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Mooney M20K, Service And Maintenance Manual

The Mooney M20K Service And Maintenance Manual is a comprehensive guide for owners and operators of this high-performance aircraft. This manual covers all maintenance procedures and service requirements to ensure optimal performance. Download your free manual from our website for easy reference.

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OLDWILLWAYNE

Summary of Contents for M20K

Page 1: ...E MANUAL 3 r 1 MOONEY AIRCRAFT CORPORATION LOUIS SCHREINER FIELD KERRVILLE TEXAS 78028 IS HANDBOOK INCLUDES THE MAINTENANCE INFORMATION REQUIRED TO BE AVAILABLE BY FAR PARr23 ISSUED September 1997 MAN...

Page 2: ...TENANCE MANUAL LOG OF REVISIONS Always destroy superseded pages when you insert revised pages DATE OF RNISION CHAPTERS AFFECTED DATE OF RR ISION CHAPTERS AFFECTED 9 97 Reissue list of effective pages...

Page 3: ...manual holders when APPUCATION OF NUMBERING SYSTEM another manual is prepared to replace the subscription and advises that no more revisions will be sent out The Mooney Aircraft Corporation is in the...

Page 4: ...TSIO 360 G GB series engines X30571 for TSIO 360 LB series engines X30584 for MB sen es engines and X30671 for SE series engines MAINTENANCE AND OPERATOR S MANUAL Form Number s X30584 forTSIO 360 MB s...

Page 5: ...E LIMITS MAINTENANCE CHECKS 00 GENERAL 10 TIME LIMITS 20 SCHEDULED MAINTENANCE CHECKS 6 DIMENSIONS AND AREAS 00 GENERAL 7 LIFTING 10 JACKING 8 LEVELING AND WEIGHING 00 LEVELING 9 TOWING AND TAXIING 00...

Page 6: ...G 20 STANDARD PRACTICES AIRFRAME 00 GENERAL 21 ENVIRONMENTAL SYSTEMS 00 CABIN VENTILATION SYSTEM 40 HEATING 24 ELECTRICAL POWER 00 GENERAL 30 DC GENERATION 50 ELECTRICAL LOAD DISTRIBUTION 27 FLIGHT CO...

Page 7: ...E AND RAIN PROTECTION 00 GENERAL 30 PITOT AND STATIC 60 PROPELLERS 32 LANDING GEAR 00 GENERAL 10 MAIN LANDING GEAR AND DOORS 20 NOSE LANDING GEAR AND DOORS 30 MTENSION AND RETRACTION 40 WHEELS AND BRA...

Page 8: ...SS 35 OXYGEN 00 GENERAL 37 VACUUM 00 GENERAL 10 DISTRIBUTION 20 INDICATING 39 ELECTRICAL PANELS AND COMPONENTS 00 GENERAL 10 INSTRUMENT AND CONTROL PANELS 20 ELECTRICAL AND ELECTRONICS EQUIPMENT RACKS...

Page 9: ...ITnNGS 50 nLLETS FAIRINGS 55 STABIUZERS 00 GENERAL 10 HORIZONTAL STABILIZER 20 ELEVATOR 30 VERTICAL STABILIZER 40 RUDDER 56 WINDOWS 00 GENERAL 20 WINDSHIELD CABIN WINDOWS 50 PLMIGLASS DRILLING 57 WING...

Page 10: ...YSTEM 00 GENERAL 10 DISTRIBUTION 20 CONTROLLING 30 INDICATING 74 IGNITION 00 GENERAL 10 POWER CONTROL 20 EMERGENCY SHUTDOWN 76 ENGINE CONTROLS 00 GENERAL 10 RIGGING 77 ENGINE INDICATING 00 GENERAL 10...

Page 11: ...CHAPTER SUBSYSTEMI TITLE SECTION 80 STARTING 00 GENERAL 10 CRANKING 81 NRBINES 00 GENERAL 10 POWER RECOVERY 20 NRBOCHARGER 91 SCHEMATICS 00 GENERAL 20 ELECTRICAL SYSTEM HARDWARE CHARTS 14V 28 V 30 SCH...

Page 12: ...1100NEY AIRCRAFT CORPORATION M20K SERVICE AND MAINTENANCE MANUAL BLANK INTRODUCTION 10 OLDWILLWAYNE...

Page 13: ...CHAPTER TIME LIMITS MAINTENANCE CH EC KS OLDWILLWAYNE...

Page 14: ...Cabin Heating Ventilating systems 5 5 00 07 FuelSystem S 5 10 00 Time Limit Components 5 5 10 01 Airworthiness Limitations 6 Ovemaul and Replacement Schedule 5 20 00 Schedule Maintenance inspections 6...

Page 15: ...Effectivity 1 2BLANK 9 97 ti Contents 3 4BLANK 9 97 5 00 00 5 997 5 00 04 6 9 97 5 1 0 01 7 997 5 20 01 8 997 5 20 01 9 997 5 20 01 10 997 5 20 05 11 9 97 5 20 06 12 9 97 5 20 06 13 9 97 5 20 06 14 9...

Page 16: ...urce Hot air from the heater muff m uted prevents electric gear retraction on takeoff until a safe with ambient air controls cabin temperature Air routed flying speed is attained A gear throttle wamin...

Page 17: ...Na 292 NOTE Components should be inspected and serviced at regular intervals perthe servicing lubrication and inspection chart of this manual The general points to be covered dun ng inspection are 5...

Page 18: ...Use TeRon Threadseal Tape Oxygen Lines Use only Mil T 5542 thread 1 Continue to tighten until frtting is correctly compound or Teflon thread seal tape on threads of positioned but do not overrun or b...

Page 19: ...RQUES Untreated Screw Black Finish Fiiction Coeficient 0 14 NOMINAL PROPERTY DIAMETER CLASS Coarse Thread TORQUE Ma 5 6 8 8 10 9 12 9 Nm ft lb Nm ft lb Nmift lb Nm ft lb M3 0 60 0 44 1 37 1 01 1 92 1...

Page 20: ...t lb Nm ft lb NmPlb Nmm lb M3 0 56 0 41 1 28 0 94 1 80 1 33 2 15 1 59 M4 1 28 0 94 2 90 2 14 4 1 013 02 4 95 3 65 M5 2 50 1 84 5 75 4 24 8 1 0 5 97 9 70 7 15 M6 4 3 3 1 9 9 7 3 14 10 3 16 5 12 1 M7 7...

Page 21: ...60 M12 x 1 25 88 64 125 92 150 110 M14 x 1 25 140 103 195 143 235 173 M16 x 1 5 210 154 295 217 350 258 M18x1 5 305 224 425 313 510 376 M20 x 1 5 425 313 600 442 720 531 M22 x 1 5 570 420 800 590 960...

Page 22: ...00 6600 11000 13000 6600 8000 Coarse Thread Series 8 32 12 15 7 9 10 24 20 25 12 15 1 4 20 40 50 2530 5 1 6 18 80 90 48 55 3 8 16 160 185 95 1 00 7 1 6 1 4 235 255 140 155 1 2 13 400 480 240 290 9 1 6...

Page 23: ...ts compression Jleck To verify corection of malfunctions for security and abnormalities perform a second engine runup and a I Check cylinders for evidence of overheating flight test after completing t...

Page 24: ...tach hinge NOTE and bean ng locations including wing and empennage Cablecraft control cables are lubricated for life to fuselage mating points Operating limit replacement of control cable DO NOT remov...

Page 25: ...ecommended in paragraph 7 10 00 for SM 25 0001 thru 25 1224 the following inspections 2 PROPELLER INSPECTION H Inspect nose gear for dearhes nd damage i sped orbroicen ioli pins A Remove spinner if no...

Page 26: ...racks NOTE crazing scratches condition of seals and security of Seal all receptacles and plugs outside cabin installation environment with Dow Coming 4 D Inspect wings flaps and ailerons for corrosion...

Page 27: ...h LH 6 RH side ofwing F Check operation of pitot head heater 1 Visually Inspect doubler and mounting G Check operation of cluster gauge hardware for structrual integrity H Check operation of fuel gaug...

Page 28: ...16 25 0001 25 0780 o o Oo e O 27 27 25 0781 TEA 25 1000 THRU TEA 20 r 21 r 22 r 22 27 7 1 28 I r 2 7 Y 29 25 24 26 26 30 28 WING ACCESS COVERS MAY VARY TO SURE DEGREE BETWEEN MODEL YEAR AIRCRAFT COMPO...

Page 29: ...vator Rudder Controls Control Tube Rod End Bearings y 100 Bellcranks C 100 AIP electric pftch carder bearing assembly 100 Battery Stabilizer Tn m Control Shaft Universal Joints 3 100 Guide Blocks 0 10...

Page 30: ...vator Rudder Controls 100 Control Tube Rod End Bean ngs 9 Bellcranks Z 100 Guide Blocks O 100 nap Indicator Cable Z 100 Electde Flap Actuator Gear Box n 500 Electric Flap Actuator Ball Screw r 100 17...

Page 31: ...ote Compass Flux Valve 32 Strobdight Power Supply 33 ELT Batteries 28 Volt 8 100 LUBRICATION SYMBOL LEGEND SYMBOL MIL SPEC NO DESCRIPTION I I MlL L 7870 Low Temperature Oil 6eneral Purpose nP MIL G 81...

Page 32: ...ir Avoil Ejocon Aviation Oil EE BP Aero Oil Delta Avoil NOTE Unlan Aircraft Engine Oil i ID Mooney Aircraft are delivered with the proper breakin oil MIL L 6032 MIL C 6529C Type II or Gulfpride Aviati...

Page 33: ...SERVICE AND MAINTENANCE MANUAL M20K MOONN AIRCRAFT CORPORATION BLANK 5 20 07 22 OLDWILLWAYNE...

Page 34: ...CHAPTER DIMENSIONS AND AREAS OLDWILLWAYNE...

Page 35: ...SUBJECT Effedivity Contents 1 2BLANK 9 97 6 00 00 3 9 97 6 00 01 4 9 97 6 00 01 5 9 97 6 00 01 6 9 97 6 00 01 7 9 97 6 00 02 8 9 97 TABLE OF CONTENTS CHAPTER SECTION SUBJECT SUBJECT PAGE 6 00 00 Dimen...

Page 36: ...de Vicosity SAESOW Below 500F SAE 30 Wor 20W 50 All temperatures 15W 50 50 or 50W 65 Below 400F 30 10W 30 15W50 or 20W50 Oil Capacity 8 qts 7 57 Liters Minimum Safe OiiLevel 5 qts 4 73 Liters Oil Cons...

Page 37: ...able Absolute Press Controller TCM640655 28 Used with Airesearch Turbocharger oneraiional P ess ure Raiio PROPELLER 25 0001 thru 25 1999 Propeller Mfg McCauley Harhell Q Tip Optional Constant Speed Co...

Page 38: ...NGS A Airfoil At Wing Root 632215 B Airfoil At Wing Tip 641412 C Mean Aerodynamic Chord At Wing Sta 94 848 61 inches 154 94 cm D Center of Gravity Range 43 5 to 49 3 in 110 5 to 125 2 cm E Geometric T...

Page 39: ...K MOONEV AIRCRAFT CORPORATION I 25 5 774 7cm Tn i T f 74 _71 8 4 7 5 254cm 11 U 1 I 181 73cn I 27 9 cm 11 9 358 1cm S N 25 1225 thru 25 TEA have landingltaxi lights in k 9 3 4 c 276 2cm wings DIMENSIO...

Page 40: ...193 50 WING STATIDN RIBS STA S N 25 1000 thru 25 TEA 51375 WING STATIONS FIGURE 6 2 STA 3 68 r 1 r 1 I j STA STA STA STA STA STA STA 99 50 164 00 130 00 88 00 53 00 21 80 5 00 FUSELAGE STATIDNS SMK 6...

Page 41: ...06 so meters C Flaps 17 9 so fl 1 66 so meters D Vertical Fin 7 8 so ft 0 73 so meters E Rudder 625 se ft 0 52 so meters I Horizontal Stabilizer 21 42 so ft 1 90 so meters G Elevators 180sq ft 1 21 s...

Page 42: ...CHAPTER LIFTING AND SHORING OLDWILLWAYNE...

Page 43: ...ON CHAPTER 7 LIFTING AND SHORING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE I EfflContents 1RBLANK 9 97 7 10 00 3 9 97 7 10 00 4 9 97 TABLE OF CONTENTS CHAPTER SECTION SUBJECT SUBJECT P...

Page 44: ...be checked fore and aff boots Cushion with a layer of 3 8 inch thick hard rubber or equivalent NOTE i Install jack points in tiedown mounting holes It is not recommended to use tail tie do Yn outboar...

Page 45: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK i 10 00 OLDWILLWAYNE...

Page 46: ...CHAPTE R LEVELING AND VVEIGHING OLDWILLWAYNE...

Page 47: ...NG AND WEIGHING LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT 8 Effedivity Contents 112BLANK 9 97 8 00 00 3 9 97 8 00 01 4 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 8 00...

Page 48: ...all equipment as listed in 8 Weigh the aircraft the Weight and Balance Record 9 Find reference point by dropping a plumb bob 2 Charlie Weight Installation The aircraft as from center of nose gear trun...

Page 49: ...O IN 5 IN IN IN Distance from center Distance from Result of computation CG FUS STA Nose Gear Trunnion to Nose Gear Above a Distance Aft of Center of Main Wheel Trunnion to Datum Empty Axles Horizonta...

Page 50: ...CHAPTER TOVVING AND TAXIING OLDWILLWAYNE...

Page 51: ...F EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT 9 Effedivity Contents I12BLANK 97 9 00 00 3 997 9 30 00 4 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 9 00 00 Ground Handling 3 9 10...

Page 52: ...angle of 14 degrees either side of 1 Tum electrical switches OFF center Exceeding the turn limits shown on the turn 2 Discharge fire extinguisher into engine indicator may cause structural damage Max...

Page 53: ...SERVICE AND MANINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK 9 30 00 OLDWILLWAYNE...

Page 54: ...CHAPTER PARKING MOORING STORAG E RTN TO SVC OLDWILLWAYNE...

Page 55: ...AGE DATE SECTION SUBJECT 1 O Effedivity Contents 1 2BLANK 9 97 10 00 00 3 9 97 10 20 00 4 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 10 00 00 General 3 10 10 00 Parking 3 10 10 01 Sto...

Page 56: ...ngar the aircraft during severe w e ath erwin ds and high Oi1 10 Clean and reinstall engine air inlet filter 11 Check ignition harness lo lo ol STORAGE FLYABLE 12 Clean and regap spark plugs Outdoor s...

Page 57: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRATT CORPORATION BLANK 10 20 00 OLDWILLWAYNE...

Page 58: ...CHAPTER PLACARDS AND MARKI NGS OLDWILLWAYNE...

Page 59: ...OF EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT ii Effedivity Contents 1 2BLANK 997 11 00 00 3 9 97 i 1 20 30 00 4 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 11 00 00 General 3...

Page 60: ...NOTE Catalog All placards should be inspected for proper 11 20 30 00 PLACARDS EXTERIOR INTERIOR location readability and security during maintenance actions When an airplane has been All required plac...

Page 61: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK 11 20130 00 OLDWILLWAYNE...

Page 62: ...CHAPTE R SERVICING OLDWILLWAYNE...

Page 63: ...97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 12 00 00 Servicing 3 12 00 01 SeM cing Intervals 3 12 10 00 Replenishing 3 12 10 01 FuelTanks 3 12 10 02 Fuel Drains 3 12 10 03 Engine Oil 3 1...

Page 64: ...ns it is only necessary to remove the drains each tank to provide for drainage of moisture and and to operate the gascolator drain sediment Use the small plastic cup fumished with the flyaway kit to d...

Page 65: ...or oil continue with cleaning steps 4 through 7 pressure check 4 Soak finer in nonsudsing detergent for 15 minutes Any time fittings are disconnected on the oxygen then agitate finer back and forth f...

Page 66: ...essed or pulling 12 20 06 CLEANING 3 inspect wheels for damage Cleanliness is a major prerequisite to adequate 4 Inspect wheel bearings for condition and inspection and maintenance of an aircraft Clea...

Page 67: ...a soft cloth Never use gasoline benezene carbon tetrachloride acetone fire extinguisher fluid NOTE de icer fluid lacquer thinner or household window Foam type shampoos and cleaners for vinyl cleaning...

Page 68: ...CHAPTER STANDARD PRACTICES AIRFRAME OLDWILLWAYNE...

Page 69: ...N SUBJECT 20 Effedivity Contents 1 2BLANK 9 97 20 00 00 3 9 97 20 00 01 4 9 97 20 00 01 5 9 97 20 00 02 6 9 97 20 00 03 7 9 97 20 00 03 8 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 20...

Page 70: ...50 59 25 24 50 STA 193 50 5 1 r4 I r3 I r2 18 15 19 13 12 17 i 11 10 i 14 J L9 WING SKIN PANELS WING SKIN PANELS FIGURE 20 1 INDEX SKIN MATERIAL INDEX SKIN MATERIAL NO THICKNESS NO THICKNESS 1 0 063...

Page 71: ...EX SKIN MATERIAL NO THICKNESS NO THICKNESS 1 0 025 2024 T 3 CLAD In 0 032 2024 T 3 CLAD 2 0 040 d 2024 0 CLAD II 0 032 a 2024 T 3 CLAD 3 0 025 c b 2024 T 4 CLAD 12 0 032 2024 T 3 CLAD 4 0 025 2024 T 3...

Page 72: ...NDEX SKIN MATERIAL NO THICKNESS NO THICKNESS 1 0 025 2024 T 3 CLAD 8 0 025 2024 T3 CLAD 2 0 025 2024 T 3 CLAD 9 0 020 2024 T 3 CLAD 3 0 025 2024 T 3 CLAD 10 0 032 2024 T 3 CLAD 4 0 025 2024 T 3 CLAD 1...

Page 73: ...when the aircraft A few simple precautions will prevent chemical is being washed Rinse aircraft e derior after e q osure corrosion to salt air or industrial fallout 1 Be sure battery vent is free from...

Page 74: ...now be ready for priming and painting C Apply zinc chromate pn mer to cleaned area by b On steel Remove all grease gn me loose spray or brush Area needs to be painted within 24 paint eic by wiping wi...

Page 75: ...e stripped of all paint prior to repainting h is required that repainted 1 Apply three coats of white base andlor color control surfaces be removed and rebalanced finish allowing three to five minutes...

Page 76: ...CHAPTER AIR CON DITIONI NG OLDWILLWAYNE...

Page 77: ...TAL SYSTEMS LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT 21 Effedivity Contents 1 2BLANK 9 97 21 40 00 3 9 97 21 40 00 4 997 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 21 00 0...

Page 78: ...lot and co pilot seats Individual fresh air removed This will provide a continuing check for the outlets are located on each side of the cabin side prevention of carbon monoxide in the cabin Any panel...

Page 79: ...SERVICE AND MAINTENANCE MANUAL M20K MOONN AIRCRAFT CORPORATION BLANK 21 40 00 OLDWILLWAYNE...

Page 80: ...CHAPTER ELECTRICAL POVVEF OLDWILLWAYNE...

Page 81: ...g Procedures 8 24 35 00 Lighting Circuits 9 24 3600 Landing Gear Circuits 9 24 37 00 FuelSystem Circuits 9 24 38 00 Miscellaneous Circuits 11 24 39 00 TroubleShooting Charts 11 24 39 01 AltematorTroub...

Page 82: ...ts 3 4BLANK 9 97 24 00 00 5 9 97 24 31 02 6 9 97 24 32 00 7 9 97 24 34 00 8 9 97 24 35 00 9 9 97 24 37 00 10 9 97 24 38 00 11 9 97 24 39 00 12 9 97 24 39 02 13 897 24 39 03 14 9 97 24 39 04 15 9 97 24...

Page 83: ...ng current for simuRaneous on main circuit breaker panel Reset if open operation of multiple radios anticollision lights and C Inspect battery for corroded cable connections navigation lights On S N 2...

Page 84: ...ircraft for 15 to 20 minutes charging rate altematbr removal process should slowly drop to 10 amperes or less A very low battery will take longerto show a drop in charging current Belt Dn ven Alternat...

Page 85: ...and Low Vacuum Waming Circuit A switch 25 0999 30 voltsfor 25 1000 thru 25 TEA in the vacuum system controls the vacuum waming NOTE light on the annunciator panel Vacuum below 4 25 IN Use bushings pro...

Page 86: ...ged and the fast recharge 5 Turn Master Switch OFF set annunciator from the higher potential source battery aitemator Cal Switch to Norm position install annunciator generator rectifier etc will sever...

Page 87: ...ci no OFF when MASTER switch Is turned OFF if door b actuator stops The gear up limit switch controls the closed landing gear un safe light The red light comes on 4 Anti Collision Lights A circuit bre...

Page 88: ...Conned the positive lead to the slide resistor LOW POSITION Adjust the power supply voltage level to 13 75 25 volts 25 0001 thru 25 0999 28 6 t 25 volts for 25 1000 thru 25 TEA Adjust the slider REAS...

Page 89: ...ter e dinguished A cigarlighter is mounted in the n ght instrument panel F Tum Left AReemator OFF and turn Right 5 Current Sensor Monitor Alternator ON Reference Figure 24 3 G Repeat Steps E 3 F with...

Page 90: ...ttery charged RPM Ammeter should indicate a heavy charge rate with all electrical equipment tumed off Rate should taper off in 1 3 minutes A voltage check at the bus should indicate a reading of 13 75...

Page 91: ...ance is low repair or replace a 1250001 25 0999 243992 GENERATOR TROUBLE SHOOTING For Standby Generator 25 0001 thru 25 0999 TROUBLE PROBABLE CAUSE REMEDY Generator operating within Generator operatin...

Page 92: ...Y TROUBLE SHOOTING TROUBLE PROBABLE CAUSE REMEDY Discharged battery Battery worn out Replace battery Improper charging rate setting Reset charging rate Excessive discharging Tum off some equipment whe...

Page 93: ...all wiring Binding wom improperly seated BNshes should fit free in brush brushes brushes have boxes without excessive side excessive side play play Clean binding brushes and brush boxes with a Varsol...

Page 94: ...ament of DSI Assy A2 open 3 The gear down lamp is dim when the position lights are off CR24 Assy A open 4 The gear unsafe lamp will not light dun ng TEST but does light when the gear is in transit CR3...

Page 95: ...igh or low vacuum situation Filament of DS5 AssyA2 open 07 Assy Al defective 20 The high low vac lamp will not light in a low vacuum situation but does light in a high vacuum situation 08 Assy Al defe...

Page 96: ...ls previously dimmed and near 0 is not intended to serve as a bench service aid in that VDC to reset the dimmed channels to a bright reference designators in various Figures are not condition The chan...

Page 97: ...discussed herein Signals from the junction of the left and n ght fuel transducers and the left and n ght fuel quantity gauges are applied respectively to each of the inputs INPOS3 4 0 LANDING GEARIND...

Page 98: ...esistor R29 which reduces the brilliance of the lamp In the bright mode R29 is shorted by 06 and nH g a CR13 which provide a low impedance path to ground oX Transistor 06 is controlled in condudion by...

Page 99: ...07 CRI1 R23 6 61 SOi L 6UPC ES1 I t C L_UY N J I ff l R V5 U I 3 fi IP I1 DC j uc33oz uJ D 40 4J r 1 1 Pu IOK cs e os Ds vDC R g 3 17 n ar csx cia tK 19 Izxi CRII llOK Rca Rjg BK 4R 7 tttJ LMXt Pt 2u...

Page 100: ...left altemator regulator and one signal derived intemally that R63 indicates that the aircraft bus voltage is less than 26 5 CR27 VDC When low voltage is detected internally or when IN 005 low curren...

Page 101: ...educed in value below drives Q12 into conduction regardless of the states of the voltage set by R83 the comparator Us goes high either comparator U6 or U7 Similarly TEST will dn ve and drives 013 into...

Page 102: ...two parallel paths The path to provide a dim indication is through resistor R85 which reduces Y the brilliance of the lamp In the bn ght mode R85 is shorted by 014 and CR34 which provide a low impedan...

Page 103: ...ator and from the generator to the standby generator bus This will allow battery through the battery relay The negative battery limited equipment to be operated until aircraft can be lead attaches to...

Page 104: ...CHAPTE R FLIGHT CONTROLS OLDWILLWAYNE...

Page 105: ...50 00 Wing Flap System 11 27 60 00 Aileron Rudder Inter conned System 12 27 90 00 Miscellaneous 27 91 00 Control Surface Static Balancing 12 27 92 00 Equipment Maten als Static Balancing 12 27 93 00...

Page 106: ...ECTION SUBJECT a l Effedivity 1 2BLANK 9 97 27 Contents 3 4BLANK 997 27 00 00 5 9 97 27 20 00 6 997 27 20 00 7 9 97 27 30 00 8 997 27 31 00 9 9 97 27 40 00 10 9 97 27 40 01 9 97 27 60 00 12 9 97 27 93...

Page 107: ...down and for than occasional lubrication Specially designed aluminum alloy extrusions that permit Rush skin at ward to allow aileron balance weights to clear wing tip tachment form the leading edges...

Page 108: ...st remaining control tubes F B D Figure 27 1 1H and R H if applicable in order to freely attach to the bellcranks and jackshaft E Remove n g pins F Adjust aileron stops Reference Figure 27 2 per parag...

Page 109: ...NIZO 44 S1 27 3A F Unclamp rudder pedals G Adjust rudder stops M F ure 27 8 so that FIGURE 27 3A TRAVEL BOARD LOCATIONS rudder travel is 23 degrees 1 0 degrees right and left travel may be bent to obt...

Page 110: ...HORN ADJUSTMENT 27 30 00 ELEVATOR SYSTEM C Remove elevator to the rear Elevator construction is essentially the same as that of D Install elevators in reverse sequence of removal the ailerons Both el...

Page 111: ...ermissable Check for positive clearance betuYeen cable and pulley sheave C Set stops P Figure 27 8 in empennage stinger for elevator ptravel and downtravel of 20 A Set stabiber to maximum negative pos...

Page 112: ...control A Loosen setscrew in stop A Figure 27 10 Turn n gging is now complete stop A clockwise or counterclockwise to align aff edge 3 Stabilizer Tr un Indicator Rigging of stop A with last thread of...

Page 113: ...the down inch diameter position and located on the console adjacent to the flap position indicator The flaps can be retmcted com pletely by placing the switch in the up position or to WHEEL any settin...

Page 114: ...27 brackets on rudder control tube so the in E Install wing flaps in reverse sequence of Stalled length of each spn ng is 4 90 in Clamp bracket in place dnll through brackets and into control tube rem...

Page 115: ...ife edges and level hinge line if a 12 oz gauge weight is used 28 oz SM 25 1000 RISM control surfaces should be balanced inverted for thru 25 TEA computation of moments will not be greater sensit rvit...

Page 116: ...cked NOTE The absolute limits must be satisfied if a different balance procedure is used requiring calculation of balancing moments CONTROL SURFACE CONTROL WEIGHT UMIT GAUGE WEIGHT 12 DESCRIPTION DIST...

Page 117: ...27 19 NOTE B Rudder The rudder trailing edge may be If balance limits cannot be met with existing trimmed right or left as required weight on any control surface a lighter or heavier C Elevator A ful...

Page 118: ...st flights before the desired setting can be reached access cover aft of the switch on the lower wing The stall waming should actuate at no less than 5 KTS nor more than 10 KTS preceding the stall and...

Page 119: ...tem components U til proper operation in night is obtained identification 27 96 02 MAINTENANCE SPEED BRAKE SYSTEM 27 96 01 SPEED BRAKE CARTRIDGE REMOVAL AND REPLACEMENT ELECTRICAL OR VACUUM SYSTEMS 1...

Page 120: ...SERVICE AND MAINTENANCE MANUAL M20K MOONN AIRCRAFT CORPORATION BLANK 27 96 02 18 OLDWILLWAYNE...

Page 121: ...CHAPTER FUEL OLDWILLWAYNE...

Page 122: ...0 Gascdator Screen Cleaning 11 2 23 00 Fuel Injection System 11 28 24 00 Engine Priming 11 2 25M Fuel Selector Valve Removal and Installation 11 11 2830 00 Dump 2831 00 Fuel System Drains 11 28 32 00...

Page 123: ...E PAGES CHAPTER SECTION SUBJECT PAGE DATE 28 Effectivity 1 2BLANK 997 28 Contents 3 4BLANK 9 97 28 00 00 5 9 97 28 10 00 6 9 97 28 11 00 7 9 97 28 12 00 8 9 97 28 12 00 9 9 97 28 13 00 10 9 97 28 22 0...

Page 124: ...INE SUPPLY LINE L riE SELECTOR wL taSCOU Cs IJ SETU N LINE BOOST PUMP SwlTCHES InER SwlTCH HI ENCI I l f r fCE P P FCEL FLJ 2 LCI 80051 PU P I Ir C I E I II DPI Lc r _LI FUEL SYSTEM FIGURE 28 1 2 The...

Page 125: ...ter Sealants may also be obtained from SMX28 2 Products Research Co 5454 San Fernando FUEL FILLER CAP ASSEMBLY MAINTENANCE Road Glendale CA 91209 Ph 800 423 2411 or FIGURE 28 2 Chem Seal Corp 11120 Sh...

Page 126: ...circulate through tank access covets B Sealant Mi dng NOTE 1 For best results use kits with proper proportions of base compound and accelerator Sealant in tube form have mixing instructions on each tu...

Page 127: ...aled 1 Apply a coat of access door sealant PR 1403 EB2 to either faying surface using a short stiff NOTE bristle brush spatula or extrusion gun If an extrusion Refer to Mooney SE M20 230 for proper gu...

Page 128: ...stener head on fuel tank e derior immediately after area is wiped clean For a temporary repair to be satisfactory structural 4 Running Leak A fuel leak that flows i tegrity must be retained in leak ar...

Page 129: ...ning Wax allows excess fuel to return to the supplying tank Carbo Wax 1500 through a separate retum line C Thirteen ounces Alkaryl Sufonate wetting agent 28 21 00 FUEL BOOST PUMP REMOVAL AND D Distill...

Page 130: ...skins directs the fuel to two atomizing nozzles in the forward 2 40 00 INDICATING end of the induction risers See TCM engine overhaul 28 41 00 FUEL QUANTITY INDICATING manual for servicing instructio...

Page 131: ...utboard outer wing surface and record total quantity less the float may be adjusted if required for 1 2 and 314 gauge unusable fuel readings 28 43 03 FUEL QUANTITY GAUGE 5 Finish filling tank and veri...

Page 132: ...leak in system Repair leak 28 92 00 FLARED FITTINGS relubricated before they are reinstalled Torque all fit tings in accordance with flare fitting torque chart When installing flared fittings and hose...

Page 133: ...MOONEY AIRCRAFT CORPORATION M20K SERVICE AND MAINTENANCE MANUAL BLANK 28 92 00 14 OLDWILLWAYNE...

Page 134: ...CHAPTER ICE AND RAIN PROTECTION OLDWILLWAYNE...

Page 135: ...3 30 30 00 Pitot oeschptidn g Operation 3 30 60 00 Propellers Descn ption 8 Operation 3 30 60 01 Schematic Propeller De ice 4 30 61 00 SeM ce Guide 4 30 61 01 HelpfulTips 4 30 61 02 TroubleShooting Ch...

Page 136: ...l go full defledjon each 90 seconds as the OPERATION timer turns the de ice boots ON OFF ON SM 25 1225 A standard heated pitot tube is located on the left wing thru 25 TEA have a BLUE light PROP DE IC...

Page 137: ...normal operating modes of the system See 4 A conside able number of timers have been returned Section IX of P O H Read all of the Trouble entn es for repair which proved on test to be fully operable t...

Page 138: ...r leads See de icing system wiring schematic for power and ground lead and pin identification If low or no voltage locate and coreet open or high resistance in wire harness Check continuity from appro...

Page 139: ...De leers for loose or corroded connections or partially broken win ng Correct as required Ammeter shows low current over Aircraft voltage low under Check voltage into switch entire cycle normal operat...

Page 140: ...rush assembly WRh between two adjacent Megger check insulation circuits slip n ngs to De leers resistance from one rign of slip n ng assembly to bare prop Reading should be as least 5 Megohoms after o...

Page 141: ...and the de icer switch in the ON position At some convenient point between bus bar and check voltage from Pin B 12V Ifrom wire from shunt ammeter connect a volt ohmmeter with an ammeter 24Vll of the...

Page 142: ...test range ohmmeter Ifthe resultant readings are not 1 55 one in the pilot s compartment to monitor the ammeter to 1 78 ohms disconnect De leer lead straps to while the other checks the De leer boots...

Page 143: ...CH OF BRUSHH SHOULD BE ALLOWED TO PROTRUDE FROM BRUSH BLOCK THIS IS THE NORMAL POSITION OF THE BRUSH WHEN INSTALEI ON THE AIRCRAFT SMM30 2 MEASURING BRUSH WEAR FIGURE 30 2 Qol 3E2042 1 V g Su O cEwnn...

Page 144: ...e of plastic housing replace with same part for brush to slip ring alignment number module 30 69 00 ALIGNMENT OF SUP RING D Restack modules and spacers as shown Figure 30 2 Check AIB C or A B 24V stac...

Page 145: ...ging the torque of mounting recommended Keeping the brushes rree of dirt oil screws or bolts grease and carbon build up will prevent those contaminants from being transferred to the slip n ng If the s...

Page 146: ...CHAPTER LANDING GEAR OLDWILLWAYNE...

Page 147: ...1000thru25TBA 11 32 30 03 Nose Ldg Gear System Rigging 13 32 30 04 Emergency Gear E dension System Fiigging 14 32 30 05 Landing Gear Actuator Clutch 15 32 30 06 Landing Gear Actuator 16 32 30 07 Manua...

Page 148: ...00 5 9 97 32 1 0 02 6 9 97 32 1 0 05 7 9 97 32 1 0 06 8 997 32 20 03 9 897 32 30 02 10 897 32 30 02 11 9 97 32 30 02 12 9 97 32 30 03 13 9 97 32 30 04 14 9 97 32 30 05 15 9 97 32 30 06 16 9 97 32 32...

Page 149: ...me 5 Detach main gear retracting tube M Ftgure 32 mdybdenum tubular steel heat treated for greater 9 from retracting truss G and remove bolts H from strength and wear resistance Main gear attaching re...

Page 150: ...ct gear while checking for binding in door linkage and proper contact of gear door edges with 5 If adjustments are required adjust outboard gear wing DO NOT make final gear door adjustments until door...

Page 151: ...to adjust then retract to check this may result in higher actuator loads than adjustment necessary 4 Check main gear overcenter preload torque for 3 Adjust outboard door link to close all gap at prop...

Page 152: ...Heim d end bean ng and AN4 NOSE GEAR INSTAUA TION bolt through block Torque and safety 32 20 02 1 Lubricate wheel bean ngs retraction linkage and CAUTION left and right mount bearings Bump gear up CA...

Page 153: ...g thumb on rear end of tool S and press for eccentrics have been moved Figure 32 4 IC ward B Hold 10 torque wrench R and place thumb 32 30 00 EXTENSION AND RETRACTION on wing bottom apply force until...

Page 154: ...ic NOTE o rigged position to be OJO to 070 in This is a starting point only This dimension may vary to permit retraction tubes to connect NOSE GEAR BUNGEE SPRING FIGURE 32 6 with zero preload 4 Tth be...

Page 155: ...ungee assy and insert 3 16 in pin wrenchlshim stock procedure after electrical CAREFULLY BUMP the gear UP with the gear safety extension bypass swrtch untii there is zero load on bungee SIN 254000 thr...

Page 156: ...s 8 tighten set hole screw c 27 Reinstall assist bungee per Section 32 1 10 With main retract bellcrank held in position tum 28 Using emergency gear extension move gear actuator barrel nut until rod e...

Page 157: ...condition LANDING GEAR WARNING ADJUSTMENT 3 Measure nose gear bungees dimension P Fig 1 Check that landing gear waming light circuit 32 6 and record for future reference breaker is pushed IN 4 Push la...

Page 158: ...11 dure stopping when gear down light JUST illuminates aside re engage RED lever Check manual extension 15 Measure nose gear bungee assemblies dimen system to verify that it is fully disengaged by pul...

Page 159: ...htly Reference S I M20 52 forAvionics Products actuator CAUTION DISASSEMBLY AVIONICS PRODUCTS Use extreme care to prevent ball bearing from i Remove two nuts item 1 Note position of cable dropping out...

Page 160: ...ar 3 Remove two 2 recoiler spn ngs and two 2 of 1 Pull landing gear actuator C B three 3 spring spacers leaving the third spacer in 2 Move landing gear control switch to DOWN housing Be certain that s...

Page 161: ...ve circuit breaker obstructions Examine pressure tn pped or actuator ball nut binding switch for proper adjustment and on mechanicaC DOWN STOPS operation Reset circuit breaker Does gear ret act using...

Page 162: ...ast 30 32 40 02 MAIN WHEEL DISASSEMBLYI minutes Remove cup by tapping evenly ASSEMBLY To install cup heat wheel half again and then cool cup i Remove snap n ng 10 grease seal n ngs 8 and with dry ice...

Page 163: ...pam safety wire and two AN4H17A bolts 1 attaching back 332 a sn lining plate assembly 2 to brake cylinder assembly Figure 32 15 18 Remove aircraft from jacks C Visually inspect linings for wear and br...

Page 164: ...t heat to cure resins in the lining but will not cause the maten a to wear of 0 ring A scored brake cylinder should be become carburized due to excess n e heat replaced 3 MASTER CYLINDER REMOVAL J Rep...

Page 165: ...es 11 Inspect push rod for scoring grooves nicks and scratches 12 Inspect spn ng 4 for free height 500 in 030 12 Inspect piston return springs 2 for permanent set and proper length 3 670 in mi 4 05 13...

Page 166: ...allowable limit Spongy brake Air in system Bleed brake system Pressure will not hold Leak in brake system Visually check entire system for evidence of leaks Parking brake will not hold Air in system...

Page 167: ...and right travel position SB20 326092 NOSE GEAR STEERING AND SPACER PLU AB LINE TRACKING 1 Level aircraft as described in Chapter 5 2 Center nose wheel 3 Place plumb line over and foMlard of nose gear...

Page 168: ...0781 8 ON Manifold Pressure INSPECTION Check warning hom for volume in flight pen odically Hom will sound if gear is not DOWN and LOCKED 1 Aircraft with full fuel load and we M on landing gear even if...

Page 169: ...e spacers 5 being used The dimension T in a no load fully extended position should be a E Insped nose gear snubber shock absorber if nominal 3 0 inches Add spacers to either top installed for proper s...

Page 170: ...MOONEY AIRCRAFT CORPORATION M20K SERVICE AND MAINTENANCE MANUAL BLANK 32 81 00 26 OLDWILLWAYNE...

Page 171: ...CHAPTER LIGHTS OLDWILLWAYNE...

Page 172: ...33 21 02 Cabin Light Switch Replacement 4 33 22 00 Instrument flight Panel and Glareshield iights 5 33 22 01 Light Bulb Replacement 5 33 23 00 Gear Down Indicator Light Floorboard 6 33 23 01 Light Bul...

Page 173: ...desired The rocker switch light circuits are mounted in a housing designed to isolate the bulbs muted through a timer and the Master Switch and will go from engine heat and vibration The lights are a...

Page 174: ...oving the screws 3 holding panel in place 3 A II ii A i Figure 33 1 NOTE I rwn valve for the overhead ventilation that must be S N 25 0247 and ON have a butterfly shut off freed from the panel prior t...

Page 175: ...nd ty rap 5 Re assemble in reverse order securely 33 22 00 INSTRUMENT FLIGHT PANEL AND F Check for proper operation GLARESHIELD LIGHTS 4 Trim Flap Indicator Light 33 22 01 LIGHT BULB REPLACEMENT SRJ25...

Page 176: ...ctive fi dure Replace fudure LANDING LIGHTS NAVIGATION LIGHTS AND TAILLIGHT Lamp fails to light Circuit breaker switch tn pped Check for short circuit Reset circuit breaker Lamp bumed out Replace lamp...

Page 177: ...cated onthe leftside ofthe airplane 1 Wing tip strobe power supply a The power supply unit is mounted on the vertical A Gain access to wing tip po ver supply through bulkhead forward of the inspection...

Page 178: ...y a strobe light switch for the strobe lights OFF and allow at assembly is located on 24V aircraft Removal is same least 20 minutes to elapse prior to as combination 12V NAV STROBE light assembly dirs...

Page 179: ...ou will need this to pull the new wire harness back in place dun ng installation Remove cord B Remove the two screws 2 hokling the position from wire harness light lens in place H Replace complete fla...

Page 180: ...sition UH 6 RR1 main landing gear at exact distance from vertical wall ie parallel to wall 2 Place four target crosses on vertical wall at 2 1 i the following positions A 36 5 inches up vertical wall...

Page 181: ...CHAPTER NAVIGATION OLDWILLWAYNE...

Page 182: ...0 Airspeed Indicator 4 34 11 01 Airspeed Indicator Troublesh otins 4 34 12 00 Vertical Speed Indicator 4 34 12 01 Rate Of Climb Indicator Trouble Shooting Olertical Speed Indicator 4 34 1 3 00 Aitimet...

Page 183: ...hroughlines from the instrument panel make sure that no air is blown into instruments Static pressure instruments are e ctremely sensitive to pressure changes therefore the pitot and static 4 Static s...

Page 184: ...o zero the indicatorwhen the aircraft is on the ground This instrument has a single needle and two adjoining scales that read from 0 to 2000 feet per minute top 34 1 261 RATE OF CLIMB INDICATOR TROUBL...

Page 185: ...tometn e scale and Slippage of mating parts Replace instrument reference markers are out of synchronization 34 2090 DIRECTIONAL GYRO COMPASS directional heading Vacuum pressure for satisfactory This v...

Page 186: ...low temperature bar fails to Oil has become too thick Replace instrument respond or responds sluggishly and with insufficient deflection Insufficient bean ng clearance Replace instrument Bar sluggish...

Page 187: ...ed damping liquid Defective light Burned out lamp or broken Check lamp or wiring continuity circuit 34 23 00 ARTIFICIAL HORIZON Maintenance is similar to that required for the directional gym compass...

Page 188: ...Dirtyairfiiter i Examine filter and clean or replace if necessary 2 Vacuum regulating valve 2 Adjust valve improperly adjusted 3 Defective mechanism 3 Replace instrument 4 Excessive vibration 4 Test...

Page 189: ...CH APTE R OXYGEN OLDWILLWAYNE...

Page 190: ...APTER PAGE DATE SECTION SUBJECT 35 EffedivitylContents I 2BLANK 9 97 35 00 00 3 9 97 35 00 02 4 9 97 35 00 02 5 997 35 00 02 6 897 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 35 00 00 Gener...

Page 191: ...d by eitherthe and clothing are clean particularly with respect control handle being pushed forward S N 25 0001 to oil or grease for these will IGNITE upon thru 25 0780 or the control knob rotated 250...

Page 192: ...required for this servicing however several types of standard oxygen fittings are in use and F If leakage exists apply MIL L 25567 leak test a compatible fitting for the Scott Recharging Valve 2 solu...

Page 193: ...tment bulkhead Access to cylinder is obtained thru radio compartment access door or left position side of aircraff behind leff wing F Plug one oxygen mask 14 into pilots outlet 8 to check for proper s...

Page 194: ...ecause of this merely filling to 1850 PSIG will not result in a properly filled cylinder Fill to pressures indicated on Figure 35 2 for ambient temperatures AMBIENT FILLING AMBIENT FILLING TEMPERATURE...

Page 195: ...CHAPTER VACUUM OLDWILLWAYNE...

Page 196: ...einstall 6 37 1 2 05 Adjustment 6 37 1 3 00 Filters 7 37 13 01 Maintenance Practices 7 37 1 3 02 Servicing 7 37 1 3 03 Removal 7 37 1 3 04 Reinstall 7 37 1 4 00 Hoses 7 37 14 01 Maintenance Practices...

Page 197: ...IRCRAFT CORPORATION CHAPTER 37 VACUUM LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT 37 EFF 1 2BLANK 9 97 37 CONTENTS 3 4BLANK 9 97 37 00 00 5 9 97 37 1 1 02 6 9 97 37 1 3 00 7 997 37 30 00...

Page 198: ...0K 1 Dry air pump coupling aircraft This kit can be installed by the factory or in the field The standby vacuum system should be activated CAUTION manually when low vac light flashes on regular engine...

Page 199: ...nstall a pump that has been dropped 1 Undemeath instrument panel remove both instru ment lines from vacuum regulator cap to prevent 1 Consult airframe manufacturer s current parts foreign objects from...

Page 200: ...nunciator panel the instruments 37 21 01 DESCRIPTION 37 13 04 INSTALLATION The switch is a low and high vacuum sensing adjus i Prior to installing a new vacuum regulator filter table unit check regula...

Page 201: ...37 30 00 DRY AIR PUMP REPAIR 5 Push engine coupling drive gear 2 into place on It is not recommended that the Airborne Dry Air Pump pump drive coupling 1 be repaired Remove the faulty pump and instal...

Page 202: ...CHAP ER OLDWILLWAYNE...

Page 203: ...02 Avionics Equipment 6 39 10 03 Engine Instruments and Circuit Breakers 6 3411 00 night Instrument Panel 6 39 11 01 Cluster Gauge 7 39 11 02 Landing Gear Switch 8 39 11 03 Landing Gear Safety Overri...

Page 204: ...LECTRICAL PANELS AND COMPONENTS LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT 39 Effedivity 1 2BLANK 9 97 39 Contents 3 4BLANK 997 39 00 00 5 997 39 1 0 02 6 9 97 39 11 01 7 997 39 1 1 02...

Page 205: ...l on either side of cover plate carefully lift glareshield to expose discon the pilots control column nects for glareshield lights Disconnect wires and lift The cluster gauge containing fuel quantity...

Page 206: ...ircuit breaker through panel any instrument or circuit breaker 2 Installation 1 Removal A Installation of new instrument or circuit breaker A Remove glareshield refer to Section 39 10 01 i to panel is...

Page 207: ...auge will require removal from panel to allow room to pull modules out LIGHT BULB ACCESS s o sM SMD m YN r VIEW LOOKING AT BACK SIDE OF PILOT S PANEL MODULE TERMINAL SIU S CONFIGURAT1ON OF CLUSTER GAU...

Page 208: ...ibration Gauge indicates 1 2 when On dual sender systems the tank is full isolated sender may be grounded The lead between the isolated sender and the grounded sender is grounded Either sender defecti...

Page 209: ...er and 3 Loosen nut on stem and hold nut located inside push switch through face of panel Disconnect wires mounting bracket The red lensmay need to be removed emove and replace defective switch to ful...

Page 210: ...ment bulkhead Access is gained through the large access INSTRUMENT AND RADIO LIGHT CONTROL BOX door in tailcone aft of the left wing trailing edge The FIGURE 39 5 battery and battery box auxiliary pow...

Page 211: ...CHAPTER STANDARD PRACTICES STRUCTURES OLDWILLWAYNE...

Page 212: ...Repair 10 51 13 03 Stub Spar Repair 11 51 13 04 Rear Spar Repair 13 51 13 05 Rib Repair 13 51 13 06 Wing Tip Repair 13 51 13 07 Wing Skin PanelRepai 13 51 14 00 Horizontal Stabilizer Vertical Fin Repa...

Page 213: ...LANK 997 51 Contents 3 4BLANK 9 97 51 00 00 5 997 51 10 01 6 897 51 11 00 7 997 51 12 01 8 897 51 12 01 9 9 97 51 12 02 10 997 51 13 03 11 997 51 13 03 2 997 51 13 04 13 9 97 51 13 07 14 9 97 51 14 00...

Page 214: ...ille Texas should connect the main spar to the stub and rear spar A be consulted for special repair procedures when repair stretch formed skin wraps around the leading edge n bs of damaged str jdure i...

Page 215: ...to drill for and install the ne d is oversize standard size larger diameter rivet of the same type and maten al as the original n vet 1 Machine Countersink Joint If the edge distance is a minimum of...

Page 216: ...d for 4 AN BOLT NUT AND WASHER replacement can be purchased from SERVICE PARTS INSTALLATION To compensate for material thickness DEPARTMENT Mooney Aircraft Corporation Louis tolerances the length of A...

Page 217: ...IDE 5A INNER SLEEVE SPLICING FIGURE 51 2 secure in position with a rosette weld on each side at G Weld the inner sleeve to the tube stubs through one half the on ginal tube diameter from the the 8 inc...

Page 218: ...insert B Form the split sleeve from sheet steel when an inner sleeve see Figure 51 3 outside diameter of the original tube is one inch or A Form the split sleeve from steel tube or sheet more steel wh...

Page 219: ...system tem components is not recommended Use only new tubing or assemblies engine mounts or heat treated hardware when installing new parts After installation of steel components except as stated belo...

Page 220: ...ch is completely where the protective coating has been removed 2 SPAR CAP REPAIR Spar caps outboard of STA 3 SPAR WEB REPAIR Repair all damage to spar webs in accordance with AC 43 13 If there is 103...

Page 221: ...OF WSTIHG STTZIHGERS 5 PER smo 0 0000100QOOI 750 WC O 750 5 5 RR Spg SPLICE 1 82 2014 76 000000 O000000 d a PER smo SNi15Id STRINGER REPAIR FIGURE 51 6 SPLICE ANGLE HATERIAL17075 T6 875 WO rid 688 15...

Page 222: ...e to gain ac together using wet primer on all rivets cess to stn ngers for rivet bucking Rivet skin to upper stn ngers 51 13 04 REAR SPAR REPAIR 6 Rivet skin to tip rib starting at leading edge Buck r...

Page 223: ...o 9959 rrpurr vr 999 99 mcc n 995 9 REIYP 599 RV m Hmr rri 950 ama 9 99 99 o D o o o o o o I o oo o oooooooooo 7AO 4 On r REPUCD PIOr 9e9L REAR SPAR REPAIR FIGURE 51 9 RIB REPAIR FIGURE 51 10 1 I I 1...

Page 224: ...red by sanding out thecrack Cracks in dimples which do not extend beyond the dimple radius can be repaired by a stop drilling the crack with a No 60 drill b and b by adding rivets the same size as tho...

Page 225: ...34 0 and spar web See Figure 51 15 on the spar upper flange and between STA 9 00 and STA 40 0 on the spar Ibwer flange with a splice angle 2 Repair main spar cap damage between STA 34 formed from 070...

Page 226: ...rill 10 rivet holes through stinger remating can be facilitated by using huckbolt splice angle and web on each side of the damaged substitution information contained in Section 51 10 01 web area The d...

Page 227: ...s from the cracked portion Hardner 3 Prepare surface for repair as shown in Figure United States Gypsum OR 51 20 Figure 51 21 and Figure 51 22 Resin Ren Epoxy CG 1304 4 Prior to continuing the repair...

Page 228: ...n paragraph 5 5 Apply one additional ply of 181 cloth bridging 5 Place rigid aluminum plates on both sides of the total repaired area and bond in place repair area and clamp into place with C clamps P...

Page 229: ...ickness 10 Mix epoxy resin and catalyst per manufacturers 4 Apply one layer of 181 fiberglass cloth to the specifications and apply to the appearance surface non finished side of laminate extending 1...

Page 230: ...ne Splices may be repeated to acquire a satisfactory surface Static system lines may be lengthened shortened or finish spliced to allow the replacement of sections of damaged lines The fittings are ca...

Page 231: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK 51 16 00 22 OLDWILLWAYNE...

Page 232: ...CHAPTER DOQRS OLDWILLWAYNE...

Page 233: ...00 4 997 52 12 00 5 9 97 52 31 00 6 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 52 00 00 General 3 52 10 00 Cabin Door Maintenance Practices 3 52 11 00 Cabin Door Rigging Adjustment Pr...

Page 234: ...the door within door frame to obtain proper sealing baggage door closed Refer to AFM POH Section III A Place door with new hinge installed into posi for specific procedures to operate auxiliary exit h...

Page 235: ...abin door latching mechanism has several 1 Adjust cabin door linkage to satisfy requirements adjustment points that may be utilized to obtain proper listed below 7 SLID OYP13_6 LATCH JAWS 9 ADJUSTME P...

Page 236: ...ean hinge and hinge mounting area open and slide cam at end of its full travel thoroughly of all sealant or foreign material NOTE 2 Repair Slide cam 7 moves 1 13 in from the full latched The baggage d...

Page 237: ...nd door The outside handle has to be unlatched and fully frame opened and inside mechanism secured to correctly re H Reinstall door assembly and cleco securely in engage latching mechanism after use o...

Page 238: ...CHAPTER FUSELAGE OLDWILLWAYNE...

Page 239: ...9 97 53 40 02 7 9 97 53 40 03 8 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 53 00 00 General 3 53 10 00 Main Frame 3 53 1 0 01 Tubular Structure Frame 3 53 10 02 Tailcone Structure 3...

Page 240: ...indshield Earlier aircraft had the tubular structure dipped in zinc chromate primer after sand blasting frame that will not accept the radar display unit S N The tailcone bulkheads forners etc are for...

Page 241: ...ular structure is covered with See Figure 53 3 aluminum skins after mating to tailcone The skins a e The belly skins are removable to provide access to all riveted and bolted to support angles forners...

Page 242: ...AIRCRAFT CORPORATION M20K SERVICE AND MAINTENANCE MANUAL II k 4 1 25 II I 6 6A 81 22 0 11 12 13 12 23 21 18 1 9 i 17 2 15 16 24 28 2131 AND ON INSPECTION PANEL AND COVERS FIGURE 53 3 53 30 00 OLDWILL...

Page 243: ...il Light Harness Connections Travel Stops 23 Empennage Attachment Trim Jack Screw 10 Rudder Controls Elevators Rudder Bellcranks 11 Brake Master Cylinders Rudder Torque Tube 24 All components 12 18 21...

Page 244: ...ached empennage assembly secures stabilizer trim jack to rear bulkhead 3 Figure 53 6 of tailcone The screw 5 Figure 53 5 and 4 Figure 53 6 Lateral hinge attach pin 6 Figure 535 is held in place with s...

Page 245: ...hould be inspected at any scheduled main r tenance action for wear Grease fittings 8 are installed at pivot points of main landing gear assembly for lubrication per Section 5 Reference Figure 53 7 53...

Page 246: ...CHAPTER STABILIZERS OLDWILLWAYNE...

Page 247: ...PAGE SECTION SUBJECT 55 00 00 General 3 55 1 0 00 Horizontal Stabilizer 3 55 1 0 01 HorizontalStabilizer Removal 3 55 1 0 02 Horizontal Stabilizer Installation 4 55 20 00 Elevator 4 55 20 01 Elevator...

Page 248: ...ft vertical fin spar 11 is attached to horizontal The elevator and rudder are constructed from an ex stabilizer structure through a bracket 12 which is fas truded leading edge spar assembly covered wi...

Page 249: ...nboard and outboard ribs Figure 55 2 7 1 i r4 3 6 1 5 2 e 1 DETAIL A Al ELEVATOR FIGURE 55 2 The skins are attached to leading edge e drusion 5 55 20 01 ELEVATOR REMOVAL and n bs 6 with blind n vets E...

Page 250: ...e as the elevator with stretch formed skins 1 Ref Fig 55 spar extrusion 4 riveted to an extruded leading edge 2 and riveted together at the trailing edge The rudder lower skins 3 if are drop hammer fo...

Page 251: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION 1 4 1 1 10 i 8 1 z 1 c 9 7 r j 4 5 RUDDERASSEMBLY FIGURE55 4 55 40 02 OLDWILLWAYNE...

Page 252: ...CHAPTER VVIN DOVVS OLDWILLWAYNE...

Page 253: ...7 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 56 00 00 Gene al 3 56 00 01 Clean6g Acrylic 3 56 20 00 Windshield and Cabin Windows 3 56 21 00 Windshield 4 56 21 01 Windshield Removal 4 56 21...

Page 254: ...on door fr me Never use gasoline benezene carbon tetrachloride acetone lacquer thinner deicer All the windows are heated in an auto dave to fluid house hold cleaning fluid or any other approximately...

Page 255: ...break bond The new windshield being forced into cavity between outer skin 4 and inten or retainer 7 will extrude ex Carefully pull the windshield away from its location cess sealant After windshield i...

Page 256: ...ay be required to break Check replaced window for leaks bond between acryfic and outer skin Care should be Reinstali interior tn m panels exercised to keep window from twisting and possibly 5 23 00 ST...

Page 257: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION B LAN K 56 50 00 OLDWILLWAYNE...

Page 258: ...CHAPTE R MIINGS OLDWILLWAYNE...

Page 259: ...TENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 57 00 00 General 3 57 00 01 Wing Removal and Installation 3 57 00 02 Stall Stn p installation 4 57 10 00 Main Frame 4 57 20 00 Au a liary Strudures 5 57 20 0...

Page 260: ...he fuel is contained in wet wing type fuel cells between main spar and baffles forward of spar The F Attach A frame hoist to propeller or support with tanks are sealed dun ng manufacturing with curren...

Page 261: ...See heater wires if installed Section 28 for resealing procedures k Hardware shown in Figure 57 1 The wing is manufactured in three sections the center CAUTION section 2 the left outboard section 3 an...

Page 262: ...s are The M20K wing tips are non structural fiberglass not restn cted in movement either direction components They are riveted to the upper and lower wing skins during final assembly of the wing struc...

Page 263: ...PLY CONNECTORS 8 WILL VARY SMK57 4 FIBERGLASS WING TIP ASSEMBLY FIGURE 57 4 9 tttul rr 10 3mi I ILL 1 TVD OLt 12 19 O 4 I I I I I O O ts 19 17 Bc 9 BO ITM CEN ER SECTION 0 LODKING UP 13 7 O NOrEl 15 P...

Page 264: ...s 6 Wing skin 025 thickness 16 Auto pilot servos 7 Fuel tank access 17 Gym compass flux valve tone of these depending on installed equipment left wing only 8 Fuel tank filler 18 Main landing gerar ret...

Page 265: ...structure of flaps consists of a leading to this sub assembly To complete control surface edge extrusion 5 trailing edge stiffener 8 n bs O hinges 6 and balance weights O are installed The and top and...

Page 266: ...CHAPTER STANDARD PRACTICES PROP ROTOR OLDWILLWAYNE...

Page 267: ...R 60 STANDARD PRACTICES PROPELLER LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT 60 Effedivity Contents 1 2BLANK 9 97 60 00 00 3 9 97 60 00 00 4 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SE...

Page 268: ...cCauley 2 blade propeller installed Refer to Teledyne Continental Motors TCM An option forthe M20K S N 210001 thru 25 1999 is a maintenance publications for engine inspection Hartzell 2 blade propelle...

Page 269: ...SERVICE AND MAINTENANCE MANUAL M20K MOONC AIRCRAFT CORPORATION BLANK 60 00 00 OLDWILLWAYNE...

Page 270: ...eHAPTER PROPELLERS PROPU LSORS OLDWILLWAYNE...

Page 271: ...0 7 9 97 61 40 00 8 9 97 TABLE OF CONTENTS CHAPTER SUBJECT DATE SECTION SUBJECT 61 00 00 General 3 61 00 10 Spinner Dome and Propeller RemoMI 3 61 00 20 Propeller Installation 4 61 10 00 Propeller Ass...

Page 272: ...late 4 Reference Figure 61 1 twisting moments and spring force on propeller blades B Pull doubler plates from behind propeller decrease propeller blade pitch and increase RPM C Carefully pull spinner...

Page 273: ...er bulkheads 7 fits snug as spinner dome is being installed 61 00 20 PROPELLER INSTALLATION i If aft spinner bulkhead was removed re install 7 Conduct operational and leak check on propeller using bol...

Page 274: ...t of panel to increase the governor arm position friction or loosen the nut to decrease friction 6 Attach control rod end to governor arm and RetigMen lock nut on back side to secure cable to replace...

Page 275: ...varnish Check speeder spnng ends for proper settings Bent pilot valve Remove head and replace pilot valve Excessive internal leakage in Check ngglng and make necessary part govemor replacements Excess...

Page 276: ...smoother opera CAUTION tion The vendor system used should be an approved Place weights washers or whatever balance system and the procedures followed very carefully The weights are specified at the lo...

Page 277: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK 61 40 00 OLDWILLWAYNE...

Page 278: ...CHAPTER POVVERPLANT OLDWILLWAYNE...

Page 279: ...16 71 10 00 Engine Cooling 16 71 10 01 Engine Cooling Cleaning Inspei tion Repair 17 71 11 00 Cowling Removal 17 71 11 01 TopCowling 17 71 11 02 Bottom Cowling 17 71 12 00 Cowling Installation 17 71...

Page 280: ...71 Effedivity 1 2BLANK 9 97 71 Contents 3 4BLANK 9 97 71 00 00 5 97 71 00 40 6 997 71 00 50 7 997 71 00 50 8 997 71 00 50 9 497 71 00 50 10 997 71 00 50 il 9 97 71 00 50 12 997 71 00 50 3 497 71 00 50...

Page 281: ...ncreases Manifold Pressure from 36 In Hg Reverse the engine removal procedure for installation to 39 In Hg and reduces RPhi from 2700 RPM to 2600 RPM Sea level power can be maintained up to 20 000 i E...

Page 282: ...heck 030027 501 for binding B Miscellaneous hand tools Required for I Check baffles and cowling for security adjustment and to disconnect or conned frttings and hoses G Open cowl flaps check operation...

Page 283: ...manifold valve ffow divider manifold pressure port on calibrated gauge Connect fuel pressure hose between this port and fitting on right hand side of firewall Connect another D AII connedions should...

Page 284: ...e as follows cylinder head temperature is in the lower one q_uarter of GREEN are and oil temperature is 1600 to 180P F 1 Operate engine until oil temperature has reached a needle width past center of...

Page 285: ...M govemor head as required to obtain required RPM m udure control FULL RICH proceed as follows Recheck control for required cushion after setting RPM 2 Reduce engine speed to 2000 RPM with the K FLIGH...

Page 286: ...700 RPM Idle Speed 700 25 RPM FULL POWER PERFORMANCE MP SHIP ST RPM 0 25 F F SHIP F F TEST IbsJHr GROUND CRITICAL OAT PRESSURE ALT 29 92 Hg DENSITY ALT RPM FLIGHT CRITICAL OAT PRESSURE ALT 29 92 Hg F...

Page 287: ...NIP RPM C AI INST REMARKS ALTITUDE F F MP RPM SHIP INST Temperature variations from NASA Standard Day temperature causes approximately 7 Ibs per hour fuel now change with each 1 degree C variation mi...

Page 288: ...t Rsachsd s i Pqlmt atoDanyA d 1150 ntlr Bla p IS WR WLthlnB d 1 RP H dSt tic 2250 Dendty A toQ 11 1I 050 n Rslult 11 WIlMn B d i iiii I ii t 1 14 Fl 1 i Irr i i 1 I rr i i I LILLLI IY ii nl W1 tipr r...

Page 289: ...m sye Iri i IC ec o z r B lt nm I Fj n Bi P m m 5 r 7 f3 1 2 DECK REF PORT g FUEL MANIFOLD VALVE TEST FTTflJG OI I AF 910E m 4 IDLE 80880 AD3082MENT 8CREW 6 IDLE FUEL PRESSURE ADJUSTMENT c w INCREASE...

Page 290: ...pq o o 24000 8 22000 20000 18000 t c O w w 16000 Y Y X r I r X Y P 14000 6PL 8 12000 P I I V y y y My vr I I P ioooo soool l l I y y y y y I I p 6000 r n 4000 4 2000 O 50 40 30 20 10 1 0 20 32 4 0 SO...

Page 291: ...decreases below 38 Hg at full throttle Enter point on chart at Pressure Altitude and OAT If point is within the depicted altitude band critical altitude is within tolerance If outside the altitude ba...

Page 292: ...e manifold pressure should stabilize Do not operate starter in excess of 30 seconds g tfk0e l 42 0 and 44 0 In Hg there should be no loss allow cooling time before re engaging of power and the fuel fl...

Page 293: ...3 01 COWL FLAP RIGGING 3 Unlatch 2 cam locks located on bottom cowling 25 0001 thru 25 0999 between cowl flaps S N 250001 thru 25 0999 i Adjust both the left and right cowl flaps so that in the 4 Unla...

Page 294: ...om bar on display nose gear box Readjust as required 5 Repeat steps 2 through 4 until no further 71 15 00 COWL FLAP POSITION INDICATOR adjusment is required 25 1000 thru 25 1999 6 Cycle cowl flap syst...

Page 295: ...s and grommets if removed and replaced induction air through the filter and turbocharger for any reason should be sealed after routing the cable or housing then to the engine wire assembly from the en...

Page 296: ...ch is mounted on the cable knob and the panel in the cabin atthis position altemate air box and should be n gged to extinguish the 3 An electn cal switch on the cockpit control light with bottom of do...

Page 297: ...CHAPTER ENGINES OLDWILLWAYNE...

Page 298: ...ATION CHAPTER 72 ENGINE LIST OF EFFECTIVE PAGES CHAPTER PAGE DATE SECTION SUBJECT 72 Effedivity Contents 1 2BLANK 9 97 72 00 00 3 9 97 72 00 00 4 897 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUB...

Page 299: ...NERAL MB Manual No X30671 SB and Ovemaul and Maintenance Manual No s X30030A GB LB MB or Refer to Teledyne Continental Motors CTCM X30672A SB for detailed information Maintenance and Operators Manual...

Page 300: ...SERVICE AND MAINTENANCE MANUAL M20K MOONC AIRCRAFT CORPORATION BLANK 72 00 00 OLDWILLWAYNE...

Page 301: ...CHAPTER ENGINE FUEL AND CONTROL OLDWILLWAYNE...

Page 302: ...OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 73 00 00 General 3 73 30 00 Indicating 3 73 31 00 Fuel Flow System General System bescription 3 73 31 01 Panel Mounted Instrument 3 73 31 02 Fuel Flow...

Page 303: ...pdates the totafu ed fuel quantity in a Installed per SI M20 49 random access memory chip The Total Fuel Used quantity is retained dun ng aircraft shut down by 73 31 00 FUEL FLOW SYSTEM GENERAL connec...

Page 304: ...ARRANGEMENT FIGURE 73 2 configuration selection block located inside the TRU FLOW 1 indicator has several arrangements to change 2 f T1O1A HOSKINS System data readout a desired Jumpers should not be A...

Page 305: ...rear of in H K3 HH K1 dicator which also removes connector latch and 2 on side of indicator Then remove electronic assembly by Arrange the jumpers according to Figure 73 3 A simultaneously pushing on...

Page 306: ...ment transducers new transducer should have the same K factor as the units being B Connect the nuts of lines 4 and 5 to fRtings replaced Specify K factor code when ordering 8 leave them snug not tight...

Page 307: ...or airframe ground If OK change indicator A SINGLE FLIGHT TOTALIZER The aircraft B Displays zeros with engine running should be topped with fuel before each Right so the 1 Remove cowling for access to...

Page 308: ...t isolate the Alcor Inc 10130 Jones Maftsberger Road PO Box problem or do not find a problem contact the Customer 32516 San Antonio Tx 78284 telephone 830 Service Department of Mooney Aircraft Company...

Page 309: ...CHAPTER IGNITION OLDWILLWAYNE...

Page 310: ...ATE SECTION SUBJECT 74 Effedivity Contents 1 2BLANK 997 74 00 00 3 997 74 30 00 4 997 TABLE OF CONTENTS CHAPTER SU IECT PAGE SECTION SUBJECT 74 00 00 General 3 74 1 0 00 Electrical Power 3 74 10 01 Ig...

Page 311: ...Hard starting A Assure that the impulse couplings are operating B Check magneto timing to engine LOWER SPARK PLUGS 2 Engine roughness A Install new spark plugs IWN FIROt mOrn 1 633 5 1 f Q1IC1 B Check...

Page 312: ...SERVICE AND MAINTENANCE MANUAL M20K MOONCI AIRCRAFT CORPORATION BLANK 74 30 00 OLDWILLWAYNE...

Page 313: ...CHAPTE R ENGINE CONTRO LS OLDWILLWAYNE...

Page 314: ...ONTROLS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE ISEFWCONTENTS 1 2BLANK 9 97 76 00 00 3 9 97 76 1 0 00 4 9 97 TABLE OF CONTENTS CHAPTER SECTION SUBJECT SUBJECT PAGE 76 00 00 Engine Co...

Page 315: ...ONEY AIRCRAFT CORPORATION M20K SERVICE AND MAINTENANCE MANUAL 7640 00 ENGINE CONTROLS 76 10 00 ENGINE CONTROLS RIGGING See Section 71 00 52 for Engine Controls Rigging Adjustments 76 00 00 OLDWILLWAYN...

Page 316: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK 76 10 00 OLDWILLWAYNE...

Page 317: ...CHAPTER ENGINE INDICATING OLDWILLWAYNE...

Page 318: ...97 77 1 0 02 4 9 97 77 20 02 5 9 97 77 20 02 6 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 77 00 00 General 3 77 00 01 Ranges 3 77 1 0 00 Power Indicating 3 77 1 0 01 Tachometer 3 77...

Page 319: ...rt develops in the tachometer A Green are 30 to 80 PSI GB 8 LB engines 25 1000 thru SS TBA Green are 30 to 60 PSI MB 8 SB engine 8 Yellow arc l0 to 30 PSI The tachometer indicating system is a fully s...

Page 320: ...25 2012 may be retrofitted to SB configuration if desired by owner MANIFOLD PRESSURE TROUBLE SHOOTING TROUBLE PROBABLE CAUSE REMEDY Excessive error at e cisting Pointer shifted Replace instrument baro...

Page 321: ...for 251000 thru 25TBA An optional system The cylinder head temperature CHT instrument provides a probe in each cylinder to provide moniton ng provides the operator with an indication of how hot or or...

Page 322: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK 77 20 02 OLDWILLWAYNE...

Page 323: ...CHAPTER EXHAUST OLDWILLWAYNE...

Page 324: ...R SECTION SUBJECT PAGE DATE 78 EFF CONTENTS 1 2BLANK 897 78 00 00 3 9 97 7840 00 4 997 TABLE OF CONTENTS CHAPTER SECTION SUBJECT SUBJECT PAGE 78 00 00 General 3 78 10 00 Exhaust System Installation 3...

Page 325: ...To properly inspect exhaust system components must Install only correct parts be clean and free of oil grease etc Clean as follows DO NOT FORCE FIT any component A Spray engine exhaust system componen...

Page 326: ...SERVICE AND MAINTENANCE MANUAL M20K MOONC AIRCRAFT CORPORAIION BLAN K 78 40 00 OLDWILLWAYNE...

Page 327: ...CHAPTER OIL OLDWILLWAYNE...

Page 328: ...79 30 02 5 997 79 30 02 6 997 79 30 02 7 997 79 30 02 8 997 79 40 00 9 997 79 40 00 10 997 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 79 00 00 General 3 79 00 01 Oil Filter RemoMI 3 79 00...

Page 329: ...y overhauled 4 Perform leak check prior to flight engine hould have the oil and filter changed at 50 hours of operation after changing to 5 Reinstall lower and upper cowling see Sedion detergent oil t...

Page 330: ...MPERATURE 79 30 01 OIL PRESSURE The oil temperature gauge is an electric unit receiving its signal from a temperature bulb in the engine case Oil pressure indicating is provided through a pressure loc...

Page 331: ...SERVICE AND MAINTENANCE MANUAL j RBOCHARGER tlRBO OtL P I ort PRESSUR TRANSD WD I 1 s i URBOCf 1ARGER Oft SCAVENGE LINE FllE W t00iCIEIGUP AT TURBOCHARGER O L LUBRICATION SYSTEM FIGURE 79 3 25 0001 th...

Page 332: ...L M20K MOONEY AIRCRAFT CORPORATION 1PF O1L SEPARATOR fFW TURB O OIL SCAVENGE DRY Al VACUUM PUMP Oit PRESSURE TRANSDUSER rr Ifs i DOWN At REAR L TURBOCHARGER OIL RETURN SYSTEM FIGURE 79 4 25 0001 thru...

Page 333: ...L LINE FRO H 7URBOCHARGER o TO SCAVENGE PUMP OsL LINE FROM ic2 GALLERV E TO TURBOCHAROER a I 1 8 c o p o B d E mn lo fi5 B 2 c O 2 Z t r o g c I iri E 3m I 3 F I I i I g VIEW LOOKING UP z 8 OLDWILLWAY...

Page 334: ...ON VIEW LOOKINC D0WN OH r OIL TRANSDUCER UPPER LEFT ENGINE HDUHT FWD ENGINE IUOUNf E f I VIEW LOOKING UP UNDER CENTER C Y L I no E R 9 4 LEFT SIDE ENGINE FURBOCHARCER LINE TURBOCHARGER O1L LUBRICATION...

Page 335: ...If pressure reading is incorrect go to step connected to the aircraff harness in the engine compartment by disconnecting the appropriate Druck transducer electrical connector and connecting the test...

Page 336: ...SERVICE AND MAINTENANCE MANUAL M20K MOONCI AIRCRAFT CORPOWATION BLANK i 79 40 00 10 OLDWILLWAYNE...

Page 337: ...CHAPTER STARTING OLDWILLWAYNE...

Page 338: ...Effedivity Contents 1 2BLANK 9 97 80 00 00 3 997 8 1 0 00 4 897 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 80 00 00 General 3 80 00 01 StarterTroubl hdoting 3 80 00 02 Starter Maintenance...

Page 339: ...ommutator The brushes 1 Inspect and service starter per TCM Service In should be replaced when they have worn to 1 4 inch in structions or Overhaul Manual length Brush tension should be 32 to 40 ounce...

Page 340: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK i I ao om OLDWILLWAYNE...

Page 341: ...CHAPTER TURBINES OLDWILLWAYNE...

Page 342: ...97 81 20 00 5 997 81 20 00 6 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 81 00 00 General 3 81 10 10 Turt ochadercon rol system Rotomastkr 3 81 10 11 Test Procedures 3 81 10 20 Turt oc...

Page 343: ...hes Hg if operating properly If manifold pressure It is mandatory that the waste gate be properly exceeds 38 0 inches Hg dun ng this check the adjusted prior to aircraft operation See Section overboos...

Page 344: ...r 3 I I IUABI E Ll n ll cRovao I ILPIPE WISTLCITEY LVE TURB OCHARGER SYSTEM 25 0001 25 0999 FIGURE 81 1 IHTt tCObLElt OVL BDOSI IIFE1 VILYE COYILt O l u wD 9 I e uuw ucl rmwrr GU YIII IILL IIbOLVIL c...

Page 345: ...or overhaul or repair Leak in engine intake of Tighten loose connections or replace exhaust manifold manifold gaskets as necessary Rotating assembly bean ng Remove turbocharger and retum to seizure ap...

Page 346: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION BLANK 81 20 00 OLDWILLWAYNE...

Page 347: ...CHAPTE R OLDWILLWAYNE...

Page 348: ...7 thru 89 9 97 91 30 00 90 9 97 TABLE OF CONTENTS CHAPTER SUBJECT PAGE SECTION SUBJECT 91 00 00 General 3 91 00 01 Electrical System Notes 3 91 00 02 Wiring Identification System 4 91 00 03 Abbreviati...

Page 349: ...nals must be preinsulated or must be insulated with Ampsulation or equivalent 6 Wires without dash numbers are furnished by the manufacturer and are included with the equipment 7 The symbol indicates...

Page 350: ...D PC Dump CF Wing Flaps Electn e CT Trim CV Stand by Vacuum DA Instruments Ammeter DB Instruments Tum Coordinator DC Instruments Cylinder Head Temperature DD Instruments Outside Air Temperature DE Ins...

Page 351: ...Pressure WL Waming System Landing Light WM Warning System Gear Position Waming Manual WN Warning System Pressurization WS Warning System Stall Warning WT Waming System Press to Test WV Warning System...

Page 352: ...FA ALT EMER FRENCH I H FUSE HOLDERS FN PHONES FU FUSES NV ALT EMER FIELD FRENCH GD GROUND HS HORIZNTAL SITUATION INDICATORO JE IGNITION ELECTONIC JM IGNITION MAGNETO JV IGNITION VIKBRATOR LA LIGHT BUL...

Page 353: ...WM WARNING MASTER WN WARNING PRESSURIZATION WP WARNING PITOT HEAT WS WARNING STALL WT WARNING ANNUNCITOR WV WARNING VACUUM WW WARNING ALTERNATE AIR 9140 03 ABBREVIATIONS EQUIPMENT LIST The abbreviatio...

Page 354: ...0238 thru 25 0246 800330 F1 25 0001 25 0247 thru 25 0298 800330 F2 25 0299 thru 25 0446 800330 F3 25 0447 thru 25 0612 800330 F4 25 0613 thru 25 0780 800330 F5 250781 thru 25 0841 800330 F6 25 0842 t...

Page 355: ...UATOR MICRO JV 5 21 CF08A SWITCH LIMIT UP MICRO V3 1 ACTUATOR MICRO JV 5 21 CFOSA SWITCH CONTROL MICRO 2TL75 10 21 CFOSB SWITCH CONTROL FLAP CUTLER HAMMER 8906K3149 21 CTO1A C B ELECTRIC TRIM MOONEY 9...

Page 356: ...MOONN 880004 501 21 DD04A C B OAT EGT KUXON 7277 2 2 21 DEO1A GAUGE CARE AIR TEMP MOONEY 660014 005 GARWIN 22 99504 21 DE02A PLUG GAUGE MS3106A 1 4S1 S CLAMP MS3057 6B 21 DE02B PLUG GAUGE MS31 06 14S...

Page 357: ...QTY RH MOONCI 640281 151 AMMRER MOONEY 640281 137 OIL PRESS MOONE 640281 141 OIL TEMP MOONEY 640281 1 39 OIL TEMP ALT MOONN 640281 159 34 CM HEAD TEMP MOONEY 640281 143 CYL HEAD TEMP ALT MOONE 610281...

Page 358: ...MP GAUGE BENDIX mDGA i 0 98S SFi 21 DKOBB PLUG FF BENDD m06A 1515S SFP 21 DK03C D PLUG FF TTT CANNON DE SS 21 DK03UF PLUG FF tom CANNON DE SS 21 DK04A C B FF KLIXON 7277 2 2 21 DKOSA SWITCH MEMORY FF...

Page 359: ...ELEC ITT LAiiC21101 21 EG04B ACTUATOR GEAR ELEC DUKES 1057 0 1 21 EGO4C ACUTATOR GEAR ELEC DUKES 4196 00 1D 21 EG04D ACUTATOR GEAR ELEC ITT LAliC2115 21 EG04E ACUTATOR GEAR ELEC TTT LAI 1 C2114 21 EG...

Page 360: ...79020 18 21 JMO2D MAGNETO LEFT SLICK 6214 21 JM02E MAGNETO LEFT SLICK 6224 21 JM03A MAGNETO RIGHT BENDIX S4LN204 21 JM03C MAGNETO RIGHT BENDIX i 0 79020 18 21 JM03D MAGNETO RIGHT SLICK 6214 21 JM03E...

Page 361: ...930 9 LAMP GE 1816 21 LLO1A C B LDG LT MWDEN AHW4 20 21 LLO1B C B U3G LT MOONN 930023 15 21 UOIC D C B LDG LT MOONN 930023 115 215 28 21 U02A RELAY LDG LT MAGNECRAFT VlS9CQX 2 21 LL03A LIGHT LDG GE 45...

Page 362: ...GE 1836R HOLDER 7 EA H H SMITH 1930 9 21 LP 8A LAMPS O MITE GE 1836 HOLDER 4 EA H H SMITH 1930 9 21 LP1 88 LAMPS GE 1816 HOLDER 10 EA H H SMITH 1930 9 21 U 1 8C LAMPS GE 1816 HOLDER 9 EA H H SMITH 19...

Page 363: ...L EL 155020 or 155120 21 LP44A CONNECTOR PLUG AMP 206060 1 CLAMP AMP 206062 1 21 LP45A CONNECTOR AMP 2061 53 1 CLAMP AMP 206062 1 21 LRO1A C B RECOGNITION LIGHTS MOONEY 930023 231 21 LR02A RECOGNITIO...

Page 364: ...PT TAIL STROBE P S AMP 1 4803050 PINS 3 EA AMP 61118 1 OR 606291 21 MAO1A AUX PV R RECEPTACLE AN2552 3A 21 MA02A RELAY AUX PV R CUTLER HAMMER 6041H105A 21 MA02B RU4Y CUTLER HAMMER 6041Hi05A 21 MA03A D...

Page 365: ...0 21 MB30A BUSS GRD 2 MOONEY 800233 000 21 MB31A BUSS GRD 3 MOONEY 800233 000 21 MB32A B C B WXRADAR COLOR MOONCI 930023 125 225 28 21 MB33A C B RADIO BLOVMR KUXON 7277 2 ii 21 MB34A RADIO BLOWER ASSY...

Page 366: ...FILTER SPRAGUE JN i4 1356A 21 PA03C FILTER CAPTOR A2637 21 PA03D FILTER CAPTOR A2638 21 PA04A C B ALT MECHANICAL PRODUCTS 1648 001 70 21 PA04B C B ALT OUTPUT ETA 41 3S14 LN2 70 21 PA05A CAPACITOR SAN...

Page 367: ...MAIN i MOONN 913127 017 21 PB1OC BUSS BAR MAIN 1 MOONEY 913127 019 21 PB11A BUSS BAR MAIN 2 MOONEY 913127 005 21 PB11B BUSS BAR MAIN 2 MOONEY 913127 019 21 PB12A BUSS BAR MAIN 3 MOONE 913127 005 21 PB...

Page 368: ...B SOCKET 50 1 0498309 21 PG07A REI4Y CONTROL MAGNACRAFT V 7CSX 2 SOCKET 70 303 21 PG08A LIGHT ON WESTERN IND 501 61 K i 1 K3BP LAMP WI 7046 21 PGOSA LIGHT O V STERN IND 501 61 K iiK3BP LAMP V n 7046 2...

Page 369: ...P 206037 1 CLAMP AMP 206070 1 21 PL1 38 PLUG ACCESS PNL AMP 2067081 CLAMP AMP 2069681 21 PL14A PLUG V SIDE CABIN AMP 206037 1 CLAMP AMP 206070 1 21 PL14B PLUG V SIDE PANEL MOONEY 930021 001 21 PL1SA P...

Page 370: ...TS TRIM AMP 20606Q i CLAMP AMP 206062 1 21 PL29A PLUG TAIL AMP 206060 1 CLAMP AMP 206062 1 21 PL29B PLUG EMPENNAGE AMP 206708 1 CLAMP AMP 20696 1 21 PL30A PLUG RADIO C B PNL AMP 206037 1 CLAMP AMP 206...

Page 371: ...39 1 CLAMP AMP 206070 1 21 PL48A PLUG FLT PNL DIM AMP 206037 1 CLAMP AMP 206070 1 21 PL49A PLUG C B GRND AMP 205838 1 C14MP AMP 206062 1 21 PLSOA PLUG CIB DIM AMP 206062 1 CLAMP AMP 206062 1 21 PL51A...

Page 372: ...P 21 PL72A PLUG VOWGS TRANSFER AMP 2058381 206062 1 CLAMP 21 PL73A PLUG MKR INVERTER AMP 205838 1 206062 1 CLAMP 21 PL74A PLUG NAVIREC AIP AMP 2058343 206070 1 CLAMP 21 PL75A PLUG ADWRMI 206037 1 2060...

Page 373: ...206070 1 21 RCO7A RECPT CONSOLE 1 AMP 206036 3 CLAMP AMP 206070 1 21 RCO7B RECPT CONSOLE 1 AMP 206153 1 CLAMP AMP 206062 1 21 RC08A RECPT HEADLINER AMP 206036 3 19 CU WIP AMP 206070 1 21 RC08B RECPT...

Page 374: ...CONE AMP 206036 3 CLAMP AMP 206070 1 21 RC24B RECPT CABIN TAILCONE AMP 206705 2 CLAMP AMP 206966 1 21 RC24C RECPT CABIN TAILCONE AMP 206036 3 CLAMP AMP 206070 1 21 RC25A RECPI WWING AMP 206036 3 CLAMP...

Page 375: ...P 206153 1 CLAMP AMP 206062 1 21 RC38A RECPT U T SW AMP 206153 1 CLAMP AMP 206062 1 21 RC39A RECPT O H Ll jiHT AFT AMP 206153 1 CLAMP AMP 206062 1 21 RC40A RECPT EMERG flD AMP 2061 53 1 CLAMP AMP 2060...

Page 376: ...RC59B A P DIM 206153 1 CLAMP AMP 206062 1 21 RCGOA RECPT K4IG2 NAMIECIAIP 2061 52 1 CLAMP AMP 206070 21 RCG1A RECPT K 14 NAVRECIAIP 2061 52 1 CLAMP AMP 206070 1 21 RC62A RECPT K 14 NAVRECIAIP 2060363...

Page 377: ...URATOR MICF O JV 5 21 V JE04A HORN GEAR UP WARN MALLORY SC628P 21 1 05A RECTIFIER SARKES TARZIAN F 4 21 06A LIGHT GEAR POSITION SLOAN 855SO U BULB 1 GE 327 21 LIGHT GEAR DOV R KORRY 250 650 5821 007 B...

Page 378: ...LIXON 7277 2 2 21 VW02A SWITCH VACUUM WARN MCONEY 880012 501 21 21 WV02B SWITCH VAC W4RN LO V MITMAN GENERAL P118V IN K5L 21 21 VW02C SWITCH VAC V IARN HI V MITMAN GENERAL P118V IN K4L 2 21 21 VW03A L...

Page 379: ...R414 20082 with 880016 501 8 800331 721 cable 14 Manufacture using Alpha Wire Co braid 2172 or 1233 2 2 ea 8 AMP terminals as necessary to connect the buss bars as shown on schematic Cover braid with...

Page 380: ...LS02B 21 LS03B 21 LS04B 8 21 LS05B 32 Effective 250447 thru 25 0780 or 24 1038 thru 24 1425 33 Standard on 24 1211 8 ON 34 Effective 25 0613 thru 25 0780 35 Alternate Turn Coordinator w lights United...

Page 381: ...PIN AMP 2061 53 1 CLAMP AMP 206062 1 JK CC1 07A PLUG 4 PIN AMP 206060 1 CLAMP AMP 206062 1 JKL CF1O1A C B FLAP ACT KLD ON 7277 2 5 JKL CF102A SWITCH FLAP C H 8906K3149 JKL CF103A SWITCH UP LIMIT MICR...

Page 382: ...OIA LOADMETER SINGLE B D 0326004 JK DA1O1B LOADMETER DUAL B D 0328003 J DA1O1D AMMETER MOONEY 640281 509 LIGHT BULB ASSY ROCHESTER 0105S00004 BULB GE 313 JK DA1 02A CONN AMMETER S E C PWDGB12 1 OS JK...

Page 383: ...SHUNT McGRAW EDISON FHN42A FUSE 5A McGRAV EDISON FM01 5A L DA163A FUSEHOLDER LT ALT SHUNT McGRAW EDISON FHN42A FUSE 5A McGRAW EDISON FMO1 SA L DA164A FUSEHOLDER RTLOAD SHUNT McGRAW EDISON FHN42A FUSE...

Page 384: ...M02A TRANSMITTER FUEL QTY O B L T MOONEY 610243 003 JKL DF104A TRANSMITTER FUEL QTY O B RT MOONEY 610243 001 KL DFIOSA TRANSMITTER FUEL QTY I B LT MOONEY 610242 003 KL DF1OGA TRANSMITTER FUEL QTY I B...

Page 385: ...PIN AMP 2061 53 1 CLAMP AMP 206062 1 J DK1O1A XDUCR FUEL PRESS MOONEY 880045 501 J DK102A PLUG FUEL PRESS XDUCR MS3106A10SL 3S L DK1SOA CIB FUELIOIL PRESSURE KilXdN 7277 2 1 L DK1S1A INDICATOR FUEUOIL...

Page 386: ...01 J DM O1A HOUR METER MOONEY 880035 507 K DM 02A HOUR METER MOONEY 880035505 L DMISOA HOUR METER AIRPAX K4205 K4207 or KF4207 ALT L DM1S1A RECPT HOUR METER 4 PIN AMP 206153 1 CLAMP AMP 206062 1 L DM1...

Page 387: ...01 PROBE EGT CYL 5 ALT MOONEY 880005 503 K DT1OGA PROBE EGT CYL 6 MOONEY 880005 501 PROBE EGT CYL 6 ALT MOONEY 880005 503 JK DV1OIA C B FUEL FLOW KLIXON 7277 2 2 JK DV102A INDICATOR FUEL FLOW MOONEY 8...

Page 388: ...IGNITION BOX LT PORSCHE 933 602 007 07 L JE153B IGNITION BOX RT PORSCHE 933 602 007 07 L JE 54B PLUG IGN BOX LT CANNON CA3106A 20A 48S B O3 L JE154B PLUG IGN BOX LT ALT CANNON GERMANY CA3106A 20A 48S...

Page 389: ...000 ADAPTER ALT SUNBANK S2900ASi 004AI S034 000 COUPLING SUNBANK S3292 BOOT RAYCHEM 202S1 21 25S L JE171C PLUG 3PIN CANNON GERMANY CAOGEHiOSLSPB14 PLUG 3 PIN ALT PORSCHE 933 612 412 00 ADAPTER RACHEM...

Page 390: ...A 10 682555 1 J JMI02B MAGNETO ALT BENDIXSCINTILLA 10 682555 111 K JMi 03A MAGNETO RIGHT BENDIX SCINTILLA 10 79020 120 TCM 6408961 K JM103B MAGNETO RiGHT SLICK 6224 K JMI 04A MAGNENTO LEFT BENDIXSCINT...

Page 391: ...T GE 4596 K LL1OSA SWITCH LDG LT C H 8143 K21 E13 M50 L LL1SOA C B LANDING LIGHT LEFT KLIXON 7277 2 20 C B LDG LT LEFT ALT MECHANICAL PROD 4200 002 25 L LL151A C B LANDING LIGHT RIGHT KLIXON 7271 2 20...

Page 392: ...LIGHT TRAY VERTICAL SPEED U I BA28 BW3 JK LP122A LIGHT TRAY ARTIFICIAL HORIZON SIGMA TEC IV 192 971 JK LP123A LIGHTTRAY DIRECTIONALGYRO SIGMA TEC IV 192 971 K LP125A LIGHT TRAY TIT B D 0221 128 JK LP1...

Page 393: ...STROBE PWR SUPPLY RT WG WHELEN 01 0770329 00 JKL LS108A RECPT STROBE PWR SUPPLY RT AMP 1 4803050 JKL LS1OSA RECPT STROBE LIGHT P S RT AMP 1 4803050 JKL LS11OA PLUG STROBE LIGHT RT AMP i 480303 0 JKL L...

Page 394: ...XOIARIES JKL MB127A C BINVERTER KLIXON 7277 2 XXOIARIES JKL MB128A C B STEREO KLIXON 7277 2 XXOIARIES JKL MB129A C1B PROP DE ICE MOONEY 930023 223 JKL MB 31A BUS BAR 10 MOONEY 913127 019 JKL MB132A BU...

Page 395: ...MP1 02A SHUNT B F GOODRICH MS91 586 1 JK MP103A FUSEHOLDER LITTEL 155020 or i 55120 FUSE 1A LITTEL 313001 JK MP 04A FUSEHOLDER LITTtEL i 55020 or 155120 FUSE 1A LITTEL 313001 JK MP1 05A AMMETER B F GO...

Page 396: ...AMP 206153 1 CLAMP AMP 206062 1 L NF1GOA FUEL PUMP MAIN PORSCHE 933 620 001 00 L NF1G1A FUEL PUMP EMERGENCY PORSCHE 933 620 001 00 K NP1O1A FUSEHOLDER PRIMER LITTEL i 55020 or 155120 FUSE 1 OA SLO BL...

Page 397: ...PA1 23A DIODE SARKES TARZLAN 10H3P JK PA1 24A SWITCH ALiERNAT R FIELD C H 880052 503 JK PA1 25A DIODE SARKES TARZIAN 10H3P JK PA1 26A DIODE SARKES TARZV N 1 0H3P L PA1S0A ALTERNATOR LT PORSCHE 933 603...

Page 398: ...R 9 MOONEY 913127 043 JK PB11GA SHUNT KULKA 600RJ 2 L PB150A BATTERY Rli Hj GILL E243 L PB1S1A RELAY BATTERY Ri C H 6041H202 ALT C H 6041 H202A L PB152A DIODE BATTERY RELAY RT 1N2483 L PB153A SWITCH B...

Page 399: ...lNE BUS RT C H 6041H202 ALT C H 6041 H202A L PB189A DIODE 1N2483 L PB1SOA MASTER SWITCH OPT C H 8133K 21 E13 T52 L PB1S1A GRND DIMMER BOX MOONEY 80022 501 JKL PLO1A PLUG C B PANEL 1 37 PIN AMP 206150...

Page 400: ...2 j6 P IN AMP 206037 1 CLAMP AMP 206070 1 JK PL25A PLUG LIGHT CONTROL 9 PIN AMP 20670 1 CLAMP AMP i06966 1 JK PL26A PLUG G SHIELDHARNESS 4PIN AMP 206060 1 CLAMP AMP 206062 1 JK PL27A PLUG FLT PNL 2 16...

Page 401: ...1A C B IGNTTACH CIG LIGHTER KLD ON 7277 2 10 JKL PS102A SOLENOID STARTER LT C H 6041H 202 or 202A JK PS 03A FUSEHOLDER LITTEL 155020 or i 55120 FUSE iA LITTEL 313001 J PS1OSA STARTER PRESTOLITE MHB 40...

Page 402: ...06153 1 CLAMP AMP 206062 1 JK RC14A RECPT HOUK METER 4 PIN AMP 206153 1 CLAMP AMP 206062 1 JKL RC15A RECPT LEFT WING STUB 14 PIN MOONC 930021 002 JKL RC1GA RECPT GEAR CONTROL AMP 2067052 CLAMP AMP 206...

Page 403: ...206153 1 CLAMP AMP 206062 1 JKL RCSOA RECPT C B PNL kc2 AMP 206151 2 CLAMP AMP 20613 1 JKL RCS1A RECPT IGNITION SV jITCI I MOONEY 930021 506 JKL RC52A RECPT ALT STARTER CANNON MS3100K28 2P ALT MS3100...

Page 404: ...0 WD150A FUSE 1AMP LITTEL 313001 JKL WE1O1A C B GEAR WARN HORN KLIXON 7277 2 2 JKL WE102A LIGHT GEAR DOWN SLOAN 855S 0 U BULB GE 327 JK WE103A SWITCH THROTTLE MICRO V3 1 ACTUATOR MICRO JV 1 JK WE104A...

Page 405: ...P DB5i 212 1 LOCK RETAINER ITT DB51221 1 JK WV O1A C B VACUUM WARNING KLIXON 7277 2 2 JK WV102A SWITCH VACUUM WARNING MOONEY 880012 501 JK WV103A RECPT VAC WARN 4 PIN AMP 206153 1 CLAMP AMP 206062 1 J...

Page 406: ...SERVICE AND MAINTINANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION 28 VOLT S N 25 1000 THRU 25 1224 RESERVED 91 20 02 60 OLDWILLWAYNE...

Page 407: ...E 5 JK CC1OGA PLUG 9 PIN AMP 206708 1 CLAMP AMP 206966 1 JK CC107A RECEPTACLE 9 PIN AMP 206705 2 CLAMP AMP 206966 1 JK CC1 08A VARISTOR GE V47ZA05 JK CF1O A C B FLAP ACTUATOR KLIXON 7277 2 5 JK CFI03A...

Page 408: ...ULE INSTR MOONEY 880059 507 JK DG104A PLUG 28 PIN AMP 2058383 CLAMP AMP 206070 1 K DG105A MODULE INSTRUMENT MOONC 880059509 J DH1O1A PROBE OIL TEMP MOONEY 880061 501 ALT LEWIS ENGRG 56B3A9 K DH1OIA PR...

Page 409: ...20583 1 CLAMP AMP 206062 1 K DR1 038 PLUG 28 PIN AMP 205839503 CLAMP AMP 206070 1 K DR1 04A PROBE TIT MOONEY 880055501 JK DT1OIA PROBE EGT CYL i MOONEY 880005 503 ALT MOONEY 880005501 J DT1O1A ALT MO...

Page 410: ...RECEPTACLE 4 PIN AMP 206153 1 CLAMP AMP 206062 1 JK DV107A SWITCH FUEL FLOW C K 7101K JK DV108A PLUG 4 PIN AMP 206060 1 CLAMP AMP 206062 1 JK DVi 09A RECEPTACLE 4 PIN AMP 206153 1 CLAMP AMP 206062 1...

Page 411: ...AFT S 1028 WASHERS ALT SWTTCHCRAFT S 1029 JK JM1OIA SWITCH MAGNETO BENDIX SCINTILLA 10 357210 9 PLACARD BENDIXISCINTILLA 10 1 87 468 J JM102A MAGNETO BU DIXISCINTILLA P4LN2021 K JM1 02A MAGNETO LEFT S...

Page 412: ...P AMP 206062 1 JK LC 22A RECEPTACLE 4 PIN AMP 206153 1 CLAMP AMP 206062 1 JK LC123A SWITCH CABIN DOOR NEWARK 89F5544 JK LC124A RECEPTACLE 2 PIN AMP 1 4803190 PIN AMP 60620 1 JK LC125A PLUG 2 PIN AMP 1...

Page 413: ...327 AVIATION RED JK LP112A LAMPS GUS HLL LIGHTS 14a GE 327 JK LP113A LIGHT OXYGEN SLOAN 855S 0 U 6 LAMP 28V GE 327 JK LP114A LIGHT OXYGEN SLOAN 855S 0 U 6 LAMP 28V GE 327 JK LP11SA PLUG 2 PIN AMP 1 4...

Page 414: ...20 1 JK LR111A PLUG 2 PIN AMP 1 480318 0 SOCKET AMP 6061 81 JK LS1OIA C B STROBE LIGHT MOONEY 930023 237 JK LS102A POWER SUPPLY LT WING WHELEN 01 0770329 00 JK LS103A RECEPTACLE POWER SUPPLY AMP 1 480...

Page 415: ...AVIONICS BUS BAR 2 MOONEY 913127 67 JK MB1OGA AVIONICS BUS BAR 3 MOONEY 913127 87 JK MB1 07A C B INTERCOM KLIXON 7277 2 7 5 7 JK MB1 08A C B COM 1 KLIXON 7277 2 10 7 JK MB1 09A C B NAV 1 KLIXON 7277 2...

Page 416: ...1 JK NF104A RECEPTACLE 4 PIN AMP 206153 1 CLAMP AMP 206062 1 K NF1OSA C B HI BOOST PUMP MOONEY 930023 219 K NFI07A C B LO BOOST PUMP MOONEY 930023 217 K NF108A REGULATOR FUEL PUMP ELECTRO DELTA VR 53...

Page 417: ...RRENT MICRO CSLAI GE ELEMENT SENSOR MICRO SS 371 26 K PA11SA SENSOR CURRENT MICRO CSLA1GE ELEMENT SENSOR MICRO SS 371 26 JK PA120A PLUG 9 PIN AMP 206705 2 CLAMP AMP 206966 1 JK PA121A RECEPTACLE 9 PIN...

Page 418: ...P 206966 1 JK PL211A PLUG 34 PIN MOONEY 930021 507 JK PL212A PLUG 14 PIN MOONEY 930021 001 JK PL216A PLUG 16 PIN AMP 206037 1 CLAMP AMP 206070 1 JK PL217A PLUG 16 PIN AMP 206037 1 CLAMP AMP 206070 1 J...

Page 419: ...04A JK RB104A PLUG 2 PIN MOLM 03 06 1023 SOCKET MOLD 02 06 1 i 03 JK RC201A RECEPTACLE 37 PIN AMP 206151 2 JK RC203A RECEPTACLE 3 PIN AMP 206036 2 CLAMP AMP 206070 1 JK RC204A RECEPTACLE 26 PIN MOONEY...

Page 420: ...CLAMP AMP 206062 1 JK RC277A RECEPTACLE AUDIO AMP 2061 52 1 CLAMP AMP 206070 1 JK SB1OIA C B SPEED BRAKE KLIXON 7277 2 3 JK SB102A SWITCH SPEED BRAKE PRECISE FLT 01265 JK SB103A PLUG 3 PIN AMP i 3803...

Page 421: ...IXON 7277 2 1 JK WE 02A LIGHT GEAR DOWN SLOAN 855S 0 U BULB GE 327 J WE1OBA SWITCH THROTTLE MICRO V3 1 ACTUATOR MICRO JV 5 K WE1 03A SWITCH THROTTLE MICRO 1SEI T ACTUATOR MICRO JE 17 JK WE104A HORN GE...

Page 422: ...53 1 CLAMP AMP 206062 1 JK WV104A PLUG 4 PIN AMP 206060 1 CLAMP AMP 206062 1 JK WW1OIA SWITCH ALTERNATE AIR CHERRY E51 50B NOTES 1 USE AN4076 1 ADAPTER 2 USE WITH FT101 FT101A FUEL FLOW SYSTEM 3 USE W...

Page 423: ...SA MECH PROD 4200 002 5 ALT KLIXON 7277 2 5 BR7 5 CIRCUIT BREAKER 7 5A MECH PROD 4200 002 7 5 ALT KLIXON 7277 2 7 5 BR10 CIRCUIT BREAKER 10A MECH PROD 4200 002 10 ALT KLIXON 7277 2 10 BR15 CIRCUIT BR...

Page 424: ...CLAMP 25 PIN DB51212 LOCK RETAINER DB51221 1 CL25B CLAMP 25 PIN DB19S77 2 LOCK RETAINER DBS1221 1 CL25C CLAMP 25 PIN D824659 LOCK RETAINER D 20418 2 CL32A CLAMP 32 PIN M85O49 52 1 22N CL32B CLAMP BOOT...

Page 425: ...OIL TEMP MS28034 1 DI1O1A DIODE 1N2483 1 N5060 ALT dE 3720 GE D1102A DIODE 10H3P ALT ECG 5854 ALT NTE 5854 D1104A BRIDGE DIO DE FAGOR FB500i D1105A BRIDGE DIODE FAGOR FB5006 DJ1OIA XDCR OIL PRESS DRU...

Page 426: ...450004 1V 1H ETIOSA MAIN UNIT ASSY AMERI KING AK 450 FH1OIA FUSEHOLDER LITTEL FUSE 155020 ALT LITTEL FUSE 155120 FH102A FUSE HOLDER McGRAW EDISON FHN42W FO101A PHONE JACK SWTTCHCRAFT C i 1 WASHERS SWI...

Page 427: ...OONEY 880048 615 LE1 03A LENS ANNUNC US M20M MOONEY 88004 617 LE1 04A LENS ANNUNC FRANCE M20M MOONEY 880048 619 LE1 05A LENS ANNUNC M20T MOONEY 88004 621 LE1 06A LENS ANNUNC M20T MOONEY 88004 623 LE1...

Page 428: ...TAXI LIGHT MOONEY 880052 523 LT1O1B SWITCH TAXI LIGHT MOONEY 880052 1 23 LT102A BULB LIGHT TAXI LH 8 RH GE 4596 MA1O1A RECEPTACLE AUX POWER AN2552 3A MBi 01A C BSWTTCH RADIO MASTER CINHT MOONEY 93002...

Page 429: ...83 PB1OIA BATTERY GILL 6243 PB102A SWITCH MASTER MOONEY 880052 501 PB1 028 SWITCH MASTER MOONEY 880052 101 PB1 03A SWITCH BAT 1 2 MOONEY 880052 527 PB1 038 SWITCH BAT 1 2 MOONEY 880052 1 27 PB1 05A BA...

Page 430: ...04A RECEPTACLE 4 PIN AMP 206153 1 RC04B RECEPTACLE 4 PIN M3100 32 17P RC04C RECEPTACLE 4 PIN AMP 1 480426 0 RCOGA RECEPTACLE 6 PIN MATRIX SCIENCE MS3100C 2 22P RC08A RECEPTACLE 8 PIN AMP 205841 2 RCOS...

Page 431: ...AL 5 OK OHM ALLIED 753 8059 SA1OIA ALTERNATOR STAND BY B C BC41 0 1 HOUSING PLASTICCONNECTOR B C 12 003 TERMINAL 1 4 INCH B C 14 026 SA102A CONTROLLER STBY ALTERNATOR B C 8 203 2 SA103A SWITCH STBY AL...

Page 432: ...5 22 SW121A SWITCH dROljZEi 83 450 001 SW122A SWITCH CROUZET 83 452 504 SWI 23A SWITCH ALCO MPEI 06F SW124A SWITCH SW1 35A SWITCH N KK MB2085SB1WD EA VR1OIA VARISTOR GE V47ZA05 WM1 01A WARNING MASTER...

Page 433: ...MOONEY AIRCRAFT CORPORATION M20K SERVICE AND MAINTENANCE MANUAL 28V SM 25 2000 THRU 25 TEA RESERVED FOR FUTURE ENTRIES 91 20 04 87 OLDWILLWAYNE...

Page 434: ...SERVICE AND MAINTENANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION 28V S N 25 2000 MRU 25TBA RESERVED FOR FUTURE ENTRIES 91 20 04 88 OLDWILLWAYNE...

Page 435: ...MOONEY AIRCRAFT CORPORATION M20K SERVICE AND MAINTENANCE MANUAL 28V SM 25 2000 MRU 25 iBA RESERVED FOR FUTURE ENTRIES 91 20 04 89 OLDWILLWAYNE...

Page 436: ...ANCE MANUAL M20K MOONEY AIRCRAFT CORPORATION 9130 00 ELECTRICAL SYSTEM SCHEMATICS SEE ENVELOPES FOR THE ELECTRICAL SYSTEM SCHEMATICS PLEASE SEE THE NEXT PAGE FOR THE LOCATIONS OF THE SCHEMATICS 91 30...

Page 437: ...AMOB303 U 800330 F6 25 0781 thru 25 0841 AMOB304 A 800330 F7 25 0842 thru 25 0856 AMOB304 E 800330 F 8 25 0857 thru 25 0999 AMOB304 800350 Kl 2511000 thru 25 1199 AMOB304 M sheet 1 of 2 800350 K1 251...

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