoist adapter MM 71 10 ...

Страница 935: ...MM 62 10 2 MT549 2 Plate Spindle Boot MM 62 10 3 MT556 11 Kit Tools Tail Rotor Hub Bearing Replacement MM 64 41 4 MT569 2 Guide Assembly Drill main rotor hub nut MM 62 33 5 MT643 1 Support Weldment Main Rotor Hub Bearing Installation MM 62 21 6 MT759 1 Blocks Cyclic Rigging MM 18 41 7 2020HR ACES Probalancer Analyzer or equivalent dynamic balancer MM 18 10 FIGURE 99 4 SPECIAL TOOLS ...

Страница 936: ...ed Refer to Figure 99 5 Item Part Number Description 1 MT850 1 Engine Stand Assembly RR300 2 AN970 4 Washer Tap Test Tool 3 MT990 1 MT990 2 Charger Assembly BatteryMinder 24 VDC 120 VAC 50 60 Hz Charger Assembly BatteryMinder 24 VDC 240 VAC 50 60 Hz Or 1965 or later U S quarter dollar coin in good condition ...

Страница 937: ...n x 66 50 in 2 R5387 Windshield Box 21 75 in x 40 in x 66 in cardboard Holds up to four windshields 3 R5352 Main Rotor Blade Crate 21 75 in x 17 in x 206 50 in 4 R5385 Push Pull Tube Tail Rotor Drive Shaft Crate 10 25 in x 11 50 in x 192 in Dimensions are approximate and expressed in inches Dimensions are provided in height x width x length FIGURE 99 6 SHIPPING CRATES ...

Страница 938: ...23 75 in x 34 in x 60 in holds 1 bubble or 2 regular doors 2 R5388 Tailcone Crate 27 25 in x 24 in x 192 in 3 R5702 Main Rotor Blade Tailcone Crate 28 in x 30 in x 208 in 4 R7982 Main Rotor Gearbox Crate 27 in x 28 75 in x 89 50 in Dimensions are approximate and expressed in inches Dimensions are provided in height x width x length FIGURE 99 7 SHIPPING CRATES ...

Страница 939: ...CHAPTER 100 REVISION LOG Section Title Page Revision Log 100 1 JUL 2020 Chapter 100 Revision Log Page 100 i ...

Страница 940: ...Intentionally Blank Page 100 ii Chapter 100 Revision Log JUL 2020 ...

Страница 941: ...20 4 2 JUL 2020 4 3 JUL 2020 4 4 JUL 2020 4 5 JUL 2020 4 6 JUL 2020 4 7 JUL 2020 4 8 JUL 2020 4 9 JUL 2020 4 10 JUL 2020 5 i JUL 2020 5 ii JUL 2020 5 1 JUL 2020 5 2 JUL 2020 5 3 JUL 2020 5 4 JUL 2020 5 5 JUL 2020 5 6 JUL 2020 5 7 JUL 2020 5 8 JUL 2020 5 9 JUL 2020 5 9A JUL 2020 5 9B JUL 2020 5 10 JUL 2020 5 11 JUL 2020 5 12 JUL 2020 5 13 JUL 2020 5 14 JUL 2020 5 15 APR 2017 5 16 APR 2017 5 16A APR...

Страница 942: ...3 JUL 2020 8 14 JUL 2020 9 i 25 OCT 2010 9 ii 25 OCT 2010 9 1 25 OCT 2010 9 2 25 OCT 2010 9 3 SEP 2012 9 4 SEP 2012 10 i 25 OCT 2010 10 ii 25 OCT 2010 10 1 SEP 2012 10 2 SEP 2012 10 3 25 OCT 2010 10 4 25 OCT 2010 10 5 25 OCT 2010 10 6 25 OCT 2010 11 i APR 2017 11 ii APR 2017 11 1 APR 2017 11 2 APR 2017 12 i JUL 2020 12 ii JUL 2020 12 1 SEP 2012 12 2 SEP 2012 12 3 APR 2019 12 4 APR 2019 12 5 SEP 20...

Страница 943: ...20 11A JUL 2020 20 11B JUL 2020 20 11C JUL 2020 20 11D JUL 2020 20 11E JUL 2020 20 11F JUL 2020 20 11G JUL 2020 20 11H JUL 2020 20 11I JUL 2020 20 11J JUL 2020 20 11K JUL 2020 20 11L JUL 2020 20 11M JUL 2020 20 11N JUL 2020 20 12 JUL 2020 20 13 APR 2017 20 14 APR 2017 20 15 JUL 2020 20 16 JUL 2020 20 17 JUL 2020 20 18 JUL 2020 20 18A JUL 2020 20 18B JUL 2020 20 19 JUL 2020 20 20 JUL 2020 20 21 JUL...

Страница 944: ...UL 2020 28 11C JUL 2020 28 11D JUL 2020 28 12 JUL 2020 28 13 APR 2017 28 14 APR 2017 28 15 JUL 2020 28 16 JUL 2020 28 17 JUL 2020 28 18 JUL 2020 28 19 JUL 2020 28 20 JUL 2020 28 21 JUL 2020 28 22 JUL 2020 28 23 APR 2019 28 24 APR 2019 28 25 JUL 2020 28 26 JUL 2020 28 27 JUL 2020 28 28 JUL 2020 29 i MAY 2015 29 ii MAY 2015 29 1 MAY 2015 29 2 MAY 2015 29 3 JUL 2020 29 4 JUL 2020 29 5 MAY 2015 29 6 M...

Страница 945: ...15 53 20 MAY 2015 53 21 MAY 2015 53 22 MAY 2015 62 i JUL 2020 62 ii JUL 2020 62 1 25 OCT 2010 62 2 25 OCT 2010 62 3 25 OCT 2010 62 4 25 OCT 2010 62 5 MAY 2015 62 6 MAY 2015 62 7 25 OCT 2010 62 8 25 OCT 2010 62 9 25 OCT 2010 62 10 25 OCT 2010 62 10A JUL 2020 62 10B JUL 2020 62 11 25 OCT 2010 62 12 25 OCT 2010 62 13 25 OCT 2010 62 14 25 OCT 2010 62 15 25 OCT 2010 62 16 25 OCT 2010 62 17 JUL 2020 62 ...

Страница 946: ...67 10 APR 2017 67 11 MAY 2015 67 12 MAY 2015 67 13 JUL 2020 67 14 JUL 2020 67 15 MAY 2015 67 16 MAY 2015 67 17 MAY 2015 67 18 MAY 2015 71 i JUL 2020 71 ii JUL 2020 71 1 JUL 2020 71 2 JUL 2020 71 3 JUL 2020 71 3A JUL 2020 71 3B JUL 2020 71 4 JUL 2020 71 5 JUL 2020 71 6 JUL 2020 71 7 JUL 2020 71 7A JUL 2020 71 7B JUL 2020 71 8 JUL 2020 71 9 JUL 2020 71 10 JUL 2020 71 11 APR 2019 71 12 APR 2019 71 13...

Страница 947: ... 92 30 JUL 2020 92 31 JUL 2020 92 31A JUL 2020 92 31B JUL 2020 92 32 JUL 2020 92 33 JUL 2020 92 34 JUL 2020 92 35 JUL 2020 92 36 JUL 2020 92 37 JUL 2020 92 38 JUL 2020 92 39 JUL 2020 92 40 JUL 2020 92 41 JUL 2020 92 42 JUL 2020 92 43 JUL 2020 92 44 JUL 2020 92 45 JUL 2020 92 46 JUL 2020 92 47 JUL 2020 92 48 JUL 2020 92 49 JUL 2020 92 50 JUL 2020 92 51 JUL 2020 90 1 JUL 2020 90 2 JUL 2020 90 3 JUL ...

Страница 948: ... 2019 95 27 APR 2019 95 28 APR 2019 95 29 APR 2019 95 30 APR 2019 95 31 APR 2019 95 32 APR 2019 96 i JUL 2020 96 ii JUL 2020 96 1 APR 2019 96 2 APR 2019 96 3 APR 2019 96 4 APR 2019 96 4A APR 2019 96 4B APR 2019 96 5 JUL 2020 96 6 JUL 2020 96 7 JUL 2020 96 8 JUL 2020 96 9 APR 2017 96 10 APR 2017 96 11 APR 2017 96 12 APR 2017 96 13 APR 2017 96 14 APR 2017 96 15 APR 2017 96 16 APR 2017 96 17 JUL 2020...

Страница 949: ...00 i JUL 2020 100 ii JUL 2020 100 1 JUL 2020 100 2 JUL 2020 100 3 JUL 2020 100 4 JUL 2020 100 5 JUL 2020 100 6 JUL 2020 100 7 JUL 2020 100 8 JUL 2020 100 9 JUL 2020 100 10 JUL 2020 98 2B JUL 2020 98 3 APR 2017 98 4 APR 2017 98 5 APR 2017 98 6 APR 2017 98 7 APR 2017 98 8 APR 2017 98 9 APR 2017 98 10 APR 2017 98 11 APR 2017 98 12 APR 2017 98 13 JUL 2020 98 14 JUL 2020 98 15 APR 2019 98 16 APR 2019 9...

Страница 950: ...Intentionally Blank Page 100 10 Chapter 100 Revision Log JUL 2020 ...

Результаты поиска

Содержание R-66 Series Lithium-Ion

Отзывы:

Бренды по названию

Популярные бренды

Robinson R-66 Series Lithium-Ion, Руководство по обслуживанию

Результаты поиска

Содержание R-66 Series Lithium-Ion

Отзывы:

Бренды по названию

Популярные бренды