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The Airplane Factory Sling 4, Руководство по обслуживанию

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DOCUMENT No.: 

REVISION: 1.2 

       DATE: 2014/11/10

 

DC-MAM-001-X-C-2 

 

 

Page 196

  

14. Disconnect the two plugs (6) between the TCU and the waste gate servo (7). This allows the servo 

to be removed with the engine (by undoing the two bolts (8) retaining it to the firewall), keeping the 
servo-to-waste  gate  cable  connection  in  place  (and  negating  the  need  to  re-adjust  the  cable  after 
reconnection).  Alternatively  disconnect  the  cable  (9)  from  the  servo  at  the  turbocharger  (10)  and 
leave the servo attached to the firewall when removing the engine. 

 

 

 

 

 

 

 

 

15. Disconnect  the  cabin  air  feed  pipe  (11)  at  the  heat  exchanger  /  muffler  assembly  by  undoing  the 

clamp (or at the firewall). 

 

 

 

 

 

 

16. Cut any / all tie wraps securing pipes (connected to the engine) and electrical cabling (connected to 

the engine) to the engine mount and which would prevent the engine and attached piping / cabling 
from pulling free of the engine mount. 

17. Support the engine in such a manner that when the bolts attaching the engine suspension frame to 

the engine mount are undone they can be removed / pulled out freely. If the engine is supported by 
hoisting  it  with  a  crane  or  block  and  tackle,  attachment  must  be  such  that  the  hoisted  assembly 
(engine, engine with propeller attached, etc.) balances evenly (about its centre of gravity) under the 
hoist when freed and moved away from the engine mount. 

 

 

6

5

1 

 

7 

 

8 

 

8 

 

9 

 

10 

 

10 

 

11 

 

7 

 

Содержание Sling 4

Страница 1: ......

Страница 2: ...FORM THE AIRPLANE FACTORY AIRCRAFT MANUFACTURER ON CHANGE OF OWNERSHIP OF THE AIRCRAFT NOTICE AIRCRAFT WHICH DIFFER FROM THE PRODUCTION STANDARD IN WHATEVER WAY ARE NOT ADDRESSED IN THIS MANUAL EXCEPT...

Страница 3: ...l inspection considerations inspection schedules and inspection procedures SECTION 3 SERVICE This section provides information regarding general service considerations and service schedules SECTION 4...

Страница 4: ...1 Corrected servo motor body orientation in Figure 14 and Figure 28 2 Updated wiring diagrams 3 Updated front occupant s safety harness es removal 4 Changed wing rear attachment bolt torque from 20 N...

Страница 5: ...soline AWG American Wire Gauge BATT Battery BNC Bayonet Neill Concelman connector type C Common CAN Controller Area Network CG Centre of Gravity DC Direct Current EFIS Electronic Flight Information Sy...

Страница 6: ...e at a specified datum QNH Barometric pressure adjusted to sea level RDAC Remote Data Acquisition Computer RSA Republic of South Africa RON Research Octane Number RS232 Recommended Standard 232 RX Rec...

Страница 7: ...GL Avionics EFIS Integrated Autopilot user and Installation Manual 9 ASTM D7547 Standard Specification for Hydrocarbon Unleaded Aviation Gasoline 10 ASTM D910 Standard Specification for Aviation Gasol...

Страница 8: ...AND PRESSURES 12 1 8 GROUND HANDLING 12 1 9 JACKING 13 1 10 PARKING AND TIE DOWN 14 1 11 AIRCRAFT LEVELLING 14 1 11 1 LONGITUDINAL LEVELLING 15 1 11 2 TRANSVERSE LEVELLING 17 1 12 AIRCRAFT ALIGNMENT...

Страница 9: ...SCHEDULE 43 2 3 1 ENGINE 43 2 3 2 PROPELLER 43 2 3 3 AIRFRAME AND SYSTEMS 43 2 4 CONDITION INSPECTION 100 HOUR ANNUALLY 44 2 4 1 INSPECTION PANELS AND INITIAL INSPECTION AND CLEANING 44 2 4 2 FUSELAG...

Страница 10: ...AP ADJUSTMENT 97 4 1 3 4 FLAP ACTUATOR MOTOR REMOVAL INSTALLATION 99 4 2 EMPENNAGE 102 4 2 1 HORIZONTAL TAIL AND ELEVATOR 102 4 2 1 1 ELEVATOR CONTROL SYSTEM 103 4 2 1 2 ELEVATOR REMOVAL INSTALLATION...

Страница 11: ...ATION 163 4 4 2 2 NOSE WHEEL REMOVAL INSTALLATION 164 4 4 2 3 NOSE WHEEL DISASSEMBLY ASSEMBLY 167 4 4 2 4 NOSE WHEEL BEARING REMOVAL REPLACEMENT 170 4 4 2 5 NOSE GEAR REMOVAL INSTALLATION 171 5 POWER...

Страница 12: ...MOVAL INSTALLATION 225 6 4 FUEL SELECTOR UNIT ASSEMBLY DISASSEMBLY 228 6 5 FUEL PUMP ASSEMBLY REMOVAL INSTALLATION 230 6 6 FUEL PUMP REMOVAL INSTALLATION FROM INTO FUEL PUMP ASSEMBLY 236 6 7 FUEL TANK...

Страница 13: ...CIRCUIT BREAKERS AND OR SWITCHES 282 10 5 REGULATOR RECTIFIER REMOVAL AND REPLACEMENT 285 11 EXTERIOR LIGHTING 287 11 1 NAVIGATION LIGHTS 287 11 1 1 NAVIGATION LIGHT REMOVAL INSTALLATION 288 11 2 LAND...

Страница 14: ...GATION LIGHTS WIRING DIAGRAM 317 13 12 RDAC TO OIL PRESSURE TRANSDUCER WIRING DIAGRAM 318 13 13 DUAL EFIS INSTALLATION WIRING DIAGRAM 319 13 14 TRANSPONDER WIRING DIAGRAM 320 13 14 1 TRIG TT21 TRANSPO...

Страница 15: ...15 Aileron autopilot servo pushrod control stick torque tube end 89 Figure 16 Flap control system 90 Figure 17 Flap hinges 93 Figure 18 Flap pushrod to flap connection 94 Figure 19 Flap pushrod to fla...

Страница 16: ...vacuum pump fitted 215 Figure 51 Propeller installation external alternator fitted 216 Figure 52 Fuel system 220 Figure 53 Fuel selector unit installation 227 Figure 54 Fuel selector port allocation a...

Страница 17: ...rvo wiring diagram 313 Figure 77 EFIS back up battery charge circuit 314 Figure 78 Headphone radio GARMIN GTR 200 intercom wiring diagram 315 Figure 79 Headphone radio GARMIN GTR 225 intercom wiring d...

Страница 18: ...ing definitions apply to warnings cautions and notes as used in this aircraft maintenance manual Indicates an action necessary to prevent injury or death Indicates an action necessary to prevent damag...

Страница 19: ...1 GENERAL This section provides general information capacities and general procedures and specifications 1 GENERAL 1 1 DESCRIPTION The Airplane Factory Sling 4 is a four seat single engine tricycle f...

Страница 20: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 2 1 2 AIRCRAFT SPECIFICATIONS AND DATA 1 2 1 AIRCRAFT 3 VIEW DRAWING Note that dimensions in this drawing are in millimetres metric...

Страница 21: ...ect ratio 7 52 Dihedral 5 Tip washout 2 Aileron area 0 62 m 6 7 ft Flap area 1 26 m 13 6 ft HORIZONTAL STABILIZER Span 2 820 mm 9 252 ft Area 1 05 m 11 3 ft Aspect ratio with elevator 3 69 Angle of in...

Страница 22: ...R Wheel track 1 95 m 6 4 ft Wheel base 1 68 m 5 51 ft 1 2 3 AIRCRAFT WEIGHTS MAXIMUM WEIGHTS Maximum take off weight 920 kg 2028 25 lb Maximum landing weight 920 kg 2028 25 lb Maximum baggage weight 3...

Страница 23: ...d cooling water cooled heads and air cooled cylinders twin carburettors and integrated reduction gearbox with torque damper Maximum power 85 85 kW 115 hp at 5 800 rpm maximum 5 minutes 74 6 kW 100 hp...

Страница 24: ...fluids NOTE AVGAS 100LL places greater stress on the valve seats due to its lead content and forms increased deposits in the combustion chamber and lead sediments in the oil system Thus it should only...

Страница 25: ...3 litres 6 34 pints BRAKE FLUID Grade type Automatic Transmission Fluid ATF AIR FILTER OIL Type K N filter oil spray or K N filter oil GLUE FUEL FUEL TANK SEALANT FUEL LEAK REPAR Type AMSS8802 Class...

Страница 26: ...in the centre of wing MIL G 3278 type grease or equivalent Flap torque tube supports Q20 or equivalent Flap actuator ends MIL G 3278 type grease or equivalent Rudder pedal bushes Q20 or equivalent Co...

Страница 27: ...rim motor installation screws Propeller extension bolts securing propeller hub assembly to the propeller extension VHF antenna retaining screws Instrument panel retaining screws Navigation light retai...

Страница 28: ...4 37 5 to 41 7 5 8 NOTE Torque values in above table are for dry not oiled threads 1 5 2 SPECIFIC ITEM TORQUE VALUE Nm ft lb Wing mounting bolts front AN7 55 40 566 Wing mounting bolts rear AN5 18 13...

Страница 29: ...peed Indicator analogue WARNING LIGHTS AND INDICATORS Alternator Charge Warning Light MGL EFIS Warning Light Turbocharger Warning Lights x2 CONTROLS Dual Control Sticks Dual Rudder Pedals Centre Posit...

Страница 30: ...he aircraft can be steered using the rudder pedals with a capable person in the cockpit or for sharp turns by lowering the tail to raise the nose wheel off the ground In this case press down on the re...

Страница 31: ...he wheel strut so as to prevent slippage If it is necessary to lift the nose gear the engine cowling should be removed and the aircraft lifted using the engine mount as the attachment point The nose w...

Страница 32: ...ie down to ground anchors at the outer wing 1 and rear fuselage 2 tie down points Aircraft tie down is essential in severe weather and high wind conditions In such conditions it is also preferable to...

Страница 33: ...calibrated torque wrench with adequate range and the correct size as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 f...

Страница 34: ...irit water or electronic level with second row of rivets down from below the canopy frame edge on the aircraft fuselage side above the wing Figure 1 Longitudinal leveling reference position 2 Adjust t...

Страница 35: ...calibrated torque wrench with adequate range and the correct size as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 fo...

Страница 36: ...ph 4 3 2 1 3 Place a spirit water or electronic level across the top of the centre carry through spar from one side to the other and at right angles to the longitudinal axis of the aircraft Figure 2 T...

Страница 37: ...skin overlays the trailing edge skin B The 12 o clock position on the front face of the engine s propeller flange i e the top of the front face of the engine s propeller flange To get access it is nec...

Страница 38: ...TOLERANCE UP LEFT DOWN RIGHT Ailerons Starting from the tips lined up with the wing tips 22 22 3 Elevator Starting from the horn lined up with the leading edge 28 20 2 Trim tab Starting flush with ele...

Страница 39: ...1 15 1 RUDDER CABLE TENSION ADJUSTMENT Refer to paragraph 4 2 2 5 1 15 2 ELEVATOR ADJUSTMENT Refer to paragraph 4 2 1 5 1 15 3 ELEVATOR TRIM TAB ADJUSTMENT Refer to paragraph 4 2 1 6 1 15 4 AILERON A...

Страница 40: ...be performed according to the following schedule Upon completion of manufacture and before the first flight Whenever new equipment is fitted or a modification is done which influences the weight of th...

Страница 41: ...Y WEIGHT CENTRE OF GRAVITY TABLE ITEM WEIGHT kg lb ARM mm inch MOMENT weight x arm AIRCRAFT EMPTY CG Right Main Wheel WR LR 2 236 mm 88 032 Left Main Wheel WL LL 2 236 mm 88 032 Nose Wheel WN LN 548 m...

Страница 42: ...ove list is not necessarily a complete list of all required tools and equipment needed A calibrated torque wrench with adequate range and the correct size as implied by the above tool list accessories...

Страница 43: ...e aircraft must be weighed in a level attitude 11 Position the scales under each tyre or a scale under one tyre and blocks under the remaining tyres 12 In the case where one scale and two blocks are u...

Страница 44: ...sh do not use polishing detergents Original or equivalent corrosion prevention if used must be re applied after any alteration or repair If any trace of corrosion is detected it should be removed as s...

Страница 45: ...ectrolyte Leave the chromic acid solution on the part for at least five minutes and then remove the excess with water or a damp cloth Apply protective finish the same day in which treatment begins CAB...

Страница 46: ...Remove the fuel completely from the tanks lines and carburettor bowls Ethanol based fuel should not be stored in the tanks or carburettors for extended periods Clean the aircraft thoroughly Clean any...

Страница 47: ...IRCRAFT TO SERVICE Inspect tyres for proper inflation refer to paragraph 1 7 Inspect battery for general condition and charge If necessary charge the battery according to the battery manufacturer s in...

Страница 48: ...filter 90 Mesh filter EN FIL 005 X X 0 Airplane Factory part no Oil filter Rotax Rotax part no 825010 012 Nose wheel tyre 5 00 5 6 ply UN TYR 001 X A 0 Airplane Factory part no Main wheel tyre 15 00...

Страница 49: ...ever is located on the central tunnel between the two front seats and is indicated by a BRAKE label PARKING BRAKE VALVE The park brake shutoff valve is located to the rear of the central tunnel betwee...

Страница 50: ...h breaker is individually labelled FLAPS The flap control is located on the instrument panel and is labelled FLAPS Flap positions are labelled as UP 1 2 and 3 from top of controller to bottom IGNITION...

Страница 51: ...sole and is labelled OFF LEFT and RIGHT indicating selection The selector lever is labelled FUEL ELECTRIC FUEL PUMPS The electric fuel pumps are activated by switches on the upper left of the instrume...

Страница 52: ...the nose wheel fairing is a placard 102 mm x 9 mm indicating tyre pressure 1 8 bar IDENTIFICATION PLATE The following stainless steel placard is located on the central console inside the aircraft cab...

Страница 53: ...OPERATE UNDER VMC ONLY MAXIMUM PERMISSIBLE AIRSPEED 135 KIAS MAXIMUM PERMISSIBLE RPM 5 800 RPM FOR 5 MINUTES MAXIMUM CONTINUOUS RPM 5 500 MAXIMUM PERMISSIBLE MASS 920 KG 2 024 LB WARNING NON TYPE CER...

Страница 54: ...n an aircraft Wear protective eye wear when working on an aircraft especially when inflating or deflating tyres working with power tools with fluids or when working with pressurized air equipment Alwa...

Страница 55: ...tyre It is advisable to inflate the tyre on a newly assembled wheel assembly in a cage built for that purpose Spilled hydraulic fluid brake fluid and fuel represent a safety hazard Blank off disconnec...

Страница 56: ...ling 4 for flight these should be emailed to sales airplanefactory co za The following information should be included in the email Aircraft make model and serial number Engine make model and serial nu...

Страница 57: ...ion of panel covers ribs frames stringers etc absence of cracks deformation rivet slackening corrosion and any other apparent sign s of damage CABLES AND PUSHRODS Inspect cables for broken strands kin...

Страница 58: ...form of collapse chafing proper radius any form of deterioration security of attachment corrosion of fitments couplings In addition to the above metal fluid lines tubing should be free of dents FILTER...

Страница 59: ...uit breakers BATTERY Inspect for security of attachment correct rating sufficient charge physical integrity leakage and cracks Inspect the battery terminal connections for security of attachment crack...

Страница 60: ...the cabin Small round tail cone side holes provides access to the elevator control horn and pushrod end The vertical and horizontal tail nacelle fairings provide access to vertical and horizontal tai...

Страница 61: ...LLER Comply with inspection schedule as indicated in the latest revision of the propeller operator s manual 2 3 3 AIRFRAME AND SYSTEMS The airframe and systems inspection schedule is as follows Inspec...

Страница 62: ...of failure and defective or insecure attachment of fittings 2 Inspect systems and components for improper installation apparent defects and unsatisfactory operation 2 4 3 CABIN AND COCKPIT GROUP 1 In...

Страница 63: ...tachment 8 Inspect accessories for apparent defects in security of mounting 9 Inspect all systems for improper installation poor general condition defects and insecure attachment 10 Inspect electrical...

Страница 64: ...components and systems for 1 General condition 2 Skin deterioration 3 Distortion 4 Evidence of failure 5 Insecurity of attachment 6 Improper component installation 7 Improper component operation 2 4 8...

Страница 65: ...correct operation and functionality 2 Inspect wiring and conduits for improper routing insecure mounting and obvious defects 3 Inspect bonding and shielding for improper installation and poor conditi...

Страница 66: ...e mounts Inspect engine mount for any signs of distortion or cracks Fuel pumps and hoses Verify fuel pump assembly securely attached to firewall Electrical wire connections to pumps in fuel pump assem...

Страница 67: ...opens and close correctly Engine air intake system Verify the security of the clamps and the security and integrity of the air hoses from the intake air distributor air box to the carburettors Visual...

Страница 68: ...ery earth on firewall Verify security of starter solenoid mounting lock nuts and wires wire terminals Verify presence and integrity of wire boots on terminals Verify security of all transducers sensor...

Страница 69: ...seat Electrical and avionics Verify correct operation of alternator charge light Verify security of landing taxi and navigation strobe light connectors connections iBOX electrical wires and connector...

Страница 70: ...lve to filters Verify security of fuel hoses from filters to tanks Verify correct and unobstructed fuel hose routing Verify correct fuel selector valve operation Verify security of fuel selector valve...

Страница 71: ...rity and security of lateral torque tube mounting brackets and integrity and security of bushes and locking rings Control arms horns securely riveted to lateral torque tubes Pushrods correctly adjuste...

Страница 72: ...n on panel Slip indicator balance ball air bubble not visible Magneto switch guard in place if separate magneto switches Instrument markings correct Altimeter indicates correctly with QNH QFE set All...

Страница 73: ...eron system pushrod lock nuts secure Aileron system rod ends free at full deflections Verify pitot tube security Verify correct operation of pitot tube Security of navigation lights and lens integrity...

Страница 74: ...m motor electrical connector and wiring Trim tab hinge secure Trim tab pivot secure split pin present Pushrod locked Verify operation Trim tab adjusted correctly deflections correct Rudder Correct def...

Страница 75: ...e the FAA Advisory Circular AC43 13 1B Acceptable Methods Techniques and Practices Aircraft Inspection and Repair Removed parts should be replaced with parts with the same part number from the same ma...

Страница 76: ...epair cracks dents and delamination as necessary FLUID LINES HOSES TUBES AND CONNECTIONS Fluid lines should be replaced with lines of the same part number material size inner and outer diameter pressu...

Страница 77: ...y wire is installed in such a manner as to prevent the loosening of the part to which it is applied Where specified bolts and nuts should be torqued to the indicated value Use a calibrated torque wren...

Страница 78: ...Tyres should be inflated to the recommended pressures Incorrect inflation can cause excessive wear and tyre imbalance Tyres should be marked and indexed i e apply creep marks with the wheel rim to ena...

Страница 79: ...dures as stipulated in the latest revision of the propeller manufacturer operator s manual and or service instructions service letters and service bulletins as applicable GENERAL CONSIDERATIONS IN THE...

Страница 80: ...udder pedal bushes 100 Hours yearly 12 Control stick s 100 Hours yearly 13 Control stick torque tube bushes 100 Hours yearly 14 Nose gear support blocks 100 Hours yearly 15 Main wheel bearings 100 Hou...

Страница 81: ...sary Air filter Dusty environment 100 Hours Refer to paragraph 3 3 8 Remove and clean the air filter more frequently than the normal service period Replace if necessary Engine Oil Operating predominan...

Страница 82: ...recommended by coolant or engine manufacturer Drain and replace Fire extinguisher As indicated Service Ballistic parachute rocket 6 Years Service Ballistic parachute canopy 6 years Repack Muffler hea...

Страница 83: ...s as required Maintain proper tyre pressure If unusual tolerance is found along the transmission route of the elevator control system replace those parts displaying excessive wear 3 3 5 FIRST 25 HOURS...

Страница 84: ...ce manuals as applicable 3 3 7 EVERY 50 HOURS ANNUALLY The following service requirements should be complied with after every 50 hours of operation or on an annual basis whichever comes first Carburet...

Страница 85: ...st revision of the Rotax 914 UL operator and or maintenance manuals as applicable Brake fluid Verify the level of the brake fluid in the master cylinder located on the left upper side of the engine si...

Страница 86: ...on describes the various structures substructures systems and subsystems comprising the aircraft and describes maintenance procedures applicable to these structures substructures systems and subsystem...

Страница 87: ...the wing one providing access to the aileron bellcrank and the other providing access to the flap control arm attached to the flap torque tube Fore and aft inspection panels are located on the undersi...

Страница 88: ...are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 577 As needed Fuel tank...

Страница 89: ...removed refer to paragraph 4 3 2 1 4 Remove the matting 5 Remove the inspection panelling by unfastening the button head screws retaining them 6 Remove the wing to fuselage fairings by unscrewing all...

Страница 90: ...which would prevent the wing side wiring from moving free of the aircraft when the wing is moved away 11 Disconnect the flap torsion bar connector 7 from inside the fuselage by removing the two AN3 bo...

Страница 91: ...he centre spar Take care not to damage the pushrod and torsion bar as they exit the fuselage PROCEDURE INSTALLATION 1 Reverse the above procedure removal for reinstallation paying close attention to t...

Страница 92: ...correct placement of washers refer to Figure 7 and note that the bolt is installed with its head facing the nose of the aircraft Figure 7 Aileron pushrod to control stick connection A AN5 10A bolt B...

Страница 93: ...ables pneumatic tubes which may cause chaffing 5 Before flight verify alignment and free and correct travel for the ailerons and flaps Refer to paragraph 1 13 6 Ensure that no loose objects foreign ma...

Страница 94: ...heet metal skin without a spar An aluminium tube running inside the leading edge serves as a balancing weight Aileron hinges on the aileron side comprise of sealed ball bearings pressed into shaped pl...

Страница 95: ...ERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Inspection panel screws The above list is not necessarily a complete list of all material needed Refer to the Sling...

Страница 96: ...bellcrank 1 inspection cover 2 from the underside of the wing 2 Support the aileron and unfasten and remove the bolt 3 securing the pushrod 4 to the bellcrank 3 Support the aileron and unfasten and re...

Страница 97: ...reuse lock nuts Fit new Tighten the lock nut on the bolt through the inboard aileron hinge sufficiently observe the correct placement of washers refer to Figure 9 and note that the bolt is installed...

Страница 98: ...bserve the correct placement of washers refer to Figure 10 and note that the bolt is installed with its head facing the wingtip Figure 10 Aileron hinge outboard A AN4 7A bolt B AN4 washer 0 8 mm 0 032...

Страница 99: ...sure that with the control column vertical the aileron trailing edge is aligned with wing trailing edge and that the aileron bellcrank is in the neutral position i e the inside arm the arm closest to...

Страница 100: ...etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Inspe...

Страница 101: ...inspection panel s under the wing s 4 Ensure that the control sticks move freely left and right If the roll autopilot servo is attached it will create some resistance Without it attached the control s...

Страница 102: ...to the pushrod 4 and lines up exactly with the edges of the inspection hatch Use a straight edge to help with alignment Figure 13 Aileron adjustment wing side 9 Tighten the lock nuts at both ends of...

Страница 103: ...Page 85 14 Paint orange creep marks on the pushrod lock nuts 15 Ensure that no tools and or foreign materials remain in the wing and under the seats 16 Apply thread locking sealant to the inspection p...

Страница 104: ...TITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Inspection panel screws 3 Loctite 243 As needed Servo mounting screws 4 Tie wraps As needed The above list is not necessarily a complete lis...

Страница 105: ...the bolt 1 connecting the servo 2 control arm to the pushrod 4 Unscrew the screws retaining the connector 3 to the servo and disconnect it 5 Undo the screws 4 retaining the servo to the fuselage struc...

Страница 106: ...cable does cannot chafe against airframe parts 2 Ensure the applicable aircraft control s is are free and does not bind with the servo installed 3 Follow any applicable procedures in the latest revisi...

Страница 107: ...tube arm s and remove the pushrod INSTALLATION 1 Reverse the above procedure removal paying close attention to the following Inspect all bolts nuts and screws for damage Replace if necessary Do not re...

Страница 108: ...ure 16 The flap control system is push pull type with a linking torque tube torsion bar An actuator motor is installed in the centre channel between the front seats It controls an arm attached to a to...

Страница 109: ...REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Inspection panel screws Option2 only The above list is not necessarily a complete list of all material needed Refer to th...

Страница 110: ...ers with the exception of lock washers for reassembly 1 Extend the flaps fully 2 Disconnect the bolt 1 attaching the flap pushrod 2 the flap 3 3 Support the flap and remove the bolts washers and lockn...

Страница 111: ...f necessary Do not reuse lock nuts Fit new Tighten the lock nuts on the bolts through the flap hinges sufficiently observe the correct placement of washers refer to Figure 17 and note that the bolts a...

Страница 112: ...t of washers refer to Figure 18 and note that the bolt is installed with its head facing the wingtip Figure 18 Flap pushrod to flap connection 2 Verify the flap for alignment and correct travel refer...

Страница 113: ...1 Remove the flap inspection cover 1 from the underside of the wing 2 Support the flap and disconnect the bolt 2 connecting the flap pushrod 3 to the flap torque tube 4 control arm 3 Support the flap...

Страница 114: ...hten the lock nut on the bolt through the flap pushrod rod end bearing sufficiently observe the correct placement of washers refer to Figure 19 and note that the bolt is installed with its head facing...

Страница 115: ...so in accordance with national legislation This is the responsibility of the aircraft owner and any person who is to perform any maintenance on the aircraft PROCEDURE The procedure is identical for t...

Страница 116: ...turning the pushrods 9 Paint orange creep marks on the pushrod lock nuts 10 Verify before flight correct travel for the flap refer to paragraph 1 13 11 Ensure that no foreign material or tools remain...

Страница 117: ...nspection panel screws 3 Tie wraps As needed Actuator cable The above list is not necessarily a complete list of all material needed Refer to the Sling 4 construction manual AUTHORISED PERSONNEL Any p...

Страница 118: ...actuator motor s signal cable plug Disconnect the plug Remove tie wraps where necessary 3 Remove the central console panel next to the front seat by loosening the button head screws retaining it 4 Ope...

Страница 119: ...f washers refer to Figure 21 Figure 21 Flap actuator motor installation 2 Tie wrap the cable where necessary 3 Verify alignment and correct flap movement refer to paragraph 1 13 before closing up the...

Страница 120: ...re with front and rear spars The elevator has a similar structure though with only a front spar Bearings are again as with all other control surface bearings inch sealed bearings Elevator horns carry...

Страница 121: ...rol system Refer to Figure 23 The elevator control system is push pull type controlled from the cabin via the control columns Control is transmitted through a push pull rod and bellcrank arrangement A...

Страница 122: ...NSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed The above list is not necessarily a complete list of all material needed Refer to the Sling 4 construction manual AUTHORISED PER...

Страница 123: ...sconnect the elevator pushrod from the elevator control horn located inside the rear fuselage tail cone The pushrod rod end bearing is accessed through the two small round access holes on the left and...

Страница 124: ...cessary Do not reuse lock nuts Fit new Tighten the lock nut on the bolt through the elevator pushrod rod end bearing sufficiently observe the correct placement of washers and note that the bolt is ins...

Страница 125: ...one The bolt in the centre hinge is fitted with its head towards the larger clearance side of the elevator cut out Figure 25 Horizontal stabilizer to elevator hinge Tighten the lock nut on the bolt th...

Страница 126: ...pplicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed The above list is not necessarily a complete list of all material needed Re...

Страница 127: ...e exception of lock washers for reassembly 1 Remove the vertical stabilizer Refer to paragraph 4 2 2 3 2 Disconnect the trim tab motor cable connection plug 1 3 Support the horizontal stabilizer and u...

Страница 128: ...use lock nuts Fit new Tighten the lock nuts sufficiently observe the correct placement of washers refer to Figure 26 and note that the bolts are installed with the bolt heads head facing to the nose o...

Страница 129: ...queing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 2 4 mm Heat shrink As needed 2 6 4 mm Heat shrink As needed 3 Solder As need...

Страница 130: ...ack wire aircraft side to ease later reconnection 3 Remove the split pin from the trim tab pushrod connected to the motor push out the pin and washer and disconnect the pushrod from the servo 4 Unscre...

Страница 131: ...the black and white wires on the aircraft side to the white wires on the trim motor side Activate the trim motor and observe the direction of travel If incorrect reverse the two wire connections White...

Страница 132: ...to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Inspection panel screws The above list is not necessarily a complet...

Страница 133: ...front panel Figure 27 Elevator adjustment 4 Hold the elevator in line with the horizontal stabilizer Put an inclinometer on it and zero the inclinometer 5 Undo the lock nuts and adjust pushrods 4 and...

Страница 134: ...ISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 116 9 Apply thread locking sealant to the inspection cover screws before fitment Do not over tighten 10 Verify correct travel and full and free movement...

Страница 135: ...cessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Split pin 1 The above list is not n...

Страница 136: ...b horn 5 6 Adjust the eye bolt on the threaded rod temporarily reattach to the trim tab horn and measure the trim tab deflection downwards relative to the elevator upper surface use a protractor or me...

Страница 137: ...TEM QUANTITY NOTES 1 Tie wraps As needed 2 Orange paint As needed 3 Loctite 243 As needed Servo mounting screws The above list is not necessarily a complete list of all material needed Refer to the Sl...

Страница 138: ...to paragraph 4 3 2 2 2 Undo the bolt 1 connecting the control arm of the servo 2 to the pushrod 3 3 Undo the screws 4 retaining the servo to the bracket 5 Carefully pull the motor from the bracket It...

Страница 139: ...curing screws If applicable secure the servo cable to the aircraft frame with tie wraps in the manner it was before removal using spacers as applicable Apply thread locking sealant to the servo mounti...

Страница 140: ...ion of lock washers for reassembly REMOVAL 1 If the servo is not already disconnected removed undo the bolt and nut connecting the pushrod to the servo arm Undo the bolt and nut retaining the pushrod...

Страница 141: ...win spars 5 with wrap around stressed skin panelling An attachment plate secures the vertical stabiliser s front spar to a bracket attached to the penultimate tail cone rib The rudder consists of a sp...

Страница 142: ...terminate on two rudder pedal control horns Control stops limit movement of the pedal to cable attachment horns These horns are in turn attached to two adjustable pushrods which are attached to a con...

Страница 143: ...if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed The above list is not necessarily a complete list of all material need...

Страница 144: ...dder control horn 2 2 Push and retain the rudder to one side to gain easier access to the rudder hinges 3 Support the rudder and loosen and remove the hinge bolts 4 Carefully and slowly pull the rudde...

Страница 145: ...not reuse lock nuts lock washers or split pins as applicable Fit new Tighten the lock nuts on the bolts through the rudder hinges sufficiently observe the correct placement of washers refer to Figure...

Страница 146: ...washers refer to Figure 33 and note that the bolts are installed with their heads facing upwards Figure 33 Rudder cable connection 2 Apply orange creep marks to the bolts nuts 3 Verify for alignment...

Страница 147: ...er to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Fairing screws The above list is not necessarily a complete list...

Страница 148: ...k washers as applicable for reassembly 1 Remove the rudder refer to paragraph 4 2 2 2 2 Remove the empennage to fuselage fairing 1 by unscrewing the button head screws retaining it 3 Remove the side p...

Страница 149: ...he fuselage Note that the six bottom bolts in the rear support screw into anchor nuts attached to the fuselage Figure 34 Vertical stabilizer to fuselage connection 6 Carefully lift the vertical tail c...

Страница 150: ...pins as applicable Fit new Observe the correct placement of washers refer to Figure 34 Tighten the lock nuts on the bolts retaining the vertical stabilizer sufficiently and note that the front mounti...

Страница 151: ...ragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legislation This is the...

Страница 152: ...Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Inspection panels screws The above list is not necessarily a...

Страница 153: ...ere must be a minimum of a 3 mm clearance to the bolt heads otherwise the rudder could get jammed 5 Undo the bolts 1 retaining the springs 2 to the fuselage remove the bolts and washers and free the e...

Страница 154: ...der is straight the cable stops 4 are hard against the angled brackets Tighten the screws 11 Verify that with the rudder centred there is only a very slight tension on the rear part of the rudder cabl...

Страница 155: ...gers carry through to the centre fuselage for strength and rigidity Supporting brackets for the vertical and horizontal stabilisers are attached to the rear formers at the tail section A cross brace w...

Страница 156: ...SEAT REMOVAL AND INSTALLATION AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legislation This is the...

Страница 157: ...cut out towards the nose of the aircraft to release operate the catch mechanism securing the seat to the aircraft 2 Slide the seat clear of its railings and carefully lift the seat clear of the aircra...

Страница 158: ...ied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of...

Страница 159: ...t s to the fuselage 2 Undo the three Dzus fasteners passing through three eyelets 2 retaining the seat assembly to the baggage compartment floor Remove the seat PROCEDURE INSTALLATION 1 Inspect the Dz...

Страница 160: ...dequate quantity of detergents suitable for polymethyl methacrylate Perspex Use a soft clean cloth sponge or deerskin 4 3 2 4 UPHOLSTERY CLEANING Upholstery and covers may be removed from the cockpit...

Страница 161: ...ccommodates the engine mount engine and firewall forward firewall mounted equipment and engine cowling Refer to paragraph 14 for a schematic showing the equipment and their positions mounted on the fi...

Страница 162: ...struts Suspension is provided by the flexibility within the struts which is attached transversely via a channel 3 designed for purpose in the lower centre fuselage Wheels 4 are cantilevered on the ma...

Страница 163: ...tc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Fairing screws 2 Loctite 243 As...

Страница 164: ...e support plate and hold the inner and outer fairing sections to one another 2 Support the outside fairing half 3 and unfasten the retaining bolt 4 Remove the fairing half bolt and washers 5 PROCEDURE...

Страница 165: ...by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Split pin...

Страница 166: ...fasten the two bolts 1 holding the brake callipers together and remove the rear towards the wheel calliper assembly 2 which will come away in two parts 3 4 Remove the split pin 4 and pull out the spac...

Страница 167: ...he wheel bearings Replace if necessary Grease the bearings before installation refer to paragraph 4 4 1 5 Tighten the brake caliper retaining nuts sufficiently Do not over tighten 2 To tighten the ret...

Страница 168: ...mplied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 577 As needed Brake line fitt...

Страница 169: ...ption of lock washers for reassembly 1 Remove the wheel fairing refer to paragraph 4 4 1 1 2 Remove the wheel refer to paragraph 4 4 1 2 3 Ensure that the aircraft cannot roll move if only one wheel j...

Страница 170: ...PROCEDURE INSTALLATION 1 Reverse the above procedure for reinstallation paying close attention to the following Inspect all bolts nuts and screws for damage Replace if necessary Do not reuse lock nut...

Страница 171: ...DC MAM 001 X C 2 Page 153 A B C Main undercarriage strut Main wheel fairing mounting bracket Figure 37 Main wheel axle installation A AN4 22A bolt B AN4 washer 1 6 mm 0 063 C AN4 lock nut Nyloc Refer...

Страница 172: ...by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange pai...

Страница 173: ...done correctly the wheel could be out of balance after assembly 3 Deflate the tyre completely 4 Unfasten the bolts 1 retaining the brake disc 2 to the brake disc spacer 3 to separate the brake disc fr...

Страница 174: ...ciently Take care not to catch the inner tube between the two hub halves 4 Inspect the o ring for damage Replace if necessary 5 Push the wheel to one side of the assembled wheel hub slip the o ring ov...

Страница 175: ...needed Refer to the Sling 4 construction manual AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legi...

Страница 176: ...eeded Undercarriage channel cover plate 4 3 2 mm x 8 mm Aluminium blind rivets multi grip As needed Undercarriage channel cover plate 5 Glue PRATLEY QUICKSET CLEAR As needed To glue brake line s into...

Страница 177: ...4 4 1 3 Retain any bolts nuts except lock nuts spacers screws and washers with the exception of lock washers for reassembly 1 Hoist the aircraft onto supports If necessary balance the sideways moveme...

Страница 178: ...e fuselage cover plates between the wings and the centre fuselage 8 Drill out the rivets retaining the main gear cover plate on the bottom aircraft fuselage 9 Support the main gear assembly and undo a...

Страница 179: ...ct value refer to paragraph 1 5 2 observe the correct placement of washers refer to Figure 38 and note that the bolts are installed with the bolt heads head facing towards the rear of the aircraft App...

Страница 180: ...rk 4 supporting an axle bolt 5 The front wheel 6 is not fitted with a braking mechanism Steering motion is transmitted from the rudder pedal control horns through two adjustable pushrods attached to t...

Страница 181: ...Refer to the Sling 4 construction manual AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legislation...

Страница 182: ...ool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed T...

Страница 183: ...f lock washers for reassembly 1 Remove the nose wheel fairing Refer to paragraph 4 4 2 1 2 Lift and support the front of aircraft in such a manner as to lift the nose wheel off the ground 3 Unfasten t...

Страница 184: ...rve the correct placement of washers and bushes and the correct orientation of the nose wheel refer to Figure 40 Note that the lock nut faces the starboard side of the aircraft Figure 40 Nose wheel in...

Страница 185: ...ool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed T...

Страница 186: ...ng mount assembly 6 Remove the valve cap 1 To separate the inner tube tyre and o ring from the hubs carefully pull the two hub halves apart taking care not to damage the valve stem as it pulls out of...

Страница 187: ...one side of the assembled wheel hub slip the o ring over the other side of the assembled wheel hub and into place in the groove between the two hub halves 7 Inflate the tyre to approximately 2 5 Bar...

Страница 188: ...efer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legislation T...

Страница 189: ...THORISED PERSONNEL The above list is not necessarily a complete list of all required tools and equipment needed A calibrated torque wrench with adequate range and the correct size as implied by the ab...

Страница 190: ...ts 3 and washers on the bottom nose gear to engine mount attachment 4 Remove the two brackets 5 5 Support the nose gear loosen the bolts 6 and remove the bolts and washers the spacer 7 and the bearing...

Страница 191: ...sary Do not reuse lock nuts Fit new Tighten the lock nuts sufficiently observe the correct placement of washers and bearings refer to Figure 42 and note that the bolts are installed with the bolt head...

Страница 192: ...owling Refer to Figure 43 The engine cowling is made up of moulded fibreglass upper 1 and lower 2 parts Inspection panels 3 are located in the top cowling and are secured down by two Dzus fasteners Th...

Страница 193: ...aragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legislation This is th...

Страница 194: ...g along the upper edge of the firewall 3 Once all Dzus fasteners are loose remove the front and then side fasteners from their seating holes prior to removing those over the firewall BOTTOM COWL 1 Rem...

Страница 195: ...N BOTTOM COWL 1 Reverse the above procedure removal to install the bottom cowl paying close attention to the following Ensure that the four catches next to the radiators are properly latched Tighten t...

Страница 196: ...nchronisation no other carburettor adjustment is required Refer to the carburettor synchronization procedure in the latest revision of the Rotax 914 UL engine operator s and or maintenance manuals as...

Страница 197: ...ensure that there is no residual oil in the crank case Oil is pumped back to the oil reservoir by performing the following procedure Master switch ignition switches OFF Remove the oil reservoir cap R...

Страница 198: ...IRED ITEM QUANTITY NOTES 1 Safety wire As needed 2 Split pin 1 Only if in need of replacement The above list is not necessarily a complete list of all material needed Refer to the Sling 4 construction...

Страница 199: ...ke pipe clamp 3 2 Loosen the clamp 4 securing the air filter to the air intake manifold turbocharger 5 opening 3 Loosen the clamp securing the air filter housing to the air intake pipe from the cowlin...

Страница 200: ...closure is clean and dry on the inside Ensure that the seating area for the air filter enclosure on the air intake manifold is dry and clean Ensure that the air filter enclosure coupling to the air in...

Страница 201: ...essories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or a...

Страница 202: ...the air pipe 2 to the assembly shroud 3 3 Loosen and remove the ring clamp 4 retaining the exhaust pipe to the engine mount Undo and remove the bolts 5 retaining the assembly to the turbocharger Loos...

Страница 203: ...lied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Alumi...

Страница 204: ...rs for reassembly 1 Remove the heat exchanger muffler assembly refer to paragraph 5 2 8 2 Drill out the line of rivets 1 clamping the shroud 2 plate together Loosen the clamps 3 clamping the shroud to...

Страница 205: ...queing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accor...

Страница 206: ...ool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 577 As needed Oi...

Страница 207: ...ds of couplings 1 and 2 and fit into the radiator 3 2 Slip a two ear clamp 4 over each pipe 5 slip the pipes over the couplings 2 and move the two ear clamps into position 3 Crimp the two ear plugs 4...

Страница 208: ...1 Drain fluids as required 2 Remove the two ear clamps refer to paragraph 15 1 and pull the pipes from the fittings 3 Blank off oil pipes if to be unconnected for a substantial period of time to preve...

Страница 209: ...plied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Safety wire As needed The above list is not necessarily a compl...

Страница 210: ...the pipes 3 Use safety wire and secure the insulation blanket s around the pipe s 4 Inspect for security of attachment PROCEDURE DISCONNECTION 1 Drain fluid as required 2 Remove the safety wire securi...

Страница 211: ...ize as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOT...

Страница 212: ...tation Retain any bolts clamps spacers screws and washers with the exception of lock washers for reassembly 1 Support the tail of the aircraft adequately before removing the engine 2 Remove the propel...

Страница 213: ...ct the fuel return line from the engine Blank off to prevent drip and or spillage 8 Disconnect the throttle cables from the carburettors 9 Disconnect the choke cables from the carburettors 10 Disconne...

Страница 214: ...t exchanger muffler assembly by undoing the clamp or at the firewall 16 Cut any all tie wraps securing pipes connected to the engine and electrical cabling connected to the engine to the engine mount...

Страница 215: ...rudder pedals to the nose gear must be disconnected first and the aircraft must be supported adequately in preparation of the absence of the nose gear In this case the exhaust need not be disconnected...

Страница 216: ...e installed with the bolt heads facing forward The bottom bolts are installed with the bolt heads facing backward Observe correct placement of washers spacers bushes and vibration dampers refer to Fig...

Страница 217: ...ion of electrical wiring 6 Inspect for adequate operating fluid levels in engine Replenish if necessary 7 Inspect all cables electrical wiring and piping for security of attachment 8 If the waste gate...

Страница 218: ...achment of the Bowden cable to the carburettor throttle control lever and adjustment refer to the latest revision edition of the Rotax 914 UL engine installation manual and maintenance manuals as appl...

Страница 219: ...ling 2 construction manual AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legislation This is the re...

Страница 220: ...ol list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Split pin 1 2 Loctite 222...

Страница 221: ...rocedure removal paying close attention to the following Do not re use split pin Fit new Inspect castle nut and bolt for damage Replace if necessary 2 Adjust the throttle lever friction refer to parag...

Страница 222: ...on 5 3 1 GENERAL MAINTENANCE AND SERVICE Refer to and comply with the latest revision of the propeller operator s manual for service requirements and procedures 5 3 2 PROPELLER HUB AND PROPELLER EXTEN...

Страница 223: ...adequate range and the correct size as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PER...

Страница 224: ...the screws 1 retaining the spinner 2 to the spinner bulkhead 3 PROCEDURE INSTALLATION 1 Reverse the above procedure removal to install the spinner paying close attention to the following Inspect all b...

Страница 225: ...TED DIRECTLY TO ENGINE FLANGE LUGS SLIP RING DISC OR EXTERNAL ALTERNATOR DRIVE PULLEY FITTED BETWEEN ENGINE FLANGE AND PROPELLER EXTENSION M8 x 40 mm hex bolt Class 8 8 Apply thread locking sealant Lo...

Страница 226: ...ied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 243 As needed Bolts connecting p...

Страница 227: ...curing the propeller extension 2 to the engine flange 3 2 Slowly move the propeller assembly away from the engine flange until the signal wire connections 4 are exposed Disconnect the signal wires 3 A...

Страница 228: ...the spinner dome for security of attachment Inspect the balance weight bolt nut for security of attachment Carefully clean and dry the engine flange and propeller extension Ensure that no oil traces a...

Страница 229: ...during the installation procedure Apply electrical power and operate the propeller controls to verify correct operation 4 Before flight start and let the engine run for a few minutes operate the prop...

Страница 230: ...ller extension 2 2 Carefully and slowly pull the propeller away from the propeller extension 2 until the signal wire connectors are exposed Disconnect the wires REMOVING AT ENGINE FLANGE SIDE WITH PRO...

Страница 231: ...efore doing so use coloured stickers or paint to mark the connection of the coloured signal wires to the disc terminals connections or place an alignment mark on the propeller extension and slip ring...

Страница 232: ...any signs of damage Inspect the spinner dome for security of attachment Inspect the balance weight bolt nut for security of attachment Carefully clean and dry the engine flange propeller extension and...

Страница 233: ...r and before flight inspect for security of attachment of the propeller correct and secure attachment of the signal wires and for any damage which may have been incurred during the installation proced...

Страница 234: ...LATION WITH EXTERNAL ALTERNATOR FITTED The procedure is in general the same as that for the standard installation Note that a longer bolt is used to secure the propeller extension to the engine flange...

Страница 235: ...ories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As...

Страница 236: ...ion 3 and remove the propeller and spinner bulkhead 4 For further disassembly of the propeller assembly 2 refer to the latest revision of the propeller manufacturer operator s manual for the required...

Страница 237: ...assembly before tightening the bolts Observe washer placement refer to Figure 48 Torque the bolts securing the propeller assembly to the propeller extension to the correct value refer to paragraph 1 5...

Страница 238: ...ated panels The fuel outlet for each tank is located at the lowest point of the inboard sidewall of the tank A B A Left fuel tank F Rotax 914 UL engine B Right fuel tank G Fuel flow sensor C Fuel filt...

Страница 239: ...plits into two separate branches one for each carburettor A fuel pressure transducer H is connected to one fuel pipe branch and is connected to the EFIS via the RDAC unit A fuel flow transducer G is c...

Страница 240: ...ely 13 mm 8 mm 14 5 mm approximately 15 mm When tie wrapping fuel pipes to the engine mount other pipes or the aircraft structure to aid in routing security of attachment care should be taken that the...

Страница 241: ...if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Orange paint As needed 2 Loctite 222 As needed Inspection panel screws The above list is not...

Страница 242: ...ilters from the fuel lines and drain any remaining fuel in the lines into a container Replace the filters Note that the fuel filters are installed with the 90 elbow facing the nose of the aircraft 6 T...

Страница 243: ...ueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Inspection panel screws and four fuel selector unit ret...

Страница 244: ...he selector lever 3 to the selector valve unit Loosen the screw and remove slide off the lever 3 Loosen the four button head screws 4 retaining the plate 5 to the selector unit Push the unit towards t...

Страница 245: ...e only lines up one way with the holes in the selector unit aiding the correct orientation of the unit on installation For fuel selector port allocation and fuel hose fitting orientation refer to Figu...

Страница 246: ...ose fitting threads The above list is not necessarily a complete list of all material needed Refer to the Sling 4 construction manual AUTHORISED PERSONNEL Any person performing maintenance of any kind...

Страница 247: ...ALLOCATION A 8 mm From starboard tank feed B 8 mm To engine pumps feed C 8 mm From port tank feed D 6 mm To starboard tank return E 8 mm From engine return F 6 mm To port tank return A B C D E F RETUR...

Страница 248: ...BLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Safety wire and tie wraps 8 mmx 12 mm x 5 mm seal draft rubber strip As needed 2 Two ear clamps 15 mm 2 3 Tie wraps clear tubing As needed The above list is...

Страница 249: ...h the exception of lock washers for reassembly 1 Fuel selector in OFF position 2 Remove the cowlings refer to paragraph 5 1 1 3 Undo the button head screws 1 retaining the fuel pump assembly cover 2 s...

Страница 250: ...ull the fuel hoses from the pump frame connections 6 Drain excess fuel in the lines into a container Blank off any fuel lines to be left open for an extended time to avoid drip spillage and contaminat...

Страница 251: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 233 7 Undo the two clamps 11 retaining the pump assembly to the firewall bracket and remove the assembly Fuel Pump 11...

Страница 252: ...over button head screws excessively Ensure that the wires marked GND is connected to the terminals marked on the fuel pump connector blocks and that the wires marked MAIN PUMP and AUX PUMP are connect...

Страница 253: ...bracket 2 before fitting the assembly to the firewall 3 Before flight perform an engine ground run and verify correct operation of the fuel pumps and correct fuel flow and pressure After the engine ru...

Страница 254: ...es sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Two ear clamps 22 mm 2 Per pump 2 Two ear...

Страница 255: ...oses 2 connecting the fuel pump to the surrounding pipe framework 3 and remove the pump 4 from the pipe frame PROCEDURE INSTALLATION 1 Reverse the above procedure removal to install a fuel pump into t...

Страница 256: ...nstruction manual AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accordance with national legislation This is the responsibil...

Страница 257: ...ly a complete list of all material needed Refer to the Sling 4 construction manual AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do s...

Страница 258: ...ed completely by removing unscrewing the drain PROCEDURE REMOVAL 1 Unscrew the fuel drain from the wing Do not retain fibre washer 2 Drain fuel into suitable container PROCEDURE INSTALLATION 1 Observe...

Страница 259: ...fer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Inspection panel 2 Loctite 577 As needed Fuel tank outlet return line couplings The abov...

Страница 260: ...s of the wing s to access the fuel tank end rib s 2 Drain the fuel tank completely by removing the fuel drain refer to paragraph 6 8 3 Loosen the fuel line couplings 1 Move the fuel pipes out of the w...

Страница 261: ...tted with the edge with the single notch facing the top of the wing and the edge with two notches facing the rear of the wing Apply thread locking sealant to the fuel line couplings before fitting and...

Страница 262: ...e 57 Fuel sender installation into fuel tank A M4 x 16 mm hex head stainless steel bolt B M4 thin washer stainless steel plated C M4 Fibre washer D Sender sender bracket mounting plate E Cork mounting...

Страница 263: ...fer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Fuel fuel tank sealant As needed Refer to paragraph 1 4 2 100 x 2 5 mm tie wrap 1 The above list is not necess...

Страница 264: ...e to the terminal stud cut the tie wrap and unwind the signal wire from the bracket 2 3 Undo the screws 3 retaining the sensor 4 to the bracket 2 and remove the sensor 4 Mark the position of the float...

Страница 265: ...ntre of bent part of arm on the arm as was over the centre of the spindle of the removed sensor over the centre of the sensor spindle refer to Figure 58 Use the marks made during disassembly on the fl...

Страница 266: ...The range measured should be between 0 and 200 approximately 8 to 192 Measuring an open circuit with the float arm flush against any one of the stops indicates that the sensor wiper has moved of the...

Страница 267: ...list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircr...

Страница 268: ...angled mirror tool and small pencil flashlight light source to inspect the finger strainer on the fuel pick up Under no circumstances use a match flame or cigarette lighter flame or an open bulb to pr...

Страница 269: ...he required minimum instrumentation together with typical back up and additional instrumentation supplied with the aircraft The instrument panel in any particular aircraft may differ from that illustr...

Страница 270: ...nual propeller pitch control switch 3 Fuel pump switches 20 Ballistic parachute deployment handle 4 Charge warning light 21 Fuel selector valve handle 5 TCU boost warning light 22 Switches EFIS EFIS b...

Страница 271: ...bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Instrument panel retaining screws The above list is not neces...

Страница 272: ...ting screws before fitment INSTRUMENTS 1 Before installing any electrical instrument ensure that the master switch is OFF 2 When installing instruments follow the recommendations below Do not over tig...

Страница 273: ...rpose of determining aircraft angle of attack displayed on the EFIS Flexible plumbing connects the pitot tube and static ports to the pressure instruments being an analogue airspeed indicator altimete...

Страница 274: ...so in accordance with national legislation This is the responsibility of the aircraft owner and any person who is to perform any maintenance on the aircraft PROCEDURE 1 Ensure that all instruments th...

Страница 275: ...cordance with national legislation This is the responsibility of the aircraft owner and any person who is to perform any maintenance on the aircraft PROCEDURE 1 Ensure that all instruments that utilis...

Страница 276: ...onnect the pneumatic tubes lines from the applicable instrument s 3 Blow low pressure air into the tubes lines in the direction of the port and never towards the instrument to clear any possible obstr...

Страница 277: ...orqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Adhesive lined foam As needed If adhesive foam was removed with removal of...

Страница 278: ...sensor to the plate 4 and remove the unit 4 Alternatively mark the location of the sensor foam mounting block s footprint for later replacement in the same location and tear the unit attached to plate...

Страница 279: ...tools and equipment needed A calibrated torque wrench with adequate range and the correct size as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applica...

Страница 280: ...connections information for each socket headphone position 1 Reverse the above procedure removal for installation paying close attention to the following Observe the correct washer insulator placement...

Страница 281: ...if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Antenna mounting screws 2 Clear silicone As needed The above list is not...

Страница 282: ...LATION 1 Reverse the above procedure removal paying close attention to the following Inspect the mounting screws for damage before fitting Replace if necessary Ensure that the base of the antenna make...

Страница 283: ...mplied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Tie wraps As needed Installation The above list is not necessa...

Страница 284: ...Cut the tie wraps 1 retaining the antenna 2 to the bracket 3 Cut any tie wraps securing the cable e g to other cables and pull the cable through the rubber grommet 4 in the mounting bracket PROCEDURE...

Страница 285: ...vents are found on the left and right sides of the instrument panel each with a shut off valve that can be directed through 180 degrees The heating system is comprised of a heat exchanger on the exhau...

Страница 286: ...master cylinder and two disc brakes assemblies An intercept valve activates the parking brake Braking action is through a lever located on the cabin tunnel between seats The hydraulic circuit intercep...

Страница 287: ...ories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Brake fluid As needed Refer to paragrap...

Страница 288: ...p feeding from a reservoir filled with the correct brake fluid 4 Use the pump to pump brake fluid until it reaches the bottom of the brake fluid reservoir Tighten the nipple and remove the pipe 5 Top...

Страница 289: ...ndependently 1 Pull the brake lever to pressurise the system 2 Loosen the brake calliper nipple to allow the fluid to spurt out 3 Tighten the nipple and release the brake lever 4 Repeat steps 1 to 3 u...

Страница 290: ...eof must do so in accordance with national legislation This is the responsibility of the aircraft owner and any person who is to perform any maintenance on the aircraft PROCEDURE REMOVAL Retain any bo...

Страница 291: ...t is not necessarily a complete list of all required tools and equipment needed A calibrated torque wrench with adequate range and the correct size as implied by the above tool list accessories socket...

Страница 292: ...tached to the strut by the axle mounting bolts Undo the four axle bolts and nuts 5 to release the spat mounting plate 2 Remove the spat mounting plate 3 To obtain the second brake lining mounting plat...

Страница 293: ...use Inspect for damage and the formation of cracks which may have resulted from the riveting process Note that the caliper is fitted into plate 1 such that the grooved sides of the brass fixtures 3 in...

Страница 294: ...iBOX installation manual Figure 64 Electrical system overview A single phase alternator integral to the engine connected to a regulator rectifier mounted in the cabin supplies DC power to the main bus...

Страница 295: ...adio 7 Elevator and Aileron autopilot servos turbocharger waste gate servo 8 Flap actuator motor 9 Flap controller 10 Ignition systems 11 Landing and taxi light switches 12 Landing and taxi lights 13...

Страница 296: ...queing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any component thereof must do so in accor...

Страница 297: ...er switch OFF All other switches OFF 2 Thoroughly clean and dry the inside and outside of the battery bracket 3 Insert the battery into the bracket Ensure that the battery is inserted the right way ro...

Страница 298: ...ble Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Tie wraps 2 2 Loctite 222 As needed Instrument panel retaining screws The above list is not necessarily...

Страница 299: ...RE INSTALLATION 1 Reverse the above procedure removal paying close attention to the following Inspect all bolts nuts and screws for damage Replace if necessary The battery is installed with its positi...

Страница 300: ...plicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Instrument panel retaining screws The above list is not necessarily a complet...

Страница 301: ...sher 4 from the instrument panel 4 Slip the new washer 4 supplied with the circuit breaker over the circuit breaker threaded stub and inset the circuit breaker through the instrument panel Ensure that...

Страница 302: ...d the instrument panel when fitted 5 Ensure that the switch is inserted correct side up Align the switch body vertically and secure with the front nut 3 Do not over tighten PLEASE NOTE THAT IN CASES W...

Страница 303: ...as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing mainte...

Страница 304: ...assembly 1 Master switch OFF 2 Disconnect the connection plug 1 from the rectifier 2 3 Undo the bolts 3 retaining the rectifier and the ground wire 4 to the firewall Remove the rectifier PROCEDURE INS...

Страница 305: ...ding and taxi lights Strobe light 11 1 NAVIGATION LIGHTS Combined navigation and strobe lights are installed on the wing tips All navigation lights are controlled by a single switch located on the ins...

Страница 306: ...1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Navigation light retaining screws The above list is not necessarily a complete list of all material need...

Страница 307: ...move the light away from the wingtip until the wire connection plugs are revealed Disconnect Retain the rubber backing for reassembly PROCEDURE INSTALLATION 1 Reverse the above procedure for reinstall...

Страница 308: ...ue wrench with adequate range and the correct size as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values...

Страница 309: ...xi light switches in OFF positions 2 Undo the screws retaining the clear lens to the wing and remove the lens 3 Undo the button head screws 1 which secure the taxi 2 or landing 3 light and remove toge...

Страница 310: ...lf facing towards the top of the wing Figure 65 Landing and taxi light installation All connector connections must be covered by heat shrink see below Slide heat shrink over the wires before connectin...

Страница 311: ...essories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Tie wraps As needed The above list i...

Страница 312: ...e light to the angled plates 2 front plate 3 and ground wire 4 Cut tie wraps Remove the light PROCEDURE ASSEMBLY 1 Reverse the above procedure disassembly paying careful attention to the following Obs...

Страница 313: ...sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values AUTHORISED PERSONNEL Any person performing maintenance of any kind on the aircraft or any compo...

Страница 314: ...c are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED ITEM QUANTITY NOTES 1 Loctite 222 As needed Strobe light retaining screws The...

Страница 315: ...rom the rudder until the wire connection plugs are revealed Disconnect PROCEDURE INSTALLATION 1 Reverse the above procedure for reinstallation paying close attention to the following Inspect all bolts...

Страница 316: ...tem The system is designed to enable the pilot or passenger to deploy the parachute in case of emergency in such a manner that the aircraft structure is carried under the parachute to the ground on th...

Страница 317: ...nd the correct size as implied by the above tool list accessories sockets etc are implied for torqueing bolts nuts if applicable Refer to paragraph 1 5 for torque values CONSUMABLE MATERIAL REQUIRED I...

Страница 318: ...do the bolt retaining the lap strap to the fuselage and remove the belt strap 5 Drill out the rivets retaining the side cover plate to the fuselage and remove the cover plate to gain access to the ine...

Страница 319: ...DURE INSTALLATION 1 Reverse the above procedure for reinstallation paying close attention to the following Inspect all bolts nuts and screws for damage Replace if necessary Do not reuse lock nuts Fit...

Страница 320: ...y component thereof must do so in accordance with national legislation This is the responsibility of the aircraft owner and any person who is to perform any maintenance on the aircraft PROCEDURE REMOV...

Страница 321: ...DATE 2014 11 10 DC MAM 001 X C 2 Page 303 13 APPENDIX A AVIONICS AND ELECTRICAL SYSTEM WIRING DIAGRAMS 13 1 CHARGE AND START SYSTEM FUEL PUMPS WIRING DIAGRAM Figure 66 Charge and start system wiring...

Страница 322: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 304 13 2 SWITCHES AND CIRCUIT BREAKERS WIRING DIAGRAM Figure 67 Switches and circuit breakers wiring diagram...

Страница 323: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 305 13 3 EXTERNAL ALTERNATOR WIRING DIAGRAM Figure 68 External alternator wiring diagram...

Страница 324: ...UMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 306 13 4 FLAP SYSTEM WIRING DIAGRAM 13 4 1 MGL SP10 FLAP WITH 4 POSITION ROTARY SWITCH Figure 69 MGL SP 10 Flap trim controller wiring diagr...

Страница 325: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 307 13 4 2 INOTEC Figure 70 Flap system wiring diagram INOTEC...

Страница 326: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 308 13 4 3 E FLAPS Figure 71 Flap system wiring diagram E Flaps...

Страница 327: ...11 10 DC MAM 001 X C 2 Page 309 13 5 ELEVATOR TRIM MOTOR WIRING DIAGRAM 13 5 1 DUAL STICK TRIM Figure 72 Elevator trim motor wiring diagram dual control sticks RAY ALLEN G205 TYPE STICK GRIP SWITCH 1...

Страница 328: ...ION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 310 13 5 2 SINGLE STICK TRIM Figure 73 Elevator trim motor wiring diagram single control stick RAY ALLEN G205 TYPE STICK GRIP SWITCH 1 SWITCH 3 SWITCH 4 S...

Страница 329: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 311 13 6 EFIS SYSTEM COMMUNICATIONS BUS LAYOUT Figure 74 EFIS system communications bus layout...

Страница 330: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 312 13 7 AHRS AND COMPASS WIRING DIAGRAM Figure 75 AHRS and compass wiring diagram...

Страница 331: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 313 13 8 AUTOPILOT ROLL SERVO AND PITCH SERVO WIRING DIAGRAM Figure 76 Autopilot roll servo and pitch servo wiring diagram...

Страница 332: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 314 13 9 EFIS BACK UP BATTERY CHARGE CIRCUIT Figure 77 EFIS back up battery charge circuit...

Страница 333: ...REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 315 13 10 HEADPHONE RADIO INTERCOM WIRING DIAGRAM 13 10 1 GARMIN GTR 200 RADIO Figure 78 Headphone radio GARMIN GTR 200 intercom wiring diagram INTER...

Страница 334: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 316 13 10 2 GARMIN GTR 225 RADIO Figure 79 Headphone radio GARMIN GTR 225 intercom wiring diagram Circuit breaker on instrument panel...

Страница 335: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 317 13 11 POSITION NAVIGATION LIGHTS WIRING DIAGRAM Figure 80 Position navigation lights wiring diagram...

Страница 336: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 318 13 12 RDAC TO OIL PRESSURE TRANSDUCER WIRING DIAGRAM Figure 81 RDAC to oil pressure transducer wiring diagram and settings...

Страница 337: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 319 13 13 DUAL EFIS INSTALLATION WIRING DIAGRAM Figure 82 Dual EFIS installation...

Страница 338: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 320 13 14 TRANSPONDER WIRING DIAGRAM 13 14 1 TRIG TT21 TRANSPONDER WIRING DIAGRAM Figure 83 TRIG TT21 transponder wiring diagram XPOND...

Страница 339: ...DOCUMENT No REVISION 1 2 DATE 2014 11 10 DC MAM 001 X C 2 Page 321 13 14 2 SANDIA STX 165R TRANSPONDER WIRING DIAGRAM Figure 84 SANDIA STX 165R transponder wiring diagram XPOND MAIN BUS...

Страница 340: ...ONTROLLER ELECTRICAL WIRING INFORMATION Refer to the latest revision of the Airmaster AP3 Series and AP4 Series Constant Speed Propeller Operator s Manual 13 18 ROTAX 914 UL ENGINE ELECTRICAL WIRING I...

Страница 341: ...ED EQUIPMENT Figure 85 Firewall mounted equipment 1 Oil reservoir 7 TCU 2 Fuel pump assembly 8 GPS antenna 3 Cabin air inlet splitter box 9 Main battery 4 Turbocharger waste gate servo 10 Coolant over...

Страница 342: ...oupling length to be adjusted in situ by turning the rod 1 just as one would a turnbuckle Loosen the two lock nuts 2 and adjust the pushrod Once the desired length has been set the pushrod is locked b...

Страница 343: ...325 15 3 FITTING OF FIRE RESISTANT SLEEVING Fire resistant sleeving fitted over fuel oil hoses which are secured to fittings couplings with two ear clamps must be secured with safety wire adjacent to...

Страница 344: ...m 0 063 AN960 416 AN4 washer 0 8 mm 0 032 AN960 416L AN5 washer 1 6 mm 0 063 AN960 516 AN5 washer 0 8 mm 0 032 AN960 516L AN6 washer 1 6 mm 0 063 AN960 616 AN6 washer 0 8 mm 0 032 AN960 616L AN7 washe...

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