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Содержание 188 Series

Страница 1: ...REPRINT MODEL 188 T188 SERIES 1966 THRU 1984 SERVICE MANUAL 0 D2054 1 13 THIS REPRINT CONSISTS OF THE BASIC MANUAL DATED 25 MARCH 1983 AND INCORPORATES REVISION 1 DATED 1 AUGUST 1983...

Страница 2: ...SERIES Member of GAMA THIS REPRINT CONSISTS OF THE BASIC MANUAL DATED 25 MARCH 1983 AND INCORPORATES REVISION 1 DATED 1 AUGUST 1983 COPYRIGHT 1987 CESSNA AIRCRAFT COMPANY 25 MARCH 1983 WICHITA KANSAS...

Страница 3: ...ON 1 For Paper Publications file this cover sheet behind the publication s title page to identify the inclusion of the Temporary Revision into the manual Insert the new pages into the publication at t...

Страница 4: ...INSTRUCTIONS FOR THIS TEMPORARY REVISION 1 For Paper Publications file this cover sheet behind the publication s title page to identify the inclusion of the Temporary Revision into the manual Insert t...

Страница 5: ...faces with corrugated skins FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For Paper Publications File this cover sheet behind the publication s title page to identify the inclusion of the Temporary...

Страница 6: ...to incorporate both electrically and pressure controlled oil temperature and oil pressure gages 4 To add table to aid in trouble shooting the oil temperature gage FILING INSTRUCTIONS FOR THIS TEMPORA...

Страница 7: ...limits for turbocharger oil line check valves FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For Paper Publications File this cover sheet behind the publication s title page to identify the inclusion...

Страница 8: ...10 1 11 14 1 v 1 5 1 1 11 15 0 vi 0 5 2 thru 5 3 0 11 16 thru 11 18 1 1 thru 1 5 0 5 4 1 11 19 thru 11 24 0 1 6 1 5 5 thru 5 19 0 11 25 1 2 1 0 5 20 1 11 26 0 2 2 5 21 thru 5 24 0 11 27 thru 11 28 1...

Страница 9: ...u 16 15 0 19 9 thru 19 13 0 13 1 1 16 16 19 13A thru 19 13B 0 13 2 0 16 17 thru 16 29 0 19 14 thru 19 20 0 13 3 thru 13 6 1 16 30 thru 16 31 1 19 21 1 13 7 0 16 32 thru 16 56 0 19 22 0 13 8thru 13 9 1...

Страница 10: ...L INJECTED 1J2 1A1 11B ENGINE TURBOCHARGED 1K11 11B 1 12 FUEL SYSTEMS 2A2 12 1 13 PROPELLERS AND GOVERNORS 2B7 13 1 14 UTILITY SYSTEMS 2C1 14 1 15 INSTRUMENTS AND INSTRUMENT SYSTEMS 2C15 15 1 16 ELECT...

Страница 11: ...HANGE BLOCK CHANGE AGWAGON A 230 HP 188 188 0318 188 0572 AGWAGON A 300 HP A188 188 0318 188 0572 BLOCK CHANGE BLOCK CHANGE BLOCK CHANGE BLOCK CHANGE AGWAGON B 230 HP 188A 18800573 18800832 AGWAGON B...

Страница 12: ...k 300 HP A188B 18803297T 18803521T AGhusky 310 HP T188C T18803297T T18803521T AGwagon 300 HP 1980 A188B 18803522 18803721 AGtruck 300 HP A188B 18803522T 18803721T AGhusky 310 HP T188C T18803522T T1880...

Страница 13: ...to the Cessna as signed serials shown in the following chart SERIALS NAME MODEL BEGINNING ENDING AMC 188 AGpickup A 188B A 1880002 A 1880002 230 H P 18801034 18801034 AMC 188 AGwagon A 188B A A188000...

Страница 14: ...ssna Aircraft Company for this publication as required and include only pages that require updating 2 REISSUE Manual is reissued to dealers as required and is a complete manual incorporat ing all the...

Страница 15: ...ity to breathe deeply enough 5 Sometimes a cough is evident 6 Sometimes but not always headache fatigue anorexia loss of appetite nausea perspiration dizziness twitching dreaming irritability and mood...

Страница 16: ...1 4 AIRCRAFT SPECIFICATIONS Leading par for engine mount tailcone landing gear and wing ticulars of these aircraft with dimensions based on and strut attachment as well as supporting struc gross weig...

Страница 17: ...0 HP Fixed Pitch Two Blade 90 McCAULEY 230 HP Constant Speed Two Blade 88 McCAULEY 230 HP 300 HP Constant Speed Two Blade 86 McCAULEY 300 HP Constant Speed Two Blade 82 McCAULEY 300 HP Constant Speed...

Страница 18: ...on Fin 96 05 Track Width 88 38 Wing Span Turbo Modified Conical Tips 484 40 Wing Span Turbo High Performance Conical Tips 497 20 Length Turbo 326 53 Tail Turbo 132 00 Fin Height Turbo 98 00 Track Widt...

Страница 19: ...SERIES NOTE 23 62 Wing stations shown are NOT the equivalent of 39 00 dimensions in inches from the aircraft center line To find equivalent dimensions from air 56 41 craft centerline add 30 00 inches...

Страница 20: ...n be equally damaging because of fail during final torque back off and re torque ure of a bolt or nut from overstressing threaded areas f When installing a castle nut start alignment There are a few s...

Страница 21: ...0 25 12 15 10 32 80 100 50 60 1 4 28 50 70 30 40 1 4 28 120 145 70 90 5 16 24 100 140 60 85 5 16 24 200 250 120 150 3 8 24 160 190 95 110 3 8 24 520 630 300 400 7 16 20 450 500 270 300 7 16 20 770 950...

Страница 22: ...825 MS21045 MS20365 MS20500 NAS679 COURSE THREAD SERIES Nut bolt Torque Limits Torque Limits size in lbs in lbs MIN MAX MIN MAX 8 32 12 15 7 9 10 24 20 25 12 15 1 4 20 40 50 25 30 5 16 18 80 90 48 55...

Страница 23: ...er 1B7 2 11 Inspection During Storage 1B2 2 6 Wheels 1B7 2 11 Returning Aircraft to Service 1B3 2 7 LUBRICATION 1B7 2 11 SERVICING 1B3 2 7 Requirements 1B7 2 11 Fuel Tanks and Cells 1B3 2 7 Rod End Be...

Страница 24: ...t be strong enough to support aircraft Make sure tail stand is strong enough to support any weight placed on it A telescoping adjustable tail stand is illustrated However any suitable tail stand may b...

Страница 25: ...will cause the main wheel internal control lock and set parking brake to slide inboard as the wheel is raised tilting the jack The jack must then be CAUTION lowered for a second jacking operation Jack...

Страница 26: ...quantity of engine oil Refer locks may be installed to figure 2 4 and paragraph 2 21 for correct grade of engine oil 2 8 WEIGHING AIRCRAFT Refer to Pilot s Operating Handbook 2 11 TEMPORARY STORAGE T...

Страница 27: ...the piston in a down posi g While spark plugs are removed rotate propel ton Rotate crankshaft as each pair of cylinders is ler several revolutions to clear excess rust preven sprayed tive oil from cyl...

Страница 28: ...or indicates an NOTE unsafe condition c If the dehydrator plugs have changed color in one To throughly cover all surfaces of the cylinder half of the cylinders all desiccant material in the interior m...

Страница 29: ...h model is listed in figure 2 4 fuel grade for each model is listed in figure 2 4 Alcohol if used is to be blended with the fuel in a Fuel capacity for each model configuration is concentration of 1 b...

Страница 30: ...el system at the intervals New or newly overhauled engines should be specified Also during daily inspection of the fuel operated on aviation grade straight mineral strainer if any water is found in th...

Страница 31: ...rily brush then coat with petroleum jelly before connect by aircraft operating conditions A good general rule ing Check the battery every 50 hours or at least however is to remove and clean the filter...

Страница 32: ...y scratch the plastic surface access doors and reinstall panels and pilot s seal CAUTION 2 33 ENGINE AND ENGINE COMPARTMENT An engine and accessories wash down should be accom Do not use gasoline alco...

Страница 33: ...g agents should never be left on ings Sand smooth prime and repaint minor defects engine components for an extended period of time Failure to remove them may cause damage to components such as 2 36 LU...

Страница 34: ......

Страница 35: ...tors Specification MHS 24 and all revisions or supplements thereto must be used except as noted in paragraph 2 21 herein Refer to Continental Aircraft Engine Service Bulletin M75 2 and any superseding...

Страница 36: ...MODEL 188 T188 SERIES SERVICE MANUAL HYDRAULIC DISPERSAL SYSTEM SERVICE REQUIREMENTS...

Страница 37: ...tails 19 PROPELLER Inspect blades at hubs for red oil oil filled hubs O FIRST 25 HOURS 15 ENGINE OIL SYSTEM Drain engine sump and replace filter if equipped Refill sump with ashless dispersant oil 25...

Страница 38: ...c fluid Refer to paragraph 2 27 for details 6 FUEL DRAINS Drain off any water and sediment 500 HOURS 16 HYDRAULIC DISPERSAL SYSTEM RESERVOIR Replace fluid flush system and reservoir tank after first y...

Страница 39: ...Products of most reputable manufacturers meet or exceed these specifications LUBRICANTS PG SS G 659 POWDERED GRAPHITE OR MIL G 81322A GREASE GL MIL G 21164 HIGH AND LOW TEMPERATURE GREASE OG MIL L 78...

Страница 40: ...MODEL 188 T188 SERIES SERVICE MANUAL On installation lubri SPRAY VALVE CONTROL CABLE ASSEMBLY...

Страница 41: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 42: ...100 HOURS as necessary to insure continuous airworthiness c An inspection conducted at 200 hour intervals would likewise include the 50 hour items and 100 hour items in addition to those at EACH 200 H...

Страница 43: ...ion 1 when installed or when visual inspection indicates the need for a torque check NOTE Torque values listed in Section 1 are derived from oil free cadmium plated threads and are recommended for all...

Страница 44: ...his Manual 3 Magnito Drop 4 Engine response to changes in power 5 Any unusual engine noises 6 Fuel selector and or shut off valve operate engine on each tank or cell position and OFF position long eno...

Страница 45: ...l filter element 2 Oil cooler 3 Induction air filter 4 Induction airbox air valves doors and controls 5 Cold and hot air hoses 6 Engine baffles 7 Cylinders rocker box covers and push rod housings 8 Cr...

Страница 46: ...rge nozzles and fuel flow gage 33 Turbocharger mounting brackets 34 Turbocharger oil line check valves 22 FUEL SYSTEM 1 Fuel strainer drain valve and control 2 Fuel strainer screen and bowl 3 Fuel tan...

Страница 47: ...seals 4 Seat belts and shoulder harnesses 23 l isr 5 Seat stops seat rails upholstery structure and mounting 21 6 Control stick bearings pulley weight bearings and bellcrank 7 Instrum ents and marking...

Страница 48: ...and chain guards 7 Trim control wheel indicator and actuator 8 Travel stops 9 Decals and labeling 10 Flap control lever latch flap rollers and tracks 11 Elevator downspring system 12 Elevator trim ta...

Страница 49: ...o engne timing are within the prescribed tolerances it is recommended that the magneto be checked interally only at 500 hour intervals Magneto to engine timin should be checked with a iming light at e...

Страница 50: ...e replaced every five years or sooner if any of the following conditions exist fading sun or ultra violet deterioration graying thinning fraying or cutting defective latches and broken stitching Any o...

Страница 51: ...overhauled or replaced at specific time limits Table 1 lists those items which Cessna has mandated must be overhauled or replaced at specific time limits Table 2 lists component time limits which hav...

Страница 52: ...lier Established Replacement Time Limits A The following component time limits have been established by specific suppliers and are reproduced as follows Table 2 Supplier Established Replacement Time L...

Страница 53: ...es equipped with Slick magnetos refer to Slick Service Bulletin SB2 80C or latest revision for time limits For airplanes equipped with TCM Bendix magnetos refer to Teledyne Continental Motors Service...

Страница 54: ...R UPPER CARRY THRU TUBE INCHES OF WELDS ON BOTH SIDES OF AIRCRAFT VIEW FROM LH WING LOOKING FORWARD AND INBOARD AT FRONT SPAR UPPER CARRY THRU TUBE TYP RH ALSO NOTE Each 100 hours inspect tubular stru...

Страница 55: ...F or it may be heated on a hot plate until soft Boiling water should not be used for heat 3 4 CLEANING Refer to Section 2 ing Coat the patch evenly with plastic solvent adhe sive and place immediately...

Страница 56: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 57: ...hes which must be removed to length of crack and thickness of materal restore transparency b Temporary repairs to flat surfaces can be ac d Apply fresh tallow or buffing compound to a complished by pl...

Страница 58: ...MODEL 188 T188 SERIES SERVICE MANUAL 4...

Страница 59: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 3 3 Cabin Door Sheet 1 of 2 3 5...

Страница 60: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 61: ......

Страница 62: ...h Seal Half Assembly 2 4 LH Rib Root Seal 5 RH Rib Root Seal 6 RH Carry Through Seal Half Assembly 7 Reinforcement 8 RH Rib Root Seal Half 9 Hopper Seal 10 RH Side Panel Seal Assembly 11 Seal 12 LH Si...

Страница 63: ...re and aft to disengage seat rollers from rails 3 11 WINDOWS See figure 3 2 c Lift seat out d Reverse the preceding steps for reinstallation 3 12 REMOVAL AND INSTALLATION Ensure all seat stops are ins...

Страница 64: ...e Tube 15 5 5 Seat Back I 3v0 6 Recline Cam 7 Spacer 8 Spring 9 Bushing NOTE 10 Recline Pawl 11 Roller Seat stops 15 are 12 Adjustment Pin installed on the LH RECLINING BACK 13 Fore Aft Handle rail on...

Страница 65: ...16 Bearing Block 17 Spacer 18 Washer 19 Spring 20 Seat Frame 21 Splice Tube 22 Pivot Bracket 23 Seat Back Frame NOTE 24 Collar 25 Forward Torque Tube 26 Aft Torque Tube Thru 18802348 seat incorporates...

Страница 66: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 67: ...de of seat back then loosen upholstery retaining rings and upholstery material as required to expose rivets retaining old cam assembly c Drill out existing rivets and insert new cam assembly 2 Positio...

Страница 68: ......

Страница 69: ...eflector Cable 24 Cable Bracket l 25 Canopy Padding _ a 2 Landing Gear Strut 1 N27 Bracket 21 28 Wheel Fender Bracket Detail G THRU SERIAL 18801374 NOTE _ e s Bond padding 25 to cockpit _ i i ri s r s...

Страница 70: ......

Страница 71: ...2 REMOVAL AND INSTALLATION canopy padding consists ofa 1 4 inch black ensolite cover a Unlock the wing stud fasteners and remove the on the crash pad also urethane bumper pads bonded to fasteners comm...

Страница 72: ...f web or lower flange is cracked index 2 b Any crack in crown of rail is in any direction other than right angle to length of rail c Number of cracks on any one rail exceeds four or any two cracks ind...

Страница 73: ...bles out to the wing fuselage area no fuel provisions are made in the root wings Optional rubberized fuel cells are available h Thru aircraft serial 18800832 loosen strut for installation in the wings...

Страница 74: ...XI SERIAL 18800833 LIGHTS ARE COWL MOUNTED 1 Bolt 10 Nut 19 Airflow Fence Assembly 2 Washer 11 Rear Stub Wing Fitting 20 Aileron 3 Front Spar Fitting 12 Front Wing Gap Cover 21 Aileron Gap Seal 4 Wing...

Страница 75: ...Remove nut and bolt i Rig flap system Refer to Section 7 securing strut to wing J Refuel wing cells if installed and check for d Remove nut and bolt securing strut to fuselage leaks and remove strut...

Страница 76: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 77: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 78: ...45 6 4 6 6 7 23 f D t Detail E 2 F Detail F Detail H e 13 M 12r 11 1 11 212 11 11 3 13 BEGINNING WITH AIRCRAFT SERIAL 18801375 Detail G TORQUE BOLTS 70 100 LB INCHES TORQUE BOLTS 140 225 LB INCHES Fig...

Страница 79: ...provides access to the actuator Hinges are located on the rear spar assembly to support the Be sure to check and reset rudder and eleva elevators tor travel If any stop bolts were removed or settings...

Страница 80: ...OLT WITH NUT OUTBOARD 10 1 Nut 6 Hinge 11 Stabilizer Assembly 2 Washer 7 Elevator Pylon Bracket 12 Moulding 3 Bolt 8 Inboard Elevator Hinge 13 Leading Edge Fairing 4 Attach Fitting 9 Outboard Elevator...

Страница 81: ...from the bond area This i Disconnect deflector cable from canopy shall be done by wiping the surfaces with a j If optional quick loader system is installed clean lint free rag soaked with solvent dis...

Страница 82: ...properly install bulkhead attach to antenna and install clamps sup ed and that it passes through forward bulkhead seal porting lead without damage to either tube or bulkhead 1 Connect flashing beacon...

Страница 83: ...and Cleaning 1E21 5 33 Tailwheel Disassembly and Reassembly 1E21 5 33 Reassembly 1E18 5 30 Installation 1E21 5 33 Tailwheel Installation 1E18 5 30 Brake Lining Check 1E21 5 33 Anti Shimmy Adjustment 1...

Страница 84: ...dshield 5 4 MAIN GEAR shim spacers or washers by removing attaching bolts 5 5 REMOVAL AND INSTALLATION g Remove bolt securing inboard end of strut and a Hoist aircraft in accordance with instructions...

Страница 85: ...MODEL 188 T188 SERIES SERVICE MANUAL 5 3...

Страница 86: ...nstalled as standard equipment Service Kits 188 20 and SK188 21 are available from the Cessna Supply Division for installation of heavy duty springs on aircraft prior to 18800571 Cess na Single Engine...

Страница 87: ...R WASHER MS2000C7 WASHER NAS147 94 BOLT AN12 52A BOLT NAS147 66 BOLT MODELS 188 A188 SERIALS 188 0001 THRU 188 0049 TORQUE NUTS TO 50 70 LB FT WHEN NOT MODIFIED PER SERVICE KIT TORQUE NUTS TO 2300 250...

Страница 88: ......

Страница 89: ...MODEL 188 T188 SERIES SERVICE MANUAL AN960 1216L WASHER BETWEEN LANDING GEAR SPRING STRUT...

Страница 90: ...MODEL 188 T188 SERIES SERVICE MANUAL AN960 1216L WASHER BETWEEN LANDING...

Страница 91: ......

Страница 92: ......

Страница 93: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 94: ...16 063 WASHER LANDING GEARSS MS20002C12 WASHER SPRING e1641016 1 S1450 7H16 063 SHIM WASHER M O NAS152 88 BOLT MS20002C7 WASHER 613019 3 sp TORQUE NUTS TO 37 5 42 LB FT MS20002C7 WASHER WINGTIPS MAY B...

Страница 95: ......

Страница 96: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 97: ...NG GEAR SPRING STRUT S1450 7H16 063 WASHER 1641016 1 MS20002C7 NAS152 88 BOLT 1613019 3 LOWER iWASHER SADDLE MS20002C7 WASHER ODELS 18 A188 SERIALS 188 0050 THRU 188 0317 WHEN MODIFIED PER SERVICE KIT...

Страница 98: ......

Страница 99: ...18801332 MS20365 720C NUT MS21044N12 NUT THRU 18801332 BEGINNING WITH MS51943 38 NUT 18801333 SERVICE BEGINNING WITH PARTS 18801333 SERVICE PARTS AN960 1216L WASHER MS20002 12 WASHER Figure 5 2 Main...

Страница 100: ...5 70 LB FT 1613019 2 LOWER LUBRICATE THREADS SADDLE M So0 2 oTORQUE NUTS TO 2300 2500 LB IN l MS20002C8 COAT LIGHTLY HOLE BOLT C p WASHER i WITH ELECTRO MOLY NO 11 MIL G 21164 A MAXIMUM OF 1 MS20002 1...

Страница 101: ...rcraft is d Clean the surfaces to be bonded thoroughly If flown from surfaces with mud snow or ice a solvent is used remove all traces of solvent with the fender should be checked to make sure a clean...

Страница 102: ...Brake Cylinder 2 Grease Seal Ring 11 Grease Seal Felt 20 Pressure Plate 29 Piston 3 Bearing Cone 12 Bearing Cup 21 Anchor Bolt 30 O Ring 4 Outer Wheel Half 13 Bearing Cup 22 Brake Hose Fitting 31 Bra...

Страница 103: ...MODEL 188 T188 SERIES SERVICE MANUAL WHEEL AND BRAKE ASSEMBLY 8 50 X 10...

Страница 104: ...MODEL 188 T188 SERIES SERVICE MANUAL WHEEL AND BRAKE ASSEMBLY 8 00 X 8 17 16 15 7 BEGINNING WITH 18800833 11 9 19 20 21 35 24 32 30 31 29 28 27 26 Figure 5 4 Main Wheel and Brake Sheet 3 of 3 5 22...

Страница 105: ...er to paragraph 5 15 for wheel installation halves must be replaced Sand out nicks gouges e Remove plugs or caps from brake hose and con and corroded areas Where the protective coating nect Bleed the...

Страница 106: ...MODEL 188 T188 SERIES SERVICE MANUAL portion is 22 inch Figure 5 5 Wheel Alignment 5 24...

Страница 107: ...ng service it may be statically rebalanced Wheel balancing equipment is available from the Cessna Service Parts Center Figure 5 6 Tail wheel Bracket Removal 5 18 TAIL GEAR See figure 5 7 NOTE 5 19 DES...

Страница 108: ...MODEL 188 T188 SERIES SERVICE MANUAL 3...

Страница 109: ......

Страница 110: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 5 7 Tailgear Installation Sheet 3 of 3 5 28...

Страница 111: ...n accordance with applicable paragraphs in wipe with clean rag saturated with acetone or alcohol this section Immediately wipe dry with clean lint free cloth 5 23 REMOVAL OF TAIL WHEEL ASSEMBLY NOTE a...

Страница 112: ...ut until a slight bearing drag is they are embedded with foreign matter the felt is obvious as wheel is turned Back off nut to the near not pliable or the material is broken or does not re est castell...

Страница 113: ...crometer crank b Rotate sleeve 2 until slot 1 is at top 5 33 DESCRIPTION The hydraulic brake system c Pull handle 4 up and aft and rotate to locking consists of two master cylinders each operated by d...

Страница 114: ...5 9 d Remove piston 5 and spring 8 a Unscrew clevis 1 and jamb nut 2 e Remove packing 7 and back up ring 6 from b Remove screw 18 piston 5 c Remove filler plug 17 and setscrew 5 d Unscrew cover 4 and...

Страница 115: ...d Clamp the flat sides of the anvil in a vise sary wipe with a clean cloth saturated in hydraulic e Align new lining on back plate and place a brake fluid and inspect for damage rivet in one hole with...

Страница 116: ...3 4 CRemove plug and drill 1 16 hole ating Sleeve 8 Cu30t from vertical if pug is notScrew vented o 040 0 005 INCH DO NOT DAMAGE 9 LOCK O SEAL 14 mV12 16 151 THRU 1978 MODELS ASSEMBLY OF PISTON 1 Clev...

Страница 117: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 5 9 Brake Master Cylinder Sheet 2 of 2 5 35 5 35...

Страница 118: ...consists of a control knob nents will restore the system to its correct operation on the instrument panel which operates a double con trol one control routing to each master cylinder At 5 58 PARKING...

Страница 119: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 120: ...MODEL 188 T188 SERIES SERVICE MANUAL 11 10 SEE SHEET 1 FOR KNOB OPERATED SYSTEM 9...

Страница 121: ...he control stick and torque tube assembly trans forms lateral movement of the stick into pulling 6 2 DESCRIPTION The aileron control system motion on the cables Travel extremes are set by consists of...

Страница 122: ...re and aft the stick items removed for access pivots in a bracket at the aft end of the torque tube b TORQUE TUBE ASSEMBLY assembly providing elevator control When moved 1 Complete steps 1 2 and 3 of...

Страница 123: ...MODEL 188 T188 SERIES SERVICE MANUAL THRU AIRCRAFT SERIAL 188 0229 AIRCRAFT SERIAL 188 0230 THRU 18800707 BEGINNING WITH AIRCRAFT SERIAL 18800708 THRU AIRCRAFT SERIAL 18801348...

Страница 124: ...MODEL 188 T188 SERIES SERVICE MANUAL 7...

Страница 125: ...DEL 188 T188 SERIES SERVICE MANUAL BEGINNING WITH AIRCRAFT SERIALS 18801349 OR SERIALS 18800708 THRU 18801348WHEN MODIFIED IN ACCORDANCE WITH SK188 29 Figure 6 1 Aileron Control System Sheet 3 of 3 6...

Страница 126: ...l r J 19 Secondary DOWN Elevator Travel Stop Adjustable 20 Bob Weight 21 Mounting Plate 22 Grip Electrical 23 Sta Strap THRU AIRCRAFT 24 Wire Bundle SERIAL 18800766 6 25 Electrical Socket 5 A6 7 20 2...

Страница 127: ...MODEL 188 T188 SERIES SERVICE MANUAL 22...

Страница 128: ...alance Weight 6 Bolt 7 Nutplate 8 Plug Button 9 Access Plate DetailA 12 10 1 Cotter Pin BEGINNING WITH 18803853 18803857 11 Nut AND ON AND WHEN MODIFIED PER 12 Washer CESSNA SINGLE ENGINE SERVICE INFO...

Страница 129: ...e 4 at aileron d Disconnect cables at bellcrank 19 b Thru 18803851 and including 18803855 and e Disconnect push pull tube 21 at bellcrank 18803856 also aircraft not modified per Cessna f Remove pivot...

Страница 130: ...6 10...

Страница 131: ...the Cessna Supply is comprised of push pull rods bellcranks pulleys Division See figure 6 4 and cables all of which link the flaps to the manu ally operated lever mounted on the left side of the c Ex...

Страница 132: ...n accordance TRAVEL with paragraph 7 16 RELEASE BUTTON Release mechanism Lubricate in accordance STICKS needs lubrication with Section 2 7 5 FLAP LEVER ASSEMBLY 7 7 REPAIR Repair consists of replaceme...

Страница 133: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 134: ...MODEL 188 T188 SERIES SERVICE MANUAL NOTE All details shown are for LEFT wing RIGHT wing opposite 4 THRU SERIAL 18800707 BEGINNING WITH SERIAL 18800708 7 3 5...

Страница 135: ......

Страница 136: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 137: ...he following procedure a Lower flaps to full down position relieve tension on turnbuckles 10 24 26 b Remove access plates 1 from top leading edge and 28 DO NOT DISCONNECT TURN of flap BUCKLES c Discon...

Страница 138: ...rtravel of the control stick resulting attaches to the same point and is routed through the in excess cable stretch Two elevator down springs torque tube and around a pulley where it connects to are a...

Страница 139: ...evators working a Remove access panel from below left door and the elevator trim push pull tube out of elevator access plate from below bellcrank on tailcone e Reverse the preceding steps for reinstal...

Страница 140: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 141: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 8 1 Elevator Control System Sheet 2 of 2 8 4 8 4...

Страница 142: ...ICE MANUAL NOTE The elevator arm assembly to which the elevators Prime balance weight attach screws with MIL P 8585 Loctite primer and seal with MIL S 22473 Loctite sealer to retain screws Figure 8 2...

Страница 143: ...ary stop adjust turnbuckles 17 and 20 evenly to obtain proper tension a Remove access panel from below left door g Move control stick forward until primary DOWN b Remove access plate from below bellcr...

Страница 144: ...o cates tab position on a scale Trim tab travel is ad cated on the right elevator operated by a control justed by stop blocks secured to the control cables wheel mounted on the left side of the cockpi...

Страница 145: ...9 4 spread the crimped ends of the hinge a DO NOT remove bearing 16 from threaded before driving out pin When a pin has rod end 15 unless replacement of bearing is neces been installed crimp ends of h...

Страница 146: ...h pin beginning with MAINTAIN PROPER CONTROL 24 Actuator Detail A CABLE TENSION 25 Chain Guard 26 Sprocket CABLETENSION 10 TO 15 LBS AT AVERAGE TEMPER 28 Clamp ATURE FOR THE AREA 29 Cable Guard SEE FI...

Страница 147: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 148: ...vement with Section 2 b Determine maximum amount of allowable free c Slip collar 7 and bearing 6 on screw 9 play using formula shown in figure 9 2 d Press sprocket 5 into the end of screw 9 c Using mo...

Страница 149: ...clinometer on trim tab and lower to degree specified in figure 1 1 5 Position stop block 1 against stop block 2 and secure to cable A 6 Raise tab to degree specified in figure 1 1 then position stop b...

Страница 150: ...cables to correct tension and safety turnbuckle 17 9 14 CABLES AND PULLEYS g Rotate trim wheel 3 until position indicator 5 is on the TAKE OFF triangle 9 15 REMOVAL AND INSTALLATION See h With elevato...

Страница 151: ...Due to remedy procedures in the following trouble shooting chart it may be necessary to re rig system Refer to para graph 10 11 TROUBLE PROBABLE CAUSE REMEDY RUDDER DOES NOT RESPOND Broken or disconne...

Страница 152: ...MODEL 188 T188 SERIES SERVICE MANUAL 23 6 Detail A Detail B 7 SEE FIGURE 10 2...

Страница 153: ...nchor 8 f 11 9 Bearing Block 12 10 Arm Right Rudder Cable 18 12 11 Arm Left Rudder Cable 12 Left Rudder Bar Detail A BEGINNING WITH AIRCRAFT SERIAL 18800573 13 Bolt 14 Aileron Rudder Interconnect Spri...

Страница 154: ...ex 1 f Disconnect master cylinders 6 from rudder figure 10 1 then carefully remove rudder pedals 3 f Reverse the preceding steps for reinstallation g BEGINNING WITH AIRCRAFT SERIAL 188 0318 Rig system...

Страница 155: ...stance from pointer to pencil mark on rudder in each direction of travel Distance should be in accordance with following chart MODEL YEAR MINIMUM TRAVEL MAXIMUM TRAVEL 188 SERIES THRU AIRCRAFT 7 49 7...

Страница 156: ...move safety wire and tion relieve cable tension at turnbuckles 7 and 8 7 After cables are routed in position install e Adjust travel stop bolts 18 to obtain degree of pulleys and cable guards Ensure c...

Страница 157: ...Removal 112 11 8 Airbox Removal and Installation 1111 11 17 Inspection 112 11 8 Cleaning and Inspection 1112 11 18 Build Up 112 11 8 Induction Air Filter 1112 11 18 Installation 112 11 8 Description 1...

Страница 158: ...ft c Disconnect landing light wires at quick disconnects rear cylinder is number 2 and the cylinders on the beginning with aircraft serial 18800833 left side are identified as 2 4 and 6 For repair and...

Страница 159: ...lugs and required gap Torque 330 30 LB IN Carburetor Marvel Schebler MA4 5 Fuel Aviation Gasoline Grade Minimum 100L L Alternator 14 Volt 60 Ampere 28 Volt 60 Ampere Starter 12 Volt Automatic Engageme...

Страница 160: ...0 30 LB IN Carburetor Marvel Schebler MA4 5 Fuel Aviation Gasoline Grade Minimum 100LL Alternator 14 Volt 60 Ampere 28 Volt 60 Ampere Starter 12 Volt Automatic Engagement 24 Volt Automatic Engagement...

Страница 161: ...h 11 61 Excessive induction air leaks Correct cause of air leaks Defective carburetor Repair or replace carburetor Water in fuel system Drain fuel tank sumps fuel lines fuel strainer and carburetor En...

Страница 162: ...Refer to paragraph 11 61 Defective engine Engine repair is required POOR IDLE CUT OFF Worn or improperly rigged Rig properly Replace worn mixture control linkage Defective carburetor Repair or replace...

Страница 163: ...ary between models and op tional equipment installed however the following 2 Starter electrical cable at starter general procedure may be followed 3 Electrical wires and wire shielding ground NOTE at...

Страница 164: ...s cautiously and should always be properly and identification tags as each item is con neutralized after their use nected or installed Omit any items not 11 13 ACCESSORIES REMOVAL Removal of en presen...

Страница 165: ...rmanent set during 1 Cylinder head temperature probe at lower extended use in service Straightening a hose with a side of cylinder bend having a permanent set will result in hose 2 Electrical wires an...

Страница 166: ...MODEL 188 T188 SERIES SERVICE MANUAL 1 Bolt 2 Engine Mount Structure 3 Washer 4 Barrel Nut...

Страница 167: ...g require ments of the unit Inspect the metal parts for cracks and excessive wear due to aging and deterioration Inspect the 11 24 ENGINE MOUNT See figure 11 1 rubber pads for separation between the p...

Страница 168: ...e fective parts Clean and install replace defective parts LOW OIL PRESSURE Low oil supply Replenish Low viscosity oil Drain sump and refill with proper grade and quantity of oil Oil pressure relief va...

Страница 169: ...aged Remove Clean valve and seat If or held open by solid matter still inoperative replace Low oil supply Replenish Oil viscosity too high Drain and fill sump with proper grade and quantity Prolonged...

Страница 170: ...il will drain from g Inspect adapter gasket seat for gouges deep filter as assembly is removed from adapter scratches wrench marks and mutilation If any of c Press downward on stud 23 to remove from t...

Страница 171: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 11 3 Full Flow Oil Filter 11 15...

Страница 172: ...r damage Clean adapter in sol For overhaul and repair of the carburetor refer to vent and dry with compressed air Ascertain that all the manufacturer s overhaul and repair manual passages in the adapt...

Страница 173: ...irbox is nonremovable carburetor intake throat to obtain a slight and mo mentary gain of 50 rpm maximum at 1000 rpm en 11 47 DESCRIPTION Ram air enters the induc gine speed as mixture control is moved...

Страница 174: ...erates operation and proper rigging the breaker points at the other end of the shaft The nylon rotor gear drives a nylon distributor gear which 11 50 INDUCTION AIR FILTER transfers high tension curren...

Страница 175: ...ing position of number one piston just opening to fire No 1 cylinder e Remove magneto retainer clamps nuts and washers and pull magneto from crankcase mounting The magneto is grounded through the magn...

Страница 176: ...magneto drive gear out of mesh with its or minus five degrees when the breaker points open drive gear and rotate it to the aligned angle to fire number one cylinder remove the magneto and then push it...

Страница 177: ...ear shaft against the thrust bearing nal resistor to provide longer terminal life Spark in the distributor cap plug service life will vary with operating conditions 5 Oil the bearings at each end of t...

Страница 178: ...Figure 11 7 Control Quadrant and Throttle Arm to Idle Stop Attachment 11 22...

Страница 179: ...ion and tighten friction con 11 69 PROPELLER CONTROL Refer to Section trol knob on quadrant to prevent movement of lever 13 for rigging propeller and governor control c Move throttle control arm on th...

Страница 180: ...ircuit Defective starter switch or Install new switch or wires switch circuit Defective starter motor Repair or replace starter motor STARTER MOTOR RUNS BUT Defective overrunning clutch Install new st...

Страница 181: ...sound Check that the brushes slide type are subject to burning cracking and general freely in their holders and make full contact on the deterioration from alternate thermal stresses and commutator W...

Страница 182: ...bly 8 Clamp 9 Support 10 Ball joint BEGINNING WITH AIRCRAFT 18800800 18800802 18800805 THRU 18802706 AND 18802710 Detail A NOTE When cabin heating system is not MINIMUM CLEARANCE BETWEEN EXHAUST STACK...

Страница 183: ...eather or low battery starting Refer to paragraph 11 85 for use of the external power receptacle Begining with aircraft serials 18800833 the ball joint should be inspected in ac The following may also...

Страница 184: ...up through opening in lower cowl assembly thus heat will also prevent the accumulation of the ing both the oil and cylinders After the engine com sludge and carbon deposits partment has been preheated...

Страница 185: ...11A 16 Installation 1J7 11A 7 Adjustment 1J16 A 16 Pivoting Engine for Maintenance J8 11A 8 INDUCTION AIR SYSTEM 1J18 11A 18 Flexible Fluid Hoses 1J8 11A 8 Description 1J18 11A 18 Pressure Test 1J8 1l...

Страница 186: ...hours operating time for the IO 520 D series section disconnect alternate air rod assembly at engines employed in spraying or dusting operations alternate air door arm ball joint loosen clamp Refer t...

Страница 187: ...imited To A Maximum of 4 6cc Tetraethyl Lead Per Gallon Alternator 14 Volt 60 Ampere 28 Volt 60 Ampere Starter 14 Volt Automatic Engagement 24 Volt Automatic Engagement Oil Sump Capacity 12 U S Quarts...

Страница 188: ...ve and clean Replace if valve or dirty screen defective Clogged fuel injection lines Clean lines and nozzles Replace or discharge nozzles if defective Fuel pump not permitting fuel Replace engine driv...

Страница 189: ...perations OR LACKS POWER Restriction in aircraft fuel Refer to Section 12 system Restriction in fuel injection Clean system Replace any system defective units Engine driven fuel pump Refer to paragrap...

Страница 190: ...vent accumula manner it is to be removed and at which tion of such fuel and oil when lines or hoses point the controls should be disconnected are disconnected e Drain the engine oil sump and oil coole...

Страница 191: ...lines and hoses in place as the engine is positioned near the mount Install shock If the aircraft is equipped with an engine mounts and ground straps as illustrated in figure driven hydraulic dispers...

Страница 192: ...ance with paragraph hoisting Lug on top of the engine and take up engine 11A 10 weight with the hoist b Remove bolts from upper and lower mount to fuselage structure and carefully remove engine NOTE m...

Страница 193: ......

Страница 194: ...S SERVICE MANUAL NOTE Typical mount to firewall attachment hardware is as shown in Detail D DRAIN HOLE D SWING MOUNT Detail D BEGINNING WITH AIRCRAFT SERIAL 18801825 Figure 11A 1 Engine Mount Details...

Страница 195: ...nd dampener is a low pressure system of injecting fuel into the assembly with any tpye of cleaning solvent intake valve port of each cylinder It is a multi nozzle continuous flow type which controls f...

Страница 196: ...motive gaskets for any gaskets used in this assembly Use only approved gaskets listed in the Parts Catalogs N 1 9 1 __4 1 O Ring 2 Adapter Nut 3 Adapter 4 Threaded Insert 5 Stud 6 Filter 7 Safety Wire...

Страница 197: ...manifold valve which provides a central point for distrib NOTE uting fuel to the individual cylinders An internal diaphragm operated by fuel pressure raises or Cap all disconnected hoses lines and fi...

Страница 198: ...DJUSTABLE INTAKE AIR CHECK ORIFICE VALVE TO CONTROL UNIT VENT I VENT FUEL INLET TO FUEL FLOW GAGE _ Y y9lfc _ B S SHIELD CALIBRATED ORIFICE MANIFOLD VALVE IL A AIR INLET LEGEND W_FTRELI F PRESSUREINJE...

Страница 199: ...The filter screen is a tight fit in the body and screen fitted over the nozzle body This screen pre may be damaged if removal is attempted It vents dirt and foreign material from entering the should b...

Страница 200: ...lamp swirl well by a small pressure jet of fuel and is fed f Replace the alternator drive belt and tighten the into the vapor return line where it is returned to the nuts on the adjusting arm so that...

Страница 201: ......

Страница 202: ...eoprene two ply hose and silicone one ply a locking control in the cockpit Unlocking and hose 1 3 diameter of the maximum hose dimension pulling the control out will allow unfiltered 4 Silicone two pl...

Страница 203: ...dditional Palnut type precaution locknut was installed in back of the existing k Check operation of air door in both directions locknut at the engine end of all throttle and making sure the control in...

Страница 204: ...g ring assembly 20 to control arm 16 at the engine end of the control just clears 4 In the cockpit carefully pull mixture the end of control housing when the idle control OUT until retaining ring at t...

Страница 205: ...l attaching pans as noted when NOTE reconnecting controls Refer to the inspection chart in Section 2 Disconnect mixture control 22 rod end for inspection lubrication and or replace from arm 16 ment in...

Страница 206: ......

Страница 207: ...NUAL THRU AIRCRAFT SERIAL 188 0428 SERIAL ALL VIEWS AFT LOOKING FORWARD VIEW A A OF MIXTURE ROD Figure 11A 6 Engine Controls Sheet 2 of 7 11A 23 ALL VIEWS AFT LOOKING FORWARD viewA A Figure 11A 6 Engi...

Страница 208: ...MODEL 188 T188 SERIES SERVICE MANUAL AIRCRAFT SERIAL 18800708 THRU 18800832 AND ALL AIRCRAFT MODIFIED IN ACCORDANCE WITH SERVICE LETTER SE71 3 AND SE71 3 SUPPLEMENT 1...

Страница 209: ...18801629 I0 18801643 and 18801644 equipped with the 300 H P 10 520 D engine at the 100 hour inspection if the safety wire used to secure the throttle or mixture control is broken or deteriorated refe...

Страница 210: ...MODEL 188 T188 SERIES SERVICE MANUAL LEFT HAND SIDE Figure 11A 6 Engine Controls Sheet 5 of 7 11A 26...

Страница 211: ......

Страница 212: ......

Страница 213: ...assemblies for the left and right bank of cylinders Each cylinder has a a Loosen jam nuts at both ends of rod assembly riser pipe attached to the exhaust port The three 42 risers at each bank of cyli...

Страница 214: ...LL the ball joint should be inspected in ac surfaces of the exhaust assemblies can be visually cordance with Cessna Single Engine inspected Service Letter SE 78 42 NOTE 11A 73 EXTREME WEATHER MAINTENA...

Страница 215: ...K23 11B 13 Trouble Shooting 1K14 11B 4 INDUCTION AIR SYSTEM 1K23 11B 13 Static Run Up Procedures 1K20 11B 10 Description 1K23 11B 13 Removal and Installation 1K20 llB 10 Airbox Removal and Installatio...

Страница 216: ...urther recom mendations At the time of overhaul engine acces 11B 6 ENGINE sories should be overhauled Refer to Section 13 for propeller and governor overhaul periods 11B 7 DESCRIPTION An air cooled ho...

Страница 217: ...ternator 28Vdc 60 Amp Starter 24 Vdc Automatic engagement Oil Capacity 13 U S Quarts Tachometer Mechanical Drive Oil Pressure PSI Normal 30 60 Minimum Idling 10 Maximum Cold 100 Source Between No 2 an...

Страница 218: ...and clean screen Replace manifold valve or defective defective valve valve Clogged fuel injection lines or Remove and clean lines and nozzles discharge nozzles Replace defective units Defective auxil...

Страница 219: ...r vent Check for bent lines or loose con manifolding restricted or nections Tighten loose connec defective tions Remove restrictions and replace defective components Defective engine Check compression...

Страница 220: ...eplace turbocharger Improperly adjusted or defective Refer to paragraph 11B 55 waste gate Leak in turbocharger discharge Correct cause of leaks Repair pressure system or replace damaged parts Overboos...

Страница 221: ...ll connections and clamps Fuel discharge nozzle defective Inspect fuel discharge nozzle vent manifolding for leaking connections Tighten and repair as required Check for restricted nozzles and lines a...

Страница 222: ...and connections Leak in exhaust system Check for cracks and loose connections Replace defective components Tighten all clamps and connections TURBOCHARGER NOISY Turbocharger overspeeding from Refer t...

Страница 223: ...ilter obstructed Service air filter Refer to Section 2 for servicing instructions Improperly adjusted wastegate Adjust wastegate Refer to paragraph 11B 55 FUEL FLOW DOES NOT DE efective engine driven...

Страница 224: ...nd that the high RPM stop screw is adjusted proper cept for the engine driven fuel pump The four major ly Refer to Section 13 for procedures components of the system are the fuel injection pump fuel a...

Страница 225: ...raph 11B 8 maintain a proper fuel air ratio at altitude The proceed as follows aneroid is adjustable for fuel pump outlet pressure at a Remove engine cowling in accordance with para full throttle and...

Страница 226: ...obtain correct idle mixture in accordance with para achieved at fullthrottle adjust pump pres graph 11B 40 sure slightly below limits making certain h Completion of the preceding steps have provided t...

Страница 227: ...on engines An engine should idle smoothly system receives air from a scoop on the left side of without excessive vibration and the idle speed the cowling It passes through an automotive type should be...

Страница 228: ...g 2 Air Filter Housing 9 Clamp 3 Seal 10 Inlet Air Duct 4 Filter Element 11 Rotary Air Valve Arm 5 Back Plate Mounts 12 Alternate Air Control Wire 6 Gasket 13 Attaching Bolts 7 Rotary Air Valve 14 Air...

Страница 229: ...the engine exhaust system e Connect control wire 55 to arm 56 f Push alternate air control in and insure approxi 2 With vacuum cleaner operating all joints mate 1 8 cushion in the exhaust system may b...

Страница 230: ...e of 39 5 In Hg at sea level 4 1 Left Rear Oil Sump Mount Bolt 2 Bracket 3 Rear Left Oil Sump Mount Bolt 4 Throttle Parallel to Oil 5 Intake Manifold Connection 6 Throttle Arm 7 Pressure Relief Valve...

Страница 231: ...8 Gate Valve 9 Gate Valve Adjustment 10 Turbine Housing 11 Oil Fitting to Bearing Housing NOTE 12 Compressor Outlet Refer to Bolt Torque Values in Section 1 13 Compressor Inlet of this manual for tor...

Страница 232: ...LH 10 Crossover Tube Intake Balance 11 Exhaust Manifold RH 12 Intake Manifold RH 13 Exhaust Crossover Pipe 14 Wastegate Valve Adjusting Bolt 15 Tailpipe LEGEND 16 Wastegate Valve 17 Turbocharger Turb...

Страница 233: ...8803297T THRU T18803797T 4 Exhaust Divider T18803799T THRU T18803802T 5 Wastegate Valve T18803805T THRU T18803810T 6 Wastegate Valve Adjusting Bolt T18803812T THRU T18803816T 7 Turbocharger Mounting F...

Страница 234: ...T18803803T 2 Exhaust Risers T18803804T T18803811T 3 Crossover Pipe T18803817T ON 4 Exhaust Divider 5 Wastegate Valve 6 Wastegate Valve Adjusting Bolt 7 Turbocharger Mounting Flange 8 Tailpipe 9 Heate...

Страница 235: ...readjusted once set 2 The high RPM 2700 unmetered fuel pres NOTE sure is to be adjusted with the slot headed needle valve on the end of the aneroid At no time during Use caution not to overboost All t...

Страница 236: ...te Cleaning 2A18 12 17 Adjustment 2B3 12 26 Reassembly 2A19 12 18 Emergency Boost Check 2B3 12 26 Red Plastic Flush Type Priming System 2B4 12 27 Filler Caps 2A20 12 19 Description 2B4 12 27 12 1 FUEL...

Страница 237: ...thru serial 18800832 Beginning with serial Use NS 40RA 4 Snap On Tool Corp 18800833 the strainer drain control handle is located Kenosha Wisconsin ML T 544 Thread adjacent to the oil dipstick in the e...

Страница 238: ...grade and amount of fuel Fuel line disconnected or broken Connect or repair fuel lines Fuel tank outlet screen plugged Remove and clean screen and flush out fuel tank Defective fuel shut off valve Rem...

Страница 239: ...e fuel injection system NO FUEL QUANTITY Fuel tank or cells empty Service with proper grade and INDICATION amount of fuel Circuit breaker open or Reset Replace if defective defective Loose connections...

Страница 240: ...MODEL 188 T188 SERIES SERVICE MANUAL FUEL QUANTITY INDICATOR FILLER CAP QUANTITY V SCREEN TRANSMITTER SHUT OFF VALVE FUEL KNOB SHUT OFF VALVE STRAINER DRAIN...

Страница 241: ...MODEL 188 T188 SERIES SERVICE MANUAL FUEL QUANTITY INDICATOR FILLER CAP Figure 12 1 Fuel System Schematic Sheet 2 of 4 12 6...

Страница 242: ......

Страница 243: ...MODEL 188 T188 SERIES SERVICE MANUAL FUEL QUANTITY INDICATORS LEFT RIGHT LEFT WING CELL RIGHT WING CELL FILLER FILLER CHECK CAP CAP CHECK...

Страница 244: ...S SERVICE MANUAL 3 On Off Control Handle 9 Fuel Tank 14 Screw 4 Primer 10 Gasket 15 Float Arm 5 Overboard Vent Line 11 Fuel Quantity Transmitter 16 Float 6 Fuel Line 17 Nut Ring Figure 12 2 Fuel Syste...

Страница 245: ...to Detail E 1 Check Valve 7 Strainer 13 O Rl 12 14 PRIOR TO SERIAL NOTE SERIAL NO A188 0318 ON NO A 188 0318 This installation is applicable to Detail C fuel injection engines Detail D 1 Check Valve...

Страница 246: ......

Страница 247: ...8 r wise and bond to Detail G 8 Stfuel line with 7 3M EC 800 8 0 TU 1 EC 1300 or I I I1 7 11 EC 1300L a At FrREFER TO 9 I Y 1 Scoop 9 Auxiliary Pump Drain Line sLC 2 Vent Line 10 O Ring Fige 1 3 Fuel...

Страница 248: ......

Страница 249: ...MODEL 188 T188 SERIES SERVICE MANUAL Vapor return Line fitting is capped...

Страница 250: ...r Do not crowd cell in container the cell by fuel expansion Use wadding to prevent movement c Stack boxed cells to allow access to oldest cells h Any fuel vent or crossover line found plugged or first...

Страница 251: ...MODEL 188 T188 SERIES SERVICE MANUAL NOTE...

Страница 252: ...nstructed of either metal or red plastic certain that cell is extended out to the structure and Both cap assemblies incorporate a vent safety valve no corners are folded in that provides vacuum and po...

Страница 253: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 254: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 255: ...reinstall age was not due to a bad O ring or outer seal cap in the adapter assembly an additional split washer 16 may be added for a total of two prior to reassemblying cap 12 35 FUEL QUANTITY TRANSM...

Страница 256: ...l is located top assembly install screen and standpipe at the left rear side of the engine adjacent to the oil Tighten standpipe only finger tight dipstick and is accessible through the oil dipstick g...

Страница 257: ...MODEL 188 T188 SERIES SERVICE MANUAL 1 ON OFF Control...

Страница 258: ...OLE BEGINNING WITH SERIAL 18802557 1 2 39 13 15 I 2 NOTE Ji i Torque nut 15 to 25 30 lb in SAFETY WIRE HOLE SERIAL NO A188 0446 ON 1 Spring 6 Plate 12 O Ring 2 Washer 7 O Ring 13 Bowl 3 Plunger 8 Gask...

Страница 259: ...fuel from reservoir tank and lines with strainer tions from pump drain control To expedite fuel draining remove d Loosen clamps securing pump plug from bottom of reservoir tank e Remove fuel pump k Di...

Страница 260: ...d the closed position as during letdown land hot weather When the switch is in this position the ing and taxiing the fuel pump fow rate is automati auxiliary fuel pump can operate at two flow rates de...

Страница 261: ...the throttle passes the marked master switch on and the engine stopped position the intake manifolds will be flooded 7 Adjust number two resistor until an approx imate 4 gallons hr flow is indicated...

Страница 262: ...anifold thus priming the entire length of the intake manifold for each bank of cylinders Replacement of the primer is accomplished by disconnecting the fuel lines at the primer and removing the primer...

Страница 263: ...acket on the propeller cyl governor regulated propeller installed The constant inder nearer the center line of the propeller During speed is single acting in which engine oil pressure the 1976 model y...

Страница 264: ...propeller governor Refer to section 11 for TOO LOW adjustments procedures ENGINE SPEED WILL NOT Sludge in governor Remove and clean STABILIZE Air trapped in propeller Trapped air should be purged actu...

Страница 265: ...t pilot with clean engine oil and install the O ring a Remove spinner attaching screws and remove in the propeller hub spinner spinner support and spacers b Remove cowling as required for access topro...

Страница 266: ...t and washers under nut through aircraft serial 188 0537 Install screws with heads forward and washers under DETAIL A APPLIES TO CYLINDER 4 ATTACHMENT screw heads beginning with aircraft serial 188 WH...

Страница 267: ......

Страница 268: ...THREE BLADED THREADED...

Страница 269: ...MODEL 188 T188 SERIES SERVICE MANUAL 3 Blade Propeller 2 Blade Propeller 1 Relief Hole 2 Ferrule 3 Retainer Nut OIL FILLED HUB INSPECTION Figure 13 2 Constant Speed Propeller Sheet 4 of 6 13 7...

Страница 270: ...a 1 Doe 23 NOTE 1 Torque propeller mounting nuts 21 to 660 780 lb in 4 USED WITH AIR CONDITIONER SO L 5 __ 1 Spinner 14 O Ring _ y 12 3 Screw 16 Stud A 1 A 4 Washer 17 Dowel Pin P 1 K 65 Spinner Suppo...

Страница 271: ...d spinner support 3 DO NOT 13 14 15 use more than a total of 14 spacers in this 16 installation 10 11 19 1 Spinner 11 Dowel Pin 2 Screw 12 O Ring 3 Spinner Support 13 Crankshaft 4 Spacer 14 Washer NOT...

Страница 272: ...2 2 High Speed Stop Screw 4 N 3 Governor Arm Extension 5 Rod End 6 Governor Control I I 9 oi 7 Oil Pan Bolt Ref 8 Bracket 5 6 9 Safety Wire A 10 Balance Tube Ref 11 Lever 12 Washer 1 10 7 AIRCRAFT SER...

Страница 273: ......

Страница 274: ...the engine and compressed springs Oil pressure is boosted in the install mounting nuts and washers Do not force governor by a gear type oil pump A pilot valve fly spline engagement Rotate engine cran...

Страница 275: ...ely 1 8 inch and procedure lock in this position This will allow cushion to assure full contact of the governor arm with the Refer to the inspection chart in Section 2 governor high rpm stop screw for...

Страница 276: ...ed from the scoop door on the underside of the ment panel regulates the volume of heated air enter left wing stub to a connection in the ventilation sys ing the system Pulling the heater control full...

Страница 277: ......

Страница 278: ......

Страница 279: ......

Страница 280: ...MODEL 188 T188 SERIES SERVICE MANUAL NOTE If warm air valve seat 7 figure 14 1 is removed it must be sealed per Section 17 upon installation 7...

Страница 281: ...802746 See figure 14 8 14 14 DESCRIPTION The installation is com prised of two fresh air scoops mounted in the canopy 14 15B DESCRIPTION The fresh air unit in the top a plenum chamber and rotatable ai...

Страница 282: ......

Страница 283: ...10 Air Vent Door Assembly 17 Washer 3 Clamp 11 Seal 18 Actuator Assembly 4 Stay Strap 12 Canopy Top Skin 19 Washer 5 Grommet 13 Stud 20 Spring Washer 6 Lever Assembly 14 Nut 21 Spacer 7 Screw 15 Door...

Страница 284: ...5 7 3 6 1 Detail B 18801825 THRU 18802745 A B 2 M I Duct 2 Clamp 3 Screen 4 Cup Assembly 5 Seal 6 Nut V u 7 Washer 8 Lever 9 Cotter Pin 11 Pin 12 Clamp 13 Control Assembly 1 14 Control Support Plate 1...

Страница 285: ...27 Gasket 8 Cabin Top Air Inlet 28 Control Support Plate 9 Screen 29 Clamp 10 Washer 30 Door Assembly 11 Control Guide 31 Link 12 Grommet 32 Lever 13 Aft Cabin Top Plenum Assembly 33 Seal 14 Control...

Страница 286: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 14 8 Cabin Ventilation System Sheet 2 of 2 Revision 1 14 11...

Страница 287: ...uld and apply new sealant to clean dry surfaces be accomplished Refer to Section 11 for the exhaust system inspection Since any holes or cracks may 14 16 AUXILIARY CABIN AIR INSTALLATION permit exhaus...

Страница 288: ...age 2D4 15 14 15 1 INSTRUMENTS AND INSTRUMENT SYSTEMS instruments such as fuel quantity and oil pressure gages are so simple and inexpensive repairs usu 15 2 GENERAL This section describes typical all...

Страница 289: ......

Страница 290: ......

Страница 291: ...ocedure 15 2 h Disconnect static pressure lines from airspeed 15 9 DESCRIPTION The pitot system conveys ram indicator and vertical speed indicator Use suitable air pressure from the pitot mast mounted...

Страница 292: ...INES Although the pitot line and heater wires if installed Pitot and static system is designed to drain down to pitot tube open lines are removed in the usual manner after remov ing condensation may c...

Страница 293: ...sitive pressure with airspeed indicator connected into static system 1 Hold pressure hose firmly against static pressure source opening 2 Slowly squeeze air bulb to apply desired pressure to static sy...

Страница 294: ...TROUBLE SHOOTING ALTIMETER NOTE Refer to paragraph 15 13 before blowing out pitot or static lines TROUBLE PROBABLE CAUSE REMEDY INSTRUMENT FAILS TO Static line plugged Blow out lines OPERATE Defectiv...

Страница 295: ...out of housing Check cable for is a barometric instrument which indicates the ab worn spots breaks and kinks solute pressure in the intake manifold in inches of mercury The fuel flow and manifold pre...

Страница 296: ...ly supported and all connections are clean tight and properly insulated 15 27 TROUBLE SHOOTING TROUBLE PROBABLE CAUSE REMEDY GAGE INOPERATIVE No current to circuit Repair electrical circuit Defective...

Страница 297: ...line 15 31 OIL TEMPERATURE GAGE 15 33 FUEL QUANTITY INDICATING SYSTEMS 15 32 DESCRIPTION On some airplanes the oil tempera 15 34 DESCRIPTION The magnetic type fuel quan ture gage is a Bourdon tube ty...

Страница 298: ...ransmitter byreversing preceding steps No gasket paste should be used NOTE Be sure grounding is secure in accord ance with Section 12 15 38 TROUBLE SHOOTING TROUBLE PROBABLE CAUSE REMEDY FAILURE TO IN...

Страница 299: ...ass is internally lighted con 15 42 DESCRIPTION The turn and slip indicator trolled by the instrument lights rheostat switch No is operated by the aircraft electrical system and maintenance is require...

Страница 300: ...efore installing transmitter attach electrical wires and place master switch in ON position Allow float arm to rest against lower float arm stop and read indicator The pointer should be on E empty pos...

Страница 301: ...DOUS SITUATION B While the transmitter float arm is being actuated apply airplane battery electrical power as required to ensure that the fuel quantity indicator follows the movement of the transmitte...

Страница 302: ...systems can be adjusted Refer to this section for instructions for adjusting Stewart Warner fuel indicating systems Rochester fuel quantity indicating system components are not adjustable only compon...

Страница 303: ...High voltage Correct voltage Loose or defective rotor Replace instrument bearings 15 44 TURN COORDINATOR motion roll and yaw axes which is projected on a single indicator The gyro is a non tumbling t...

Страница 304: ...ck voltage at instrument Correct voltage NOISY GYRO High voltage Check voltage to instrument Correct voltage Loose or defective rotor Replace instrument bearings 15 47 STALL WARNING SYSTEM Refer to Se...

Страница 305: ...u 18803046 2F1 16 41 Circuit 2D24 16 16 Removal and Installation 2F1 16 41 Description 2D24 16 16 Flashing Beacon 2F1 16 41 Radio Protection Diode 2D24 16 16 Description 2F1 16 41 Description 2D24 16...

Страница 306: ...e right side approximate 25 ampere hour capacity A larger and the alternator mode on the left side This ar heavy duty 12 volt 33 ampere hour battery is offer rangement allows the battery to be on the...

Страница 307: ......

Страница 308: ...MODEL 188 T188 SERIES SERVICE MANUAL 16 5 20 19 23 4 3 17 12 16 5 20 19 18 3 17 22 6 7 15 21 13 14 18800833 THRU 18801824 Figure 16 1 Circuit Breaker Installation Sheet 2 of 2 16 4...

Страница 309: ...ce wiring 16 11 REMOVAL AND INSTALLATION See b T188C THRU T18803721T figure 16 2 1 Remove cover on right hand side of tailcone a A188B THRU 18803721 for access to battery 1 Remove cover on right hand...

Страница 310: ...ons should be kept clean at all discharged with use will decompose the water from times the electrolyte by electrolysis Add distilled water a Remove the battery in accordance with preced as necessary...

Страница 311: ...t rise over 125 F nor should gassing be so violent 16 19 MAINTENANCE The battery box should be that acid is blown from the vents inspected and cleaned periodically The box and cover should be cleaned...

Страница 312: ......

Страница 313: ...Screw 3 Box Assembly 13 Positive Battery Cable 23 Fuse 4 Pin 14 Diode 24 Nylon Nut 5 Angle Assembly 15 Washer 25 Nylon Washer 6 Bolt 16 1 Master Switch Wire 26 Bracket 7 Negative Ground Strap 17 Power...

Страница 314: ...2 Resistor 75 Ohm...

Страница 315: ...ox 4 Bolt 25 5 Drain Tube 6 Clamp 7 Nylon Nut 8 Nylon Washer 9 Fuse 10 Bracket 24 11 Resistor 23 12 Diode 19 Lockwasher 13 Solder Terminal 20 Battery Positive Cable 14 Spacer 21 Diode Assembly 15 Scre...

Страница 316: ...MODEL 188 T188 SERIES SERVICE MANUAL T188C ONLY A Figure 16 2 Battery and Electrical Equipment Installation Sheet 5 of 8 16 12...

Страница 317: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 16 2 Battery and Electrical Equipment Installation Sheet 6 of 8 16 13...

Страница 318: ......

Страница 319: ...862 BEGINNING WITH 18803863 13 1 Contactor Cover 2 Positive Terminal Cover 3 Sta strap 9 4 Battery Cover 5 Clamp 6 Positive Cable 7 Battery 8 Drain Tube 9 Ground Strap 10 Elbow 11 Aircraft Skin 12 Cla...

Страница 320: ...that inductive spikes orginating in the coil are and other semi conductor devices used in the air clipped when the master switch is opened Beginning craft from possible reverse polarity damage with 1...

Страница 321: ...actor and bus 2 Check for voltage at small terminal of ground service re ceptacle If voltage is not pre sent check ground service plug wiring If voltage is present proceed to step 3 Open or mis wired...

Страница 322: ...er to figure 16 1 for prior installation 1 Power Cable 9 Screw 17 Fuse 2 Nipple 10 Receptacle 18 Nylon Nut 3 Nut 11 Doubler Assembly 19 Nylon Washer 4 Star Lockwasher 12 Stud Locking 20 Nylon Spacer 5...

Страница 323: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 324: ......

Страница 325: ...e sure to place the ground strap CAUTION on the negative stud of the receptacle The alternator is very susceptible to reverse 16 31 ALTERNATOR polarity current because of the silicon diodes The diodes...

Страница 326: ...lternator if no noise filter is installed Normal indica tion does not show a direct short If a short exists in wires repair or replace wiring Shorted diodes in alternator 4 Check resistance from outpu...

Страница 327: ...bus Before performing step 4 remove radios from the panel 4 Remove plug from regulator and start engine Momentarily jumper the A and F termi nals together on the plug Ship s ammeter should show heavy...

Страница 328: ...s Service Parts Manual Observe ships ammeter ammeter should in dicate near zero after a few minutes of engine operation Replace regulator OVER VOLTAGE WARNING Faulty regulator Reset over voltage relay...

Страница 329: ...OPENS THRU 18803046 plug and recheck If circuit WHEN BATTERY AND breaker stays in replace Over ALTERNATOR SWITCHES Voltage Sensor ARE TURNED ON Short in alternator voltage Disconnect regulator plug an...

Страница 330: ...WITH ALL ELECTRICAL resistance in field circuit off all electrical loads and EQUIPMENT TURNED OFF turn on battery and alternator CHARGE RATE DOES NOT switches Measure bus voltage TAPER OFF IN 1 3 MINU...

Страница 331: ...al less 1 volt drop thru regulator if not refer to Step 3 3 Starting at F terminal of alternator trace circuit to voltage regulator at B terminal of regulator trace circuit to over voltage sensor to m...

Страница 332: ...24 1971 should be complied with On models manufactured after mid 1971 a new high strength thru bolt and a K shaped retainer are installed 1 Torque bolts 45 to 55 pound inches 2 97 1 Bolt 2 Washer 3 Ar...

Страница 333: ...UE BOLT TO 165 10 LB IN THRU 1977 MODELS 1 Nut 9 Drive Belt 2 Washer 10 Washer 3 Safety Wire 11 Bolt 4 Bolt 12 Engine 5 Washer 13 Engine Mount Support 6 Arm Adjusting 14 Lock Washer 7 Washer 15 Washer...

Страница 334: ...MODEL 188 T188 SERIES SERVICE MANUAL 4 4...

Страница 335: ...IN LB 1 I 1 TORQUE TO 450 500 IN LB X d 7 TORQUE TO 200 270 IN LB 188 0001 THRU 18803240 WHEN MODIFIED PER SK210 84 AND BEGINNING WITH 18803241 1 Washer 2 Bolt 3 Alternator 4 Arm Adjusting 5 Drive Be...

Страница 336: ...t tension should be checked within 10 to ized voltage regulator C611002 0105 and the 28 25 hours of operation volt Alternator NOTE 16 39 DESCRIPTION 28 VOLT 100 AMP ALTER NATOR The regulator is mounte...

Страница 337: ...Nut 17 Wire to Over Voltage Lamp 29 Wire Green S Lockw asher 18 Wire to Voltage Regulator 30 Wire Black 6 Filter Radio Noise 19 Capacitor 31 Altern ator 7 Screw 20 Wire to Warning Assembly 32 Adjustme...

Страница 338: ...RVICE MANUAL BEGINNING WITH 18801998 16 35 37 24 VOLT OVER VOLTAGE RELAY 14 VOLT OVER VOLTAGE SENSOR 18801998 THRU 18803046 Detail C Figure 16 5 Voltage Regulator and Over Voltage Relay Installation S...

Страница 339: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 340: ...ning assembly to the firewall and remove assem on the instrument panel When an over voltage bly tripoff occurs the over voltage sensor turns off the c Remove the four screws securing the diode alterna...

Страница 341: ...NAV LIGHTS OUT Short circuit in wiring 1 Inspect circuit breaker If circuit breaker is open proceed to step 2 If circuit breaker is OK proceed to step 3 Defective wiring 2 Isolate and test each nav li...

Страница 342: ...exchanging flash tube The tube is fragile and can easily be cracked in a place where it will not be obvious visually Make sure the tube is seated properly on the base of the nav light assembly and is...

Страница 343: ...heck voltage at flasher with master and beacon switch on Should read battery voltage Replace switch If voltage is present proceed to step 6 Defective fasher 6 Install new flasher FLASHING BEACON Defec...

Страница 344: ...air or replace wiring LIGHTS OUT Defective spray light switch Replace switch Defective switch on grip Replace switch Defective relay Replace relay ONE SPRAY LAMP OUT Lamp burned out Replace lamp Defec...

Страница 345: ...a period of six 6 months The following serial 18800833 the landing and taxi lights are mounted procedure must be used in the lower half of the cowl nose cap The landing light on the left side and the...

Страница 346: ......

Страница 347: ...THRU 18801040 1 Lower Nose Cap Detail A NOTE 2 Retainer 3 Plate Should further adjustment be desired 4 Lamp washers may be added between plate 5 Bracket 3 and retainer 2 6 Tinnerman Screw 7 Screw Figu...

Страница 348: ...rubber BEGINNING WITH AIRCRAFT Detail forward engine mounts are installed SERIAL 18801041 refer to Cessna Single engine Service Letter SE75 4 dated January 31 1975 1 Lower Nose Cap 6 Lamp 2 Retainer 7...

Страница 349: ...GINNING WITH 18801041 13 7 S AeDetailB 12 14 11 188 0318 THRU 18801040 1 Detail B 1 Shield 10 Tip Assembly Fin 2 Dome 11 Clip Detail A 3 Gasket 12 Housing Cap 4 Lamp 13 Housing Plug BEGINNING WITH 188...

Страница 350: ......

Страница 351: ......

Страница 352: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 353: ......

Страница 354: ...RIES SERVICE MANUAL 9 3 I 8 Detail A Detail B 1 Screw 2 Washer 3 Transistor 4 Mica Washer 5 Heat Sink 6 Cabin Skin 7 Housing socket 8 Rheostat 9 Instrument Panel 10 Knob Figure 16 8 Transistorized Lig...

Страница 355: ...r to provide illumination of the Power is supplied from the bus bar through a circuit contents of the hopper so the pilot can determine the breaker to the off on switch then to the dimming amount of c...

Страница 356: ...rting probe into cutout on cigar lighter the stall warning actuator switch Both heaters are to reset operated by the pitot heat switch 16 93 REMOVAL AND INSTALLATION 16 91 CIGAR LIGHTER THRU 18803872...

Страница 357: ......

Страница 358: ......

Страница 359: ...rial 18801824 Cylinder Head Temperature Ind 0 2 0 04 0 04 0 04 04 04 Flashing Beacon Light 7 0 6 0 6 0 6 0 6 0 6 0 Heated Stall Warning Pitot 10 0 4 05 4 05 4 05 4 05 4 05 Indicator Turn Bank 0 2 0 2...

Страница 360: ...Indicator Turn Coordinator 0 3 Lights Instrument Panel 1 7 Lights Position 2 5 Air Conditioning 6 7 Lights Wing Strobe 3 0 Light Overhead Flood 0 2 ITEMS NOT CONSIDERED RUNNING LOAD Auxiliary Fuel Pum...

Страница 361: ...g a fuse whether to repair or replace a major unit of structure lage will be influenced by such factors as time and labor available and by a comparison of labor costs with the 17 6 ALIGNMENT JIGS When...

Страница 362: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 363: ...el to the vertical center plane of the aircraft Zero buttock line is the vertical plane passing through the centerline of the aircraft Buttock lines are given in inches right R B L or left L B L as vi...

Страница 364: ...repair ends at A few components empennage tips for example are a structural member where no seam is used enough fabricated from thermo formed plastic or glass fiber repair panel should be used to all...

Страница 365: ...ion using dimensions specified in chart Check to see that protractor bubble is still centered 8 Proper twist is present in wing if protractor readings are the same parallel Forward or aft bolt may be...

Страница 366: ...de a smooth surface for the beam and keep the beam 90 to the hinge line of the control surface 7 Paint is a considerable weight factor In order to keep balance weight to a minimum it is recommended th...

Страница 367: ...D CONTROL jr ji 1 SURFACE MOMENT AT CENTER OF WEIGHT ADJUSTABLE SLIDING WEIGHT WEIGHT MANDREL BEAM ASSEMBLY HANGAR ASSEMBLY TO BE IN PROPER POSITION A 7 _CHORD LINE MANDREL FLAT SURFACE RUDDERS AND EL...

Страница 368: ...MODEL 188 T188 SERIES SERVICE MANUAL AILERONS NOTE Refer to chart for correct range of underbalance DETAIL A A HINGE LINE...

Страница 369: ...heavy and is defined by symbol If the balance beam sliding weight must be on the leading edge side of the hinge line to balance the control surface the control surface is considered to be underbalance...

Страница 370: ...The exception to negligible damage on the tate replacement extra access holes may be installed elevator surfaces is the front spar where a crack in the locations noted in figure 17 9 appearing in the...

Страница 371: ...hat does not extend past the stop drilled hole may remain in service without additional repair 17 42A CRACKS IN CORRUGATED FLAP SKINS Continued from page 17 10 1 It is permissible to stop drill crack...

Страница 372: ...as a crack that progresses past a stop drilled hole shall be repaired Refer to paragraphs 17 47 48 and 49 as applicable for repair information 5 A control surface that has any of the following conditi...

Страница 373: ...tress members but may be used If repair parts are formed to fit Small are essentially just covering The tubular structure cracks may be stop drilled and dents straightened Is discussed later in this s...

Страница 374: ...MODEL 188 T188 SERIES SERVICE MANUAL PATCHES AND DOUBLERS 2024 T3 ALCLAD MS20470AD4 RIVETS 24 REQD...

Страница 375: ...MODEL 188 T188 SERIES SERVICE MANUAL Figure 17 4 Skin Repair Sheet 2 of 6 17 13...

Страница 376: ...T3 ALCLAD 1 2 RADrIUS 0 IJ CLEAN OUT EDGE MARGIN _ X IET 2 X RIVET DIA CLEAN OUT S 0 0 I D DAMAGED AREA 1 2 RADIUS SIMILAR 2 1 8 RPI PR TS I RIVET SPACING p o o v 0 I d J 6 X RIVET DIA l _ Wt EEDGE M...

Страница 377: ...ERN Ad _THRU PATCH EDGE DISTANCE Q PITCH 4 8D 2D MIN Y TYPICAL 50F R MNN TYPICAL RIVET TABLE SKIN GAGE RIVET DIA i Ip _ 020 1 8 025 1 8 032 1 8 040 1 8 051 5 32 ATCH 2024 T3 ALCLAD _____FLUSH PATCH AT...

Страница 378: ...MODEL 188 T188 SERIES SERVICE MANUAL DOUBLERS 2024 T3 ALCLAD 17 16...

Страница 379: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 380: ...o RIVET SPACING TO MATCH fi o PATTERN IN SKIN 6 RIVETS EACH SIDE STRINGER OF DAMAGED AREA l CLEAN OUT DAMAGED AREA FILLER 2024 T4 ALCLAD A A A MS20470AD4 RIVETS SKIN ORIGINAL PARTS REPAIR PARTS REPAIR...

Страница 381: ...MODEL 188 T188 SERIES SERVICE MANUAL FILLER 2024 T4 ALCLAD A A STRIP 2024 T3 ALCLAD 1 4 EDGE MARGIN...

Страница 382: ...MODEL 188 T188 SERIES SERVICE MANUAL STOP DRILL CRACK CHANNEL 1 4 EDGE MARGIN Figure 17 5 Stringer and Channel Repair Sheet 3 of 4 17 20...

Страница 383: ...ALCLAD A A CLEAN OUT DAMAGED AREA 3 4 RIVET 7 SPACING l J2 2 ROWS RIVETS OUTBOARD a 0 sll sOF LIGHTENING HOLE 1 4 MARGIN DOUBLER 2024 T4 ALCLAD A AN470AD4 RIVETS ORIGINAL PARTS i REPAIR PARTS REPAIR I...

Страница 384: ......

Страница 385: ...MODEL 188 T188 SERIES SERVICE MANUAL FILLER 2024 T4 ALCLAD Figure 17 6 Rib and Bulkhead Repair Sheet 2 of 2 17 23...

Страница 386: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 387: ...MAGED AREA DOUBLER 2024 T3 ALCLAD 2024 T4 7 8 x 7 x064 AR JAWING SPAR I 3 ROWS RIVETS 1 4 MINI MUM EACH SIDE OF 3 4 RIVET SPACING EDGE MARGIN DAMAGED AREA TYPICAL ALL PARTS DOUBLER 2024 T4 ALCLAD 1 4...

Страница 388: ......

Страница 389: ...blind rivets where regular rivets cannot be bucked 4 Contour must be maintained after repair has been completed use epoxy filler as necessary and sand smooth before painting 5 Vertical size is limite...

Страница 390: ...holes forward of the front spars as close to the front spar as practicable 7 Locate new access holes aft of the front spar between the first and second stringers aft of the spar When installing the do...

Страница 391: ...AREA A A o ANGLE 2024 T4 ALCLAD 10 RIVETS EACH SIDE OF DAMAGED AREA I I FIREWALL ANGLE FILLER 2024 T4 ALCLAD V N s 1MS20470AD4 RIVETS EFIREWALL A d a a a FUSELAGE SKIN ORIGINAL PARTS REPAIR PARTS REP...

Страница 392: ...ially reformed without cracking can be ap minor defect present and cause fatigue cracks En plication of the patch Holes must cracking be ore ap gine mount members are preferably repaired by using a la...

Страница 393: ...This illustration shows the complete fuselage tubular structure assembly which may be re placed as a unit Refer to Sheets 3 thru 6 for individual tube diameters and wall thicknesses Figure 17 11 Fuse...

Страница 394: ...MODEL 188 T188 SERIES SERVICE MANUAL NOTE AGtruck ONLY Tubes not called out on this sheet for the AGtruck are the same as those called out on Sheets 3 4 5 and 6 TAILCONE 11...

Страница 395: ...eters and wall thicknesses for the Beginning with aircraft serial 18801425 original tubes inside sleeves and outside Beginning with aircraft serial 18801825 sleeves are listed in the chart on Sheet 6...

Страница 396: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 397: ...ODEL 188 T188 SERIES SERVICE MANUAL 11 7 inside Tube diameters and wall thicknesses for the Figure 17 11 Fuselage Tubular Structure Sheet 5 of 6 1 11 17 35 1 7 originaltubes inside sleeves and outside...

Страница 398: ...1 8 058 7 8 083 13 1 065 1 1 8 058 7 8 083 14 1 1 8 049 1 1 4 049 1 083 15 1 1 8 058 1 1 4 058 1 095 16 1 1 4 049 1 3 8 049 11 8 083 17 1 1 4 065 13 8 058 1 095 18 1 1 4 095 11 2 095 1 095 19 1 1 4 12...

Страница 399: ...MODEL 188 T188 SERIES SERVICE MANUAL 4...

Страница 400: ...h Coat prepared surface on outside of hopper with the adhesive and apply one layer of cloth using same NOTE technique 1 Allow repair to cure a minimum of 12 hours at A laminating kit SK188 1 a filler...

Страница 401: ...in the h Mix the adhesive according to directions fur laminating kit but is packaged separately nished i Brush a thin film of adhesive over the sanded REPAIR OF CLASS I DAMAGE The purpose of re area a...

Страница 402: ...S mI CLASS IV TYPE 128 OR EQUIVALENT TYPE 128 OR EQUIVALENT FINAL LAMINATION ONLY FINAL LAMINATION ONLY TYPE H63 OR EQUVALENT PE HG63 OR EQUIVALENT FILL HONEYCOMB AND CAVITY WITH FILLER MATERIAL AFTER...

Страница 403: ...USE EXSGR1 4 MINIMUM EDGE MARGIN USE EXISTING RIVET PATTERN a Ah f PATCH MAY OVERLAP CU T o s OR BE INSERTED UNDER o s EXISTING AILERON SKIN A m ORIGINAL PART REPAIR PATCH IN CROSS SECTION L J AA A A...

Страница 404: ...stituted for solid rivets in proportionally in creased numbers in accordance with the table SPARS Blind rivets may be installed in NUMBERS OF FLUSH RIVETS IN DIMPLED SKIN RE wing spars only in those l...

Страница 405: ...restrictions outlined in paragraph 17 83 are met Place the ring of cloth in position and thoroughly wet shear strength of the blind rivet is equivalent or with the adhesive to provide a bed for the al...

Страница 406: ...Figure 17 17 Rivet Shear Strength Sheet 1 of 2 17 44...

Страница 407: ...6 596 862 862 SHEAR STRENGTH OF RIVETS IN POUNDS FLUSH HEAD RIVETS IN SINGLE SHEAR COUNTERSUNK 1 8 inch diameter 5 32 inch diameter 3 16 inch diameter TrhinneatuU ZO J U z U Z U Sheei 016 r 020 163 02...

Страница 408: ...DASH NO 020 062 4 1 5 1 6 1 063 126 4 2 5 2 6 2 126 187 4 3 5 3 6 3 188 250 4 4 5 4 4 251 312 4 5 5 5 6 5 313 375 4 6 5 6 378 437 4 7 5 7 6 7 438 500 4 8 5 8 6 8 501 562 4 9 5 9 6 9 563 625 5 10 6 10...

Страница 409: ...26AD3 063 NAS1399B4 NAS1399D4 Countersunk 040 NAS1769D4 CR3213 4 See Note 1 025 NAS1769B4 NAS1739E4 CR3242 4 MS20426AD4 080 NAS1399B4 NAS1399D4 Countersunk 063 NAS1739B4 NAS1739D4 CR3212 4 050 NAS1769...

Страница 410: ...4 MS20364 MS21042 NAS1103 NAS1303 NAS6203 NAS529 NAS524A See Note 5 NAS1446 NAS1080C NAS1080A6 NOTE 1 Rework required Countersink oversize to accommodate oversize rivet NOTE 2 Do not use blind rivets...

Страница 411: ...or Beginning Jet Glo Serial 18802840 DUPONT LUCITE Used for color stripe on Epoxy thru ACRYLIC LACQUER aircraft serial 188 0251 EPOXY 5400 Standard used on aircraft exterior on thr AGpickup Thru 18802...

Страница 412: ...y with T 3871 thinner Thinning they must be sanded or a paint remover must ratio may be varied to fit the available spraying be used equipment c Apply one wet even coat to completely cover the 18 2 MI...

Страница 413: ...ts which are not welded ed and the surface is not contaminated shut and cannot be sprayed on the inside shall be from the use of a dirty rag Always use dipped in Red Iron Oxide Primer and then sprayed...

Страница 414: ...to 850 F will provide a superior coating 18 18 VERY HIGH TEMPERATURE ENAMEL resistant to m st solvents and fuels Alter completing the priming operation as directed d Cleaning VHT Finish VHT Enamel co...

Страница 415: ...allation and Gate Box and Spreader Assembly 2124 19 22 Rigging 2K14 19 58 Gate Box Control 2124 19 22 MANUAL CONTROL VALVES 2K14 19 58 Removal and Installation 2124 19 22 Description 2K14 19 58 Riggin...

Страница 416: ...tness in chest inability to breathe deeply enough 5 Sometimes a cough is evident 6 Sometimes but not always headache fatigue anorexia loss of appetite nausea perspiration dizziness twitching dreaming...

Страница 417: ...metal fuel tank cover if installed Hopper capacity is 200 gallons except for the AG f Remove nuts from strut attach bolts drive bolts truck which holds 280 gallons Prior to 1880083 forward until threa...

Страница 418: ...inge Halves 9 Top Loader Door 20 10 Latc Assembly 21 11 Seal A 12 Cap 13 Tubular Structure 14 Clamp 15 Overhead Vent Tube 16 Hose 17 Vacuum Relief Valve 18 Catch Assembly 21 20 19 Baffle 20 Seal 20 21...

Страница 419: ......

Страница 420: ...MODEL 188 T188 SERIES SERVICE MANUAL 37 4 CU FT HOPPER INSTALLED IN AGtruck BEGINNING WITH...

Страница 421: ...MODEL 188 T188 SERIES SERVICE MANUAL 19...

Страница 422: ...d to the full FORWARD position c Unclamp or unbolt pump assembly and remove opening the gate box door fully to jettison the contents from hopper of the hopper Pulling the control full AFT will close d...

Страница 423: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 424: ...MODEL 188 T188 SERIES SERVICE MANUAL 3 188 0001 THRU 188 0003 EMERGENCY 188 0004...

Страница 425: ...MODEL 188 T188 SERIES SERVICE MANUAL SEE FIGURE 19 3...

Страница 426: ...ad IF e 15 Cable Assembly 1 4 16 Toggle Clamp 17 Clamp 1 9 18 Support Assembly 9 a 16 Adz 0 I S of 15 p BEGINNING WITH DDetailK SERIAL NO Safety wire 10 to be a 032 da corrosion r 188 0318 1 Plate res...

Страница 427: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 428: ......

Страница 429: ...MODEL 188 T188 SERIES SERVICE MANUAL COUPLER ASSEMBLY BOOM SUPPORT BRACKET...

Страница 430: ...MODEL 188 T188 SERIES SERVICE MANUAL CLAMPS OR BOLTS 5 TO HOPPER OUTLET 4...

Страница 431: ...MODEL 188 T188 SERIES SERVICE MANUAL CLAMPS OR BOLTS TO HOPPER OUTLET SEE FIGURE 9 3...

Страница 432: ......

Страница 433: ...M Corporation FLAMABLE MATERIALS AS CONTACTOR THE SOLENOID COULD CAUSE j C A FIRE V t NOTE 1 Solenoid Trigger operation is dependent upon 2 Spacer SPRAY VALVE BUTTONS ir position of selector switch lo...

Страница 434: ......

Страница 435: ...both as a strainer and a connector to each cable tension boom assembly Removal and replacement may be accomplished while using figure 19 11 as a guide 19 15 SPRAY SYSTEM PLUMBING See figure 19 9 Chemi...

Страница 436: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 437: ...figures 19 4 sheet 4 of 4 and 19 4A sure gage is mounted in the instrument cluster above a With booms installed loosen nuts 6 and bolts the panel pad in the cockpit The gage is connected 4 on one boom...

Страница 438: ...ves aircraft performance by creating less drag and is a high volume unit 19 29 GATEBOX CONTROL Material flow through the gate box is controlled by a handle in the cockpit 19 26 TROUBLE SHOOTING See pa...

Страница 439: ...711 B2 Coast Pro Seal Compton California THRU 18802745 1 Agitator Assembly 2 Gasket 3 Cap 4 Flange Fitting 5 Flapper Valve Assembly 6 Seal 7 Propeller Blade 8 Support 9 Gear Reducer 10 Coupling and K...

Страница 440: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 441: ...e Hinge Fork Lube all bearing and pivot surfaces with 7 Bell Crank Assembly Electro Molly No 11 8 Door Mount Bolts 9 Gatebox Door Approximately 2 inches 10 Gate Seal Mount Bolts 11 Seal Retainer Appro...

Страница 442: ...MODEL 188 T188 SERIES SERVICE MANUAL 10 4...

Страница 443: ...dual installation 2 Cover Tee 8 replaces elbows 7 in 3 Box 6 the dual loading system 4 Loader Valve 5 Clamp 7 6 Hose 7 Elbow 7 8 Tee 9 9 Tube 1 10 Spring 3 11 Stiffener 12 Control Handle NOTE Beginni...

Страница 444: ...ed g Connect gate box rod assemblies 4 to door If leakage is evident adjust hinge fork brackets 5 Since rod ends are not normally bolts or gate box rod as required to seal adjusted from the 11 6 inch...

Страница 445: ...FILLER VALVE ENGINE DRIVEN 1 18800573 THRU 18801374 1 Engine znd engine driven pump running 2 Cockpit control OFF 3 Hydraulic motor INOPERATIVE 4 Relief valve CLOSED VALVE PUMP VA1 JllNGtVAVEVNLVE 188...

Страница 446: ...ydraulic motor INOPERATIVE 3 Hydraulic motor OPERATIVE 4 Relief valve OPEN 4 Relief valve CLOSED 5 Boom Pressure valve control OPEN to be located in an area where the solutions will not to keep two se...

Страница 447: ...MODEL 188 T188 SERIES SERVICE MANUAL SYSTEM ON OFF LEVER 18801375 THRU 18803521 Figure 19 17 Hydraulically Operated Dispersal System Schematic Sheet 3 of 4 19 29...

Страница 448: ...MODEL 188 T188 SERIES SERVICE MANUAL SYSTEM ON OFF LEVER...

Страница 449: ...9 PUMP w IRILER E PES P FILTER OIL FILLER SOOM PRESSURE BOOM B YPASS VALVE DPSTICK A SCREEN CONTROL KNOB Y STRAINER PRESSURE STATIC PRESSURE 0 SPRAY MATERIAL RE0 i CO RETURN FROM a O N OFF i V STRAIR...

Страница 450: ...MODEL 188 T188 SERIES SERVICE MANUAL SYSTEM ON OFF LEVER...

Страница 451: ...pit control pushed full IN move arm on ON OFF valve to full FORWARD Depress air valve core to relieve pressure position Pull control knob out approximately 1 8 before filling reservoir or removing sys...

Страница 452: ......

Страница 453: ......

Страница 454: ......

Страница 455: ......

Страница 456: ...14 Detail B Figure 19 21 Hydraulically Operated Dispersal Systems Sheet 3 of 14 19 38...

Страница 457: ...Spacer 23 o 3D L Y tf41 Spacer Assembly 243 eal 36 42 Gate Box 43 Male Coupling 25 Bearing Cage 33 44 Dust Cap 26 Key 35 37 44 Dust Cap 27 Shat 45 Female Coupling 28 Retaining Ring 35 46 Manual Valve...

Страница 458: ...801041 THRU 18801374 TANG DRIVE L r L_ 27 r SPLINE DRIVE I 26 43 _ _9 45 30 4K 44 25 24 _ 23 NOTE 22 Lubricate splines of shafts 27 with _jii221 1 MIL G 21164 upon installation 21 48 i 20 418 46 _____...

Страница 459: ...MODEL 188 T188 SERIES SERVICE MANUAL NOTE Refer to sheet 4...

Страница 460: ......

Страница 461: ...K POSITION BEFORE WORKING UNDER 63 AIRCRAFT REFER TO DETAIL E Beginnia with 18801825 50 70 piTx64 53 Micrometer 54 Hopper Control Stop 55 Bellcracket 57 Spray Valve Control Arm 58 Shalt 59 Crank Assem...

Страница 462: ...7 Duct 26 8 Washer 9 Bypass Ptn 10 Bypass Spring 11 Bypass Poppet 13 Locking Nut 21 14 Support 15 Head 16 Cartridge 18 Relief Valve 19 Shut off Control 20 Clamp Half Typ 21 Shut off Valve 27 22 Valve...

Страница 463: ......

Страница 464: ...Valve 2 Reservoir 12 Inlet Duct 3 Return Tube 13 Clamp 1 4 Bypass Tube 14 Mounting Bracket 5 Filter 15 Suction Tube TUBULAR 6 I R t S tl 6 Suction Tube 16 Bracket STRUCTURE i 13 7 Hydraulic Motor 17...

Страница 465: ......

Страница 466: ...nut 28 O ring 29 and ball 31 If filler cap is not removed little fluid will be lost while connecting flex hose However sufficient care must be exercised to avoid NOTE excessive fluid loss Use caution...

Страница 467: ...bricate all threads with Petrolatum if Install reservoir tube 64 spacers 60 and return tubes 55 and 62 and suctiom tube bafe 58 57 were removed they should be primed g Assemble and install filter bypa...

Страница 468: ......

Страница 469: ......

Страница 470: ...nurled knob on shaft to move a Wet new air filler valve stem around groove with stop 5 to full AFT position to line up with 20 on clean hydraulic fluid DEXRON Automatic Transmis placard FULLY OPEN mou...

Страница 471: ...inning 18801375 Instrument Panel 10 Control Stick Grip 19 Support Assembly 2 Relay 11 Clamp 20 Contactor 3 Control Stick 12 Electric Motor 21 Resistor 4 Control 13 Valve 5 Stop 14 Spacer 6 Support 15...

Страница 472: ......

Страница 473: ...ONTROL to bracket 12 KNOB See figure 19 21 sheets 9 and 10 e Remove bolts attaching supports 5 to support 18 remove dispenser 3 19 65 DESCRIPTION 18801375 thru 18801682 a f Remove two access covers un...

Страница 474: ...clamp 10 and support washer 11 this unit is sold only as a complete assembly The illustration is provided only to facilitate disassembly and assembly if 10 1 K SE11 1 Lower Quick Disconnect Hall 2 Pi...

Страница 475: ...e 6 with arrow pointing down on valve bracket 21 with nuts 19 washers 22 and packing b Install valve without plumbing in mounting brack nut 23 as shown on sheet 11 of figure 19 21 et assembly with sto...

Страница 476: ...three layers of Polyken 230 or ment Polyken 231 Kendall Polyken Division c Disassemble components and install packings Chicago Illinois or Tuck 92T Technical 22 34 and 39 Tape Corp Shawnee Mission Ka...

Страница 477: ......

Страница 478: ...gear 2 J 20 22 bear4n8 bushings4and shaft 5 Body assemoly tang wim Actro 7 Motor 16 Moly No 11 MIL G 21164 6 U I 27 7 29 29 Coupler Adapter 11 Leaf Actuator Assembly 20 Packing 2 Packing 12 Switch 21...

Страница 479: ...ction adjustment should not be required c Remove hose adapter 15 O ring packings 3 and 15 and shims 4 19 85 ASSEMBLY BALL TYPE VALVES See figure 19 28 CAUTION a Install ball 6 packing 20 support assem...

Страница 480: ...The following procedures will comply with b Remove coupler adapter 2 O ring packings 3 Single Engine Service Letter SE78 31 and 5 and shims 4 c Remove hose adapter 15 O ring packings 3 a Remove bolts...

Страница 481: ...16 to your right o Reinstall 0 rings 3 and adapters 2 and 15 h Slide insert 6 into valve body 17 so that p Install cap 9 and control arm 10 straight land 20 on the inside of insert is toward q Reinsta...

Страница 482: ...MODEL 188 T188 SERIES SERVICE MANUAL THRU SERIAL 18803290 1 Motor...

Страница 483: ...o not intermix total shim thickness from for a higher current draw or turn clunterclockwise end to end Insert must be centered to for a lower current draw operate freely CAUTION d Remove seal attachin...

Страница 484: ...MODEL 188 T188 SERIES SERVICE MANUAL 4...

Страница 485: ...C22 20 69 FUEL AND OIL Spray Lights 24V 3C23 20 70 Fuel Pump System 3B7 20 30 Hopper Light 3C24 20 71 Fuel Pump System 24V 3B8 20 31 HEATING VENTING AND DE ICING Fuel Pump System 12V and 24V 3B9 20 32...

Страница 486: ...lectric Spray Valve 3F21 20 140 CIRCUIT FUNCTION AND SPECIFIC CIRCUIT CODE LETTERS A Armament H Heating Air Conditioning Ventilating De Icing B Photographic HA Anti icing C Control Surface HB Cabin He...

Страница 487: ...er Red White 20 Red Green 22 Red Yellow Ground 16 Black None 18 Black White Mike Ground 22 Black None Radio Lights Dim 18 Yellow None Mike Audio 22 Tan None Tan Shielded None Mike Key 22 White Black R...

Страница 488: ...18803047 SR 7201 18801069 SR 8629 18803015 SR 7402 18801375 SR 8635 18802796 18802901T SR 7639 18801510 SR 8763 18803047 SR 7669 18801825 SR 8777 18803297 SR 7684 18801617 SR 8821 18803026 SR 7803 188...

Страница 489: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 490: ......

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Страница 500: ...MODEL 188 T188 SERIES SERVICE MANUAL...

Страница 501: ...MODEL 188 T188 SERIES SERVICE MANUAL...

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Страница 516: ...MODEL 188 T188 SERIES SERVICE MANUAL...

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Страница 587: ...MODEL 188 T188 SERIES SERVICE MANUAL...

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