Page 1 MOONEY M20V SERVICE AND MAINTENANCE MANUAL P/N: MAN185 ISSUED: MARCH 2017 REVISED: OCTOBER 2017 MOONEY INTERNATIONAL CORPORATION Copyright 2017 - All Rights Reserved MOONEY INTERNATIONAL CORPORATION - 165 Al Mooney Road, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com...
Page 3 Manufactured with 1,1,1 Trichlorethane substances which are determined to harm public health and environment by destroying ozone in the upper atmosphere. This warning applies to placards manufactured at Mooney Aviation Company, Inc. facility and installed on the Mooney Aircraft Model(s) addressed in this pubication.
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Page 5 SERVICE AND MAINTENANCE MANUAL LOG OF REVISIONS The Log of Revisions pages are updated by Mooney International Corporation each time revisions are issued. The Log of Revisions contains a list of all revisions made to the service and maintenance manual since its original issue.
Page 6: Table Of Contents
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Table of Contents Rev A Page 17 Rev A - Revised Aileron Allowable deflection up or down Chapter 28 FUEL: ALL Pages Original Issue Chapter 30 ICE PROTECTION: ALL Pages Original Issue...
Page 7 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ALL Pages Original Issue Chapter 80 STARTING: ALL Pages Original Issue Chapter 81 TURBOCHARGER: ALL Pages Original Issue Chapter 91 ELECTRICAL WIRING SCHEMATICS AND HARNESSES: ALL Pages Original Issue Chapter 95 SPECIAL TOOLS:...
Page 8 At the time of delivery, applicable service bulletins are normally incorporated. When a subsequent Service Bulletin is issued after the delivery date, Mooney International Corporation will post them on the www.mooney.com website for owner’s concerning details for compliance. The Service Bulletin number, date, title and incorporation should be noted in the log provided .
Page 9 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL S.B. DATE DESCRIPTION OF COMPLETED BY NUMBER BULLETIN LOG OF REVISIONS/SERVICE BULLETINS Page MAR 2017 Rev Date Date...
Page 10: Fuel
This manual provides servicing and maintenance infor- broad separation of content, ie., Airframe Systems vs mation for the Mooney Model M20V, Serial Numbers Powerplant Systems. These groups are identified by 33- 0001 and ON. Maintenance actions that refer to a tabs.
Page 11 The following list of Manufacturers and/or publications can provide servicing and maintenance information on com- ponents of the Mooney, Model M20V. Not all avionics equipment Manufacturers or publications are listed due to the many configurations that can be installed in the aircraft. These can be obtained from the repair stations for a particu-...
Page 12 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL FUEL PUMP (Engine Driven) Bose Corporation 145 Pennsylvania Avenue Continental Motors Framingham, MA 01701 Aircraft Products P.O. Box 90 DRE Communications Company Mobile, Alabama, USA, 36601 1723 Little Orchard Street Attn: Publications Dept.
Page 13: Table Of Contents
MOONEY AVIATION COMPANY, INC. M20V SERVICE AND MAINTENANCE MANUAL CHAPTER - SECTION - TITLE INDEX GUIDE CHAPTER SECTION TITLE 1 - 3 RESERVED - MAY BE USED LATER AIRWORTHINESS LIMITATIONS TIME LIMITS/MAINTENANCE CHECKS GENERAL TIME LIMITS SCHEDULED MAINTENANCE CHECKS DIMENSIONS AND AREAS...
Page 14 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER SECTION TITLE AUTOPILOT SYSTEMS (OPTIONAL) GENERAL GARMIN GFC- 700 TROUBLESHOOTING AUTOPILOT DISCONNECT SWITCH SYSTEM MONITORING ELECTRICAL POWER GENERAL DC GENERATION ELECTRICAL LOAD DISTRIBUTION EQUIPMENT/FURNISHINGS GENERAL FLIGHT COMPARTMENT CARGO COMPARTMENT EMERGENCY EQUIPMENT...
Page 15 MOONEY AVIATION COMPANY, INC. M20V SERVICE AND MAINTENANCE MANUAL CHAPTER SECTION TITLE LANDING GEAR GENERAL MAIN LANDING GEAR AND DOORS NOSE LANDING GEAR AND DOORS EXTENSION AND RETRACTION WHEELS AND BRAKES STEERING POSITION AND WARNING MISCELLANEOUS LIGHTS GENERAL 10/20 INTERIOR LIGHTS – MAINTENANCE PRACTICES EXTERIOR LIGHTS –...
Page 16 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER SECTION TITLE FUSELAGE GENERAL MAIN FRAME FIREWALL PLATES/SKIN ATTACH FITTINGS STABILIZERS GENERAL HORIZONTAL STABILIZER ELEVATOR VERTICAL STABILIZER RUDDER WINDOWS GENERAL 10/20 WINDSHIELD & CABIN WINDOWS ACRYLIC DRILLING WINGS GENERAL MAIN FRAME...
Page 17 MOONEY AVIATION COMPANY, INC. M20V SERVICE AND MAINTENANCE MANUAL CHAPTER SECTION TITLE ENGINE FUEL SYSTEM GENERAL DISTRIBUTION CONTROLLING INDICATING FUEL INJECTOR FUEL PUMP IGNITION GENERAL POWER CONTROL ENGINE FIRING ORDER SWITCHING ENGINE CONTROLS GENERAL ENGINE CONTROLS RIGGING MAINTENANCE ENGINE INDICATING...
Page 18 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER SECTION TITLE TURBINES GENERAL TROUBLESHOOTING SERVICING PERIODIC REPLACEMENT COMPONENTS SCHEMATICS AND HARNESSES GENERAL ELECTRICAL SYSTEM HARDWARE CHARTS SCHEMATICS AND HARNESSES SPECIAL EQUIPMENT INTRODUCTION Page MAR 2017 Rev Date Date...
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Page 20 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS...
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Page 22 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 4- Effectivity ....... . .
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Page 24 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 4- 00- 00 ......Airworthiness Limitations ......5 4- 10- 01 .
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Page 26 MOONEY INTERNATIONAL COPORATION M20V SERVICE AND MAINTENANCE MANUAL 4-00-00 - AIRWORTHINESS LIMITATIONS - MODEL M20V (Normal Category) S/N’s 33- 0001 and ON The Airworthiness Limitations Section is FAA approved and specifies maintenance required under 14 CFR ww 43.16 and 91.403 unless an alternative program has been FAA approved.
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Page 28 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS/ MAINTENANCE CHECKS...
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Page 32 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS/MAINTENANCE CHECKS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 5- 00- 00 ......General ..........5 5- 00- 01 .
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Page 34 11 AMP HR, 24 Volt, batteries. The al- ternator system has an overvoltage protective relay AIRCRAFT DESCRIPTION. The M20V series of air- and an overvoltage annunciation. Circuit breakers pro- craft are two door, four place, high- performance, tur- tect the electrical wiring and equipment from overloads.
Page 35 On Condition Powerplant (Chapter 71) Engine Refer to Engine Manufacturer’s Continued Airworthi- ness Data for specific Time Limits. Mooney has no special requirements over those found in the Manu- facturer’s Data. Propeller (See Special Note below) Refer to Propeller Manufacturer’s Continued Airwor- thiness Data for specific Time Limits.
Page 36 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Lights (Chapter 33) Position and Anti- Collision Lights LED: On Condition Note: LED lighting must have all LED segments operational. If one or more segments have failed, the entire light assembly must be replaced.
Page 37 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL G1000 - Servicing Information On Condition Servicing Maintenance Manual (#190- 00638- 01 Rev A or later FAA approved revision) . Replacement and/or servic- “On Condition” replacement and/or servicing should ing should be made only after the technician trouble-...
Page 38 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL G1000 GFC700 AFCS GFC700 ACFS System Complete Visual Inspection Aircraft Annual Flap Discrete Function Check ( Airworthiness Limita- Test the Flap- in- motion discrete inputs to the 100 Hours or Aircraft Annual tion Maintenance Requirement G1000 to verify proper operation.
Page 39 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 5-20-00 - SCHEDULED MAINTENANCE CHECKS 4. Pipe Threads - Tightening and torque procedures. Lubricate pipe threads as follows: Inspection Intervals. Perform a 25, 50, or 100- hour in- Oxygen Lines - Use only MIL- T- 5542 thread com-...
Page 40 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL TORQUE VALUES See Following Tables. FLARE NUT TORQUE VALUES- Tighten to minimum torque value for appropriate size as shown in table below. CAUTION - These torque values are derived from oil- free cadmium- plated threads.
Page 41 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 184/135 420/309 590/435 710/523 250/184 570/420 800/590 960/708 31/232 725/534 1020/752 1220/899 470/346 1070/789 1510/1113 1810/1334 635/468 1450/1069 2050/1511 2450/1806 865/637 1970/1452 2770/2042 3330/2455 1111/819 2530/1865 3560/2625 4280/3156 1440/1062 3290/2426 4620/3407 5550/4093 TIGHTENING TORQUES - Untreated Hardware (Black Finish) Friction Coefficient 0.14...
Page 42 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 230/169 530/390 745/549 890/656 295/217 675/497 960/708 1140/840 435/320 995/733 1400/1032 1680/1239 590/435 1350/995 1900/1401 2280/1681 800/590 1830/1349 2580/1902 3090/2278 1030/759 2360/1740 3310/2441 3980/2935 1340/988 3050/2249 4290/3163 5150/3798 TIGHTENING TORQUES - Electrically Zinc Plated Hardware - Friction Coefficient 0.125...
Page 43 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 7/8- 14 2500- 3000 1500- 1800 3550- 4350 2100- 2600 1- 14 3700- 5500 2200- 3300 4500- 5500 2700- 3300 1 1/8- 12 5000- 7000 8000- 4200 6000- 7300 3600- 4400 1 1/4- 12...
Page 44 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 1. Visually inspect propeller, spinner, and engine F. Inspect engine intake and exhaust systems for cowling; remove cowling. evidence of leakage, looseness or damage. G. Inspect ignition leads, harness, spark plug el- 2.
Page 45 Inspect cylinders for burned paint and cracked and bro- letins and Instructions. Check for aircraft conformance ken fins. Inspect baffle sealant. to FAA Specification 2A3 for M20V Model aircraft. K. Inspect accessory case, starter, alternator, fire- Recommended 100- hour/annual and special inspec- wall and fittings for security and damage.
Page 46 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL cable housing swage at the HEAD tube and security of 3. LANDING GEAR and RETRACTION SYSTEM attachment. INSPECTION. A. Inspect tires for proper inflation, cuts, blisters, -NOTE- slippage and excessive wear. Replace with new, ap- Cablecraft control cables are lubricated for the proved, tire(s), if necessary.
Page 47 D. Inspect tubular structure for corrosion and dam- 27-96-01). age (interior side panels will require removal). (Refer- ence Mooney Service Bulletin M20- 208A for specific F. Inspect empennage for corrosion, damage, procedures required annually). loose or popped rivets, free- play, dents, scratches, cracks, condition and lubrication of hinge points, at- E.
Page 48 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL I. Inspect empennage attachment brackets and grommet should be wrapped. See Service hardware for corrosion. Bulletin M20-185. 8. FLIGHT CONTROL INSPECTION. MAX. TUBE WEAR- .007 in. wall thickness or .014 in. diameter reduction.
Page 49: Ice Protection
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL E. Inspect flight panel for security of mounting, if the PROP DE-ICE switch is in ON position with Green condition of shock mounts, freedom from interference PROP DE-ICE switch lamp illuminated, but PROP with structure and condition of ground straps.
Page 50 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL REFERENCE FIGURE 5- 1 FOR LOCATION OF THE FOLLOWING COMPONENTS NOTE - Access covers riveted in place during production need not be removed for routine inspections. 5-20-09 - ACCESS COVER IDENTIFICATION, LUBRICATION AND SERVICE GUIDE...
Page 51 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ITEM ITEM DESCRIPTION LUBRICATION INTERVAL SYMBOL * (HOURS) Elevator & Rudder Controls: Control Tube Rod End Bearings  Aileron Control Tube Guide Blocks Aileron Controls: Control Tube Rod End Bearing  Bellcranks ...
Page 52 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ITEM ITEM DESCRIPTION LUBRICATION INTERVAL SYMBOL * (HOURS) Engine Instruments Radios Engine Controls  Oil Dip Stick, Oil Filler Tube  Wheels & Brakes: Wheel Bearings  Brake Pressure Plates Anchor Bolts & Guide Pins ...
Page 53 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL LUBRICATION SYMBOL LEGEND SYMBOL MIL. SPEC. NO. DESCRIPTION  MIL- L- 7870 Low Temperature Oil (General Purpose) MIL- G- 81322 Grease (Wheel Bearing) or  Mobil SHC 100 Mobil Aviation Grease (Wheel Bearing) (Synthetic) ...
Page 54 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 15 & 16 ACCESS COVER IDENTIFICATION, LUBRICATION & SERVICE GUIDE FIGURE 5- 1 5-20-09 Page MAR 2017 Rev Date Date...
Page 55 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL A copy of this form can be found in the Support Section of our website at www.mooney.com QUALITY ASSURANCE FORM QA1027M FIGURE 5- 2 5-20-09 Page MAR 2017 Date Rev Date...
Page 56 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 6 DIMENSIONS AND AREAS...
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Page 60 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 6 DIMENSIONS AND AREAS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 6- 00- 00 ......Dimensions and Areas ....... . 5 6- 00- 01 .
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Page 62 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 6-00-00 - DIMENSIONS AND AREAS 6-00-01 - AIRCRAFT SPECIFICATIONS SUBJECT STANDARD METRIC/OPT/MISC. ENGINE Engine Manufacturer Continental Motors Inc. Engine Model TSIO- 550- G(5) No. Cylinders Rated Horsepower 280 HP (Maximum Continuous Power - 2500 rpm)
Page 63 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL TURBOCHARGER CMI/ Turbocharger Mfg. KELLY AEROSPACE Type Exhaust Driven Model TA36 PROPELLER Propeller Mfg. Hartzell 3- Blade Type Constant Speed PHC- J3YF- 1RF/F7693DF- 2 Model Model PHC- J3YF- 1RF/F7693DF(B)- 2 Note: (B) Indicates W/Boots Installed) Pitch Angle @ 30 in.
Page 64: Landing Gear
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL FUSELAGE - CABIN DIMENSIONS Height 44.5” 113 cm Width 43.5” 110.5 cm Length 126” 315 cm Cabin Door Width 34.0” 86.36 cm Cabin Door Height 32.5” 82.55 cm - BAGGAGE COMPARTMENT MAX. Loading 120 Lbs.
Page 65 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 6-00-03 - AIRCRAFT STATIONS NOTE The datum line station 0.0 is 13 inches aft of the nose gear trunnion pivot point (Reference Figure 8- 2.). 26’- 8” (812.8 cm) 8’- 6” 76”...
Page 66 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 103.50 210.97 147.75 59.25 24.50 193.50 WING STATION RIBS - 5.375 3.68 211.50 - 5.00 176.00 142.00 53.00 21.80 100.00 FUSELAGE STATIONS WING STATION RIBS AND FUSELAGE STATIONS FIGURE 6- 2 6-00-03...
Page 67 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 70.0 42.25 4.43 42.25 70.0 52.50 25.75 5.25 EMPENNAGE STATIONS FIGURE 6- 3 6-00-03 Page MAR 2017 Date Rev Date...
Page 68 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 7 LIFTING AND SHORING...
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Page 72 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 7 LIFTING AND SHORING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 7- 10- 00 ........Jacking ........5 7- 10- 00 .
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Page 74 010000- 000) in tiedown mounting holes outboard of each main landing gear. Install Nose Landing Gear jack point (1) (jackpoint, Mooney P/N 010000- 000) into re- -CAUTION- ceptacle (located under the cowling at Fuselage Sta- tion - 5.51) - Refer to Figure 7- 1.
Page 75: Lights
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ENGINE LIFT POINTS (CONTINENTAL ENGINE) WARNING DO NOT USE PROPELLER JACKS OR PROPELLER STANDS WARNING DO NOT USE AS A JACK POINT ENGINE DO NOT LEAVE ON LIFT POINT AIRCRAFT DURING FLIGHT (LYCOMING ENGINE) “A”...
Page 76 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 8 LEVELING AND WEIGHING...
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Page 80 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 8 LEVELING AND WEIGHING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 8- 00- 00 ......Leveling ..........5 8- 00- 01 .
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Page 82 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 8-00-00 - LEVELING 3. Ground aircraft and drain fuel tanks per Section 12-10-02. Place a spirit level on the leveling screws above the tail- 4. Add unusable fuel to each tank, (see Pilot’s Oper- cone access door (see Figure 8- 2) when leveling the ating Handbook for proper quantity of unusable fuel).
Page 83 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CENTER of GRAVITY - F.S. - mm 1050 1070 1090 1110 1130 1150 1150 2500 (Kg) LBs. “ON” or “ABOVE” LINE 1100 2400 1050 2300 1000 2200 2100 NO BALLAST WEIGHT REQUIRED...
Page 84 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL REF.POINT REFERENCE LEVEL REF. (NOSE GEAR DATUM(STA.0) (LEVELING SCREWS) TRUNNION STA. - 13) Lc/g MEASUREMENTS Lm/r Lm/n INCHES/CM INCHES/CM WEIGHT AND BALANCE DIAGRAM FIGURE 8- 2 8-00-01 Page MAR 2017 Rev Date...
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Page 86 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 9 TOWING AND TAXIING...
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Page 88 MOONEY AVIATION COMPANY, INC. M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 9 TOWING AND TAXIING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 9- Effectivity ....... . .
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Page 90 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 9 TOWING AND TAXIING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 9- 00- 00 ......Ground Handling ........5 9- 10- 00 .
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Page 92 9-10-00 - TOWING 5. Check Garmin G1000 Multi Function Display Use a towbar (Mooney P/N 010034- 515) for moving (MFD) for any sluggish response to engine control aircraft. The towbar attaches to nose gear crossbar.
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Page 94 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 10 PARKING AND MOORING...
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Page 96 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 10 PARKING AND MOORING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 10- Effectivity ....... .
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Page 98 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 10 PARKING AND MOORING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 10- 00- 00 ......General ..........5 10- 10- 00 .
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Page 100 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 10-00-00 - GENERAL 4. Raise aircraft to remove weight from tires, and block up wheels. The parking brake is set by applying brakes and pulling out on parking brake control knob. Release parking -CAUTION- brake by pushing IN on parking brake control knob.
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Page 102 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS...
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Page 106 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 11- 00- 00 ......General ..........5 11- 10- 00 .
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Page 108 All required plac- ards can be procured from any one of the Authorized 11-10-00 - MARKINGS - EXTERIOR PAINT Mooney Service Centers, visit www.mooney.com for a Exterior paint schemes are depicted in M20V Illus- list of names and contact numbers. 11-00-00 Page...
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Page 110 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 12 SERVICING...
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Page 112 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 12 SERVICING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 12- Effectivity ....... .
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Page 114 MOONEY INTERNATIONAL M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 12 SERVICING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 12- 00- 00 ......Servicing ..........5 12- 00- 01 .
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Page 116 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 12-00-00 - SERVICING -WARNING- 12-00-01 - SERVICING INTERVALS After servicing aircraft with fuel, wait at least The specified intervals (refer to Chapter 5) are consid- five minutes for moisture and sediment to...
Page 117 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 12-10-04 - OXYGEN SYSTEM -NOTE- PRECISE FLIGHT SYSTEM (OPTIONAL) When defueling using removable tank quick The oxygen cylinder, when fully charged, contain drains, it is only necessary to remove the drains approximately 77 cubic feet of aviators breathing oxy- and to operate the gascolator drain.
Page 118 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL red oil stops dripping. Replace gasket with a new on the electrolyte and water. Keep battery electrolyte above a frame surface to be mounted to the air box assembly. specific gravity of 1.225 to avoid freezing.
Page 119 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 12-20-05 - HYDRAULIC BRAKES (Bleeding) 3. Attach pressurized hydraulic fluid service unit to wheel cylinder bleeder valve and open valve. Hydraulic service unit should be free of air prior to servicing air- -CAUTION- craft system.
Page 120 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 12-20-06 - CLEANING F. Blow moisture away from areas that may trap & accumulate water, IE. engine mount at firewall attach Cleanliness is a major prerequisite to adequate inspec- points (inside cupped portion of tubing).
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Page 122 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES - AIRFRAME...
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Page 126 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES - AIRFRAME TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 20- 00- 00 ......General ..........5 20- 00- 01 .
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Page 128 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 20-00-00 - GENERAL nance, Preventive Maintenance, Rebuilding and Alter- ation and Sub Parts A, D and E of FAR 65, Certification. This chapter of the manual discusses treatment of met- Advisory Circular 43.13- 1( ) outlines inspection and re- al surfaces for corrosion control and the identification of pair practices acceptable to the F.A.A.
Page 129 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL - 5.375 3.68 211.50 - 5.00 176.00 142.00 100.00 53.00 21.80 INDEX SKIN MATERIAL THICKNESS ... . 0.025 ....
Page 130 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 42.25 42.25 25.75 INDEX SKIN MATERIAL INDEX SKIN MATERIAL THICKNESS THICKNESS ... . 0.025 ...
Page 131 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (1) Intergranular Corrosion - Selective attack -NOTE- along grain boundaries of metal alloys is referred to as ACF- 50 or equivalent can be fogged into fuse- intergranular corrosion. Aluminum alloys 2024 and lage, empennage or wing skin areas.
Page 132 .05 to 1.5 hours but not tubular structure or exterior skin) and for the year and more than 2 hours before application of the top or inter- model being repainted. (Refer to Mooney Illustrated mediate primer coat. Parts Catalog).
Page 133 .003 inch. 6. Refer to manufacturer specifications for suggest- 2. Epoxy prime per Mooney spec 20 sect 42 (contact ed equipment and precautions. Mooney Technical Support for instructions) for metallic substrates, or use p900 (catalyst no. c916) or approved...
Page 134 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL will be needed. A beveled edge with a very shallow ta- per should result. See Figure 20-5. SAND SURFACE TO A BEVEL VIEW LOOKING UP SAND DAMAGED PORTION FIGURE 20- 5 3. Prepare surface surrounding the hole by removing dust and debris.
Page 135 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL HYSOL MIXTURE PATCH SECURED CLECO AND CLAMP ALUMINUM PATCH APPLY HYSOL TO ALUMINUM PATCH FIGURE 20- 9 FIGURE 20- 7 9. Coat the outer portion of the patch and the sanded 8. Apply patch to inner surface of shell and cleco into area of shell with Resin Mix 1.
Page 136 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL plies with rubber gasket facing plies. Clamp/cleco in place. Cure at room temperature. See Figure 20- 13. FIBERGLASS PLIES RUBBER GASKET ON INNER CAUL PLATE CUT AND COAT FIBERGLASS PLIES FIGURE 20- 11 11.
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Page 138 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 21 ENVIRONMENTAL SYSTEMS...
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Page 142 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 21 ENVIRONMENTAL SYSTEMS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 21-00-00 ......Cabin Ventilation System ......5 21-40-00 .
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Page 144 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 21-00-00 - CABIN VENTILATION SYSTEM 21-40-00 - HEATING The cabin environmental system consists of three Heat is extracted from the high pressure/temperature standard ventilating systems that supply heated or flow between the compressor and intercooler through fresh air as the pilot or passengers prefer.
Page 145 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 21-50-00 - COOLING (OPTIONAL EQUIPMENT) the R- 134a compressor where the process starts all over again. GENERAL In addition to cooling cabin air, a refrigerant type sys- The type of cooling system installed in an aircraft oper-...
Page 146 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL AIR19A14 FIREWALL #1 CIRCUIT BREAKER PANEL #1 AIR COND TAILCONE AIR COND SWITCH AIR01A14 AIR COND SWITCH AIR101A CL04A PL04A RC04A CL04A AIR08A14 RED *** ORANGE *** AIR11A14 BLACK *** RED ***...
Page 147 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL DRYER/ HAT RACK CONDENSER PRESSURE BULKHEAD SWITCH TUBE TUBE HOSE HOSE TUBE HOSE FAN/MOTOR EXPANSION VALVE FIREWALL BULKHEAD HOSE TUBE EVAPORATOR HOSE HOSE TUBE EVAPORATOR FIREWALL HAT RACK BULKHEAD BULKHEAD COMPRESSOR PLUMBING SCHEMATIC – AIR CONDITIONING SYSTEM (TYP.)
Page 148 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 2. Remove, if required, any enclosures or access -CAUTION- doors to expose all tubing, hoses, fittings, etc. to the compressor- condenser module/evaporator module. Do not use any leak dye in R- 134a system or damage to system may result.
Page 149 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 4. R- 134a charging manifold, with gauges and 9. Disconnect manifold YELLOW service hose. Sys- hoses tem is ready for refrigerant charging. 5. Thermometer, 0- 150 -NOTE- 6. Inspection mirror, adjustable Excessive water and/or air in the system will cause pressure to rise/expansion valve freeze- 7.
Page 150 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 7. Move aircraft to run- up area. 13. With the system fully charged and operating, ob- serve the suction and discharge pressures shown in 8. Start aircraft engine. Select ”MAX” on air condi- the following chart.
Page 151 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 21-53-01 - SPECIAL TOOLS AND/OR EQUIP- 21-53-03 - EXPANSION VALVE ADJUSTMENT MENT The expansion valve adjustment shall be performed in accordance with, but not limited to the following: The following tools and/or equipment are required to perform expansion valve adjustment: 1.
Page 152 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 19. Replace all shrouds, covers and enclosures re- 21-54-02 - DRIVE BELT REPLACEMENT moved in step 2. PROCEDURE 1. Verify belt size and part number (see Illustrated 21-54-00 - COMPRESSOR DRIVE BELT Parts Catalog) before installing or damage may result.
Page 153 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 21-54-03 - DRIVE BELT ALIGNMENT PROCE- When alignment is correct, the extended arm will fall DURE into the center of the bottom of groove of compressor outer pulley groove within 0.020 inch.
Page 154 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 9. After five (5) hours of operation, recheck belt ten- -NOTE- sion and adjust as required to maintain 50- 70 lbs belt Checking compressor oil quantity is required tension. only if an excessive amount of oil is observed...
Page 155 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 3. Tighten mounting hardware (temporarily). -CAUTION- 4. Verify alignment of belt on all pulleys and align per Only an E.S.I. approved oil may be used in Section 21-54-03, if required. this type of compressor.
Page 156 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL H. Connect power leads to blower assembly and -NOTE- test for proper operation. At this point it is very important to observe the I. Replace all ducting, shrouds, closures, etc. Unit wire colors and connections from the resistor is ready for operation.
Page 157 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 21-57-00 - TROUBLESHOOTING R- 134a AIR CONDITIONING SYSTEM There may be a time when the system does not operate and/or perform in accordance with information contained herein. Therefore, it is necessary for the service personnel to diagnose the discrepancy by troubleshooting the system and its components.
Page 158 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL D. Evaporator noisy 1. Wobbly blower wheel 1. Replace 2.Blower wheel hitting scroll 2. Align 3. Defective blower motor bearing 3. Replace motor 4. Loose mounting bracket 4. Tighten 5. Air inlet clogged 5.
Page 159 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL J. Pressure switch cycles (high 1. System over charged 1. Reclaim refrigerant as required pressure cutout) 2. Condenser coil inlet air extremely 2. Normal condition 3. Condenser inlet clogged 3. Remove debris 4.
Page 160 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CONDENSER/EVAPORATOR COIL Inspection 500- 800 Replacement On Condition PRESSURE SWITCH Calibration check 1000 Replacement On Condition REFRIGERANT SYSTEM Performance check 500- 800 Visual inspection 500- 800 2. AIR CONDITIONING SYSTEM “OFF SEASON”...
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Page 162 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 22 AUTOPILOT SYSTEMS...
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Page 166 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 22 AUTOPILOT SYSTEMS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 22- 00- 00 ......General ..........5 22- 10- 00 .
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Page 168: Navigation
Cockpit reference guide for more detailed informa- command bars and the autopilot mode annunci- tion. ations. The LRU’s used by Mooney (if installed) B. GDU 10XX MFD - Provides controls for the autopilot functions. - GDU 10XX Multi Function Display (MFD) C.
Page 169 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL GTX 33 GDU 10(XX) PFD GIA 63 #1 GIA 63 #2 GDL 69 PITCH SERVO PITCH TRIM SERVO FORWARD/AFT AFT HARNESS ROLL SERVO DISCONNECT (ON GFC700) FORWARD HARNESS CABIN AREA GMU 44...
Page 170 USE CARE WHEN REMOVING SERVO rig the aircraft control cables. The M20V aircraft is MOUNT FROM AIRCRAFT NOT TO ALLOW equipped with 3 servos and servo mounts.
Page 171: Structures
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (see Figure 22- 3). Ensure control rod ends are prop- I. Configure software (if required) and test per erly engaged through witness holes in rod. Refer to the G1000 Line Maintenance and Configuration Chapter 27- 10- 00 for Aileron Rigging.
Page 172 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL mount. A master link on the chain will allow chain to A. For instructions on checking the slip- clutch, be removed from Aircraft . (see Figure 22- 5) refer to the GSM Slip- Clutch Setting Procedure in the GSA 8X/GSM 86 Installation Manual (Garmin B.
Page 173 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL G. Using servo mount bracket (slide up or down) set chain tension such that a 1-2 lb force causes CABLE GUARD BRIDLE CABLE COVER deflection of 1/8”. To be measured at the point of lon-...
Page 174 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL payoff angle equals or exceeds 3 deg. limit, adjust move, with some resistance, through their range of bracket position to reduce payoff angle . motion. I. Install RH Tailcone access panels. -NOTE- It is not necessary to move each trim control J.
Page 175 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ALLOWABLE RECOMMENDED ITEM SPECIFICATIONS SPECIFICATIONS GSA 8X to GSM 86 bolt torque* 25-40 in-lbs 20-50 in-lbs GSM 86 to airframe bolt torque* 25-40 in-lbs 15-40 in-lbs GSM 86 clutch retianing bolt torque*...
Page 176 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 22-10-05 FLAP POSITION DISCRETE INPUT CHECK 22-20-01 LRU REPLACEMENT PROCEDURES Also refer to the G1000 Line Maintenance and Con- figuration Manual (#190- 00303- 04 Rev F and In- Installing the LRU per procedures in the G1000 Line...
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Page 178 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER...
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Page 180 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 24-Effectivity ....... . .
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Page 182 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 24- 00- 00 ..... . General ........... . 5 24- 00- 00 .
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Page 184 RH nosegear wheelhouse area on the C. When either battery is removed from the aircraft M20V model aircraft. If the primary alternator fails in for charging, be sure that the charger is correctly con- flight, the pilot activates the standby alternator. If the nected.
Page 185 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (1) Turn Master Switch OFF. Disconnect alterna- - Loss or opening of the Alternator Off Sense wire tor wiring. or voltage (2) Remove attaching hardware and pull alterna- Whenever the TSL on the unit is Red, the AOI is on.
Page 186 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL - Loss of or open Aux Voltage Sense - Field to Ground Short Fault APAC - Alt Off- Line UNIT Troubleshooting Light (TSL) – Located on the front plate of the unit, alerts the user to the condition of the alternator/APAC system.
Page 187 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL POST INSTALLATION TEST PROCEDURE BUS BAR 1. Turn On the Alt & Bat switches, observe that the Alt Fld Alt Out AOI light is on. 50A - 125A 2. On the APAC, the TSL should be Green. If the TSL is Red, the Field is shorted to ground.
Page 188 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL TROUBLESHOOTING - GENERAL (APAC) ken. A Green TSL indicates an open field wire or a “fly- ing- open” field connection in the alternator’s field. Check the 5 Amp breaker, ALT switch and connections Alternator Out Indicator (AOI) stays on always.
Page 189 ______v -NOTE- Terminal 1 Voltage ______v Refer to the M20V POH/AFM for specific equip- ment limitations 3. Measure the voltage on Terminal 6 of the regulator. 1. Perform a normal engine start and allow the en- It should be within 0.5 volts of the bus voltage. A differ- gine to reach proper temperature for run-up RPM.
Page 190 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL coming out of the alternator. It should measure within the engine RPM up to approximately 2000. Switch OFF 0.5 volts of the measurement on Terminal 5 of the regu- the primary alternator. Wait for the STBY ALT ON lator.
Page 191: Doors
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 6. The best plan is to stop the noise at its source. A. Mix one pound of baking soda (bicarbonate of Once the noise is SlooseS, it can be difficult to filter it out soda) in one gallon of water.
Page 192 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS ANNUNCIATION ANNUNCIATION ANNUNCIATION ACTION ACTION FUNCTION COLOR TRIGGER WHEN ON WHEN OFF GEAR DOWN GREEN GREEN GEAR DOWN DISPLAYED ON G1000 STEADY OFF WHEN GREEN GEAR IS UP “GEAR DOWN”...
Page 193 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS (CONT’D) GEAR DOWN - ALERT & ANNUNCIATION GEAR UNSAFE - ALERT & ANNUNCIATION FIGURE 24- 4 “IN TRANSITION” FIGURE 24- 7 GEAR UNSAFE - MASTER WARNING SPEEDBRAKE - ALERT &...
Page 194 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS (CONT’D) ALTERNATE AIR - ALERT & ANNUNCIATION PITOT HEAT FAIL - MASTER CAUTION FIGURE 24- 10 FIGURE 24- 13 PROP DE-ICE FAIL - MASTER CAUTION PITOT HEAT FAIL - ALERT & ANNUNCIATION...
Page 195 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS (CONT’D) ALTERNATOR FAIL - ALERT & ANNUNCIATION DOOR OPEN - MASTER WARNING FIGURE 24- 16 FIGURE 24- 19 START POWER - ALERT & ANNUNCIATION DOOR OPEN - ALERT & ANNUNCIATION...
Page 196 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS (CONT’D) HIGH BOOST PUMP - ALERT & ANNUNCIATION LOW FUEL LEFT WARNING FIGURE 24- 22 ALERT & ANNUNCIATION FIGURE 24- 25 LOW FUEL WARNING - LEFT OR RIGHT...
Page 197 After engine starts, the impulse coupling flyweights do not The M20V has a second battery that may be selected engage due to centrifugal action. The coupling then as the primary battery for a particular flight. The battery...
Page 198 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 3. Reading Lights. A momentary switch operates 4 24- 36- 00 - LANDING GEAR CIRCUITS overhead lamps in 3 modes. Reading Light Switch 1. Limit switches and relays operate the reversible UP position, only the Pilot reading light is activated.
Page 199 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 3. Fuel Flow System - A turbine type, fuel flow trans- 2. GCU 275/478 KEYPAD UNIT - The GCU 275/478 ducer is installed in the fuel line between the engine refers to the Garmin Flight Management System (FMS) driven fuel pump and the throttle body control of the fuel Controller used in a Garmin Integrated Flight Deck.
Page 200 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 24- 39- 00 - TROUBLESHOOTING CHARTS 24- 39- 03 - BATTERY TROUBLESHOOTING TROUBLE PROBABLE CAUSE REMEDY Discharged battery. Battery worn out. Replace battery. Improper charging rate setting. Reset charging rate. Excessive discharging.
Page 201 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 24- 39- 04 - STARTER TROUBLESHOOTING TROUBLE PROBABLE CAUSE REMEDY Motor fails to operate. Low battery. Check & recharge battery if reqd. Defective, improper, or loose wire Refer to electrical wiring diagram &...
Page 202 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 24- 50- 00 - ELECTRICAL LOAD DISTRIBUTION 24- 51- 00 - POWER DISTRIBUTION SYSTEM The power Buss distributes direct current power to the electrical system from the alternator and from the se- lected battery through the battery relay.
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Page 204 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT AND FURNISHINGS...
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Page 208 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT AND FURNISHINGS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 25-00-00 ......General ..........5 25-00-01 .
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Page 210 25-00-01 - INTERIOR SURFACES mercially available leather cleaning products. Follow Mooney M20V interior components are finished in a va- the instructions on the product label, or: riety of materials including: A. Leather Care Instructions:...
Page 211 Re- Use wet/dry vacuum cleaner to remove foam and dry straint Systems for the Mooney M20V. Seat belts with the materials. Grease spots, on carpet, should be re- shoulder harness are standard Restraint System for moved with jelly- type spot lifter.
Page 212 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL B. When the equipment has sustained damage or -CAUTION- if malfunctions occur. INFLATABLE AIRBAG RESTRAINT SYSTEMS: C. When the equipment is transferred to another Do not immerse the airbag belt assembly into owner or for any special reason.
Page 213 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL The crash sensor’s predetermined deployment thresh- To activate the system, join (buckle) the three- point re- old does not allow inadvertent deployment during nor- straint in the same manner as any other three- point mal operations, such as hard landings, vibration, or tur- seatbelt.
Page 214 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL V23 SYSTEM DIAGNOSTIC TOOL FIGURE 25- 3 MAINTENANCE AND INSPECTION yearly by the OEM. Refer to program- specific Am- Safe’s Supplemental Maintenance Manual for return Maintenance information. No other maintenance is required other than an annual This test tool does not contain any self- annunciated inspection and functional testing of the system.
Page 215 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL System Diagnostic Tool: P/N: 508688- 201 -CAUTION- Where Used: AAIR System, V23 Aircraft (for Activa- DO NOT ATTEMPT TO USE THE SDT FOR tion Circuit AAIR Systems) SYSTEM CHECK AND/OR FAULT ISOLATION...
Page 216 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Connecting SDT: Confirm all seat positions to be tested Cable Assembly and connect the V23 SDT connector are unbuckled. Remove the Diagnostic Connector’s to the diagnostic connector. protective cap (if applicable) located on the Interface...
Page 217 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Inspection A detailed visual inspection should be performed at a minimum of once annually. Check Seatbelt Airbag Assembly for: Replace belt assembly if any of the following are ob- S Cut or worn edges...
Page 218 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Cleaning -CAUTION- It is recommended that AAIR components be cleaned WHEN CLEANING THE AAIR, CARE MUST BE on a regular (annual) basis. Build- up of dirt and TAKEN TO KEEP FOREIGN MATTER AND...
Page 219 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Torque Wrenches, In. Standard Issue -WARNING- Lb. Type to accommo- AVOID MAGNETIC FIELDS IN THE VICINITY OF date 5 to 130 In. Lbs of THE ELECTRONICS MODULE ASSEMBLY. DE- torque PLOYMENT OF THE SYSTEM MAY OCCUR.
Page 220 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 5. After removal of Inflator(s), replace Shipping Cap(s) 9. Remove Cable Interface Assembly. in the hose connector fitting. See Table 1 for torque val- 10. Remove EMA from mounting hardware (Aftermar- ket installations, refer to AmSafe Installation drawings 509760 - pilot, co- pilot seats or 509780 - passenger 6.
Page 221 25-50-00 - BAGGAGE COMPARTMENT TYPICAL EMA AIRCRAFT FORWARD INSTALLATION The M20V baggage compartment, located aft of the FIGURE 25- 6 rear passenger seats, has a capacity of 20.9 cu. ft. (0.59 cu. M) and a maximum allowable load of 120 lbs.
Page 222 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL The extinguisher has a twenty year shelf life and is not 6- Year Maintenance rechargeable. Every six years, stored pressure fire extinguishers that A344T Fire Extinguisher: (if equipped) require a 12- year hydrostatic test shall be emptied and A 1.3 lb.
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Page 224 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS...
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Page 228: Stabilizers
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 27-00-00 ......General ..........5 27-10-00 .
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Page 230: Wings
A rudder trim system is in- link to the control wheel through push−pull tubes and corporated into the M20V aircraft for pilot comfort for bellcranks. Lead counter−weights static balance the ai- high−power settings during climb and, if needed, for lerons.
Page 231 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL YOKE CONTROL CONTROL TUBE JACKSHAFT SHAFT ASSY CONTROL YOKE CONTROL TUBE CONTROL TUBE SHAFT CONTROL YOKE CONTROL WEIGHT TUBE CONTROL JACKSHAFT TUBE ASSY CONTROL YOKE YOKE JACKSHAFT CONTROL ELEVATOR ROD ASSY SHAFT...
Page 232 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL INBD VIEW AT L/H WING LOOKING UP PIN HOLE REACH 7 THRU HERE RUDDER PEDAL ADJUSTMENT FIGURE 27−4 2. Rudder Rigging and Adjustment. A. Raise aircraft nose wheel off ground. See Sec- tion 7−10−00.
Page 233 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL L. Center nose wheel by removing nut, washer and bolt (1), (Fig. 27−8), and adjusting steering idler linkage H. Unclamp rudder pedals. at (2). Bolts, nuts and washers (5) and (6) must be I.
Page 234 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (a) Trim screw jackshaft. Set elevators, RH/LH, to be level with horizontal stabi- lizer. Adjust rod end bearings (9) (Fig 27−9) at elevator (b) Trim link connecting empennage to trim horns. screw.
Page 235 -NOTE- A “stepped stop nut”, with a “jam nut” configura- tion has been incorporated. This can be retro- fitted to all M20V aircraft, if desired. This allows DETAIL trim screw nut (F) (Fig. 27−12) to contact stepped ”A”...
Page 236: Propellers
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (C). Tighten setscrew and turn trim control wheel to full The indicator is connected to the trim control wheel as- NOSE DOWN position, trim screw nut (F) against stop sembly to indicate stabilizer position relative to the air- (A) or stepped nut (E).
Page 237 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL C. Aileron−rudder interconnect system should be rigged properly prior to rigging of rudder trim system. (See Section 27−60−00) CAPSTAN LIMIT SWITCH CABLE ACTUATOR TURNBUCKLE SPRING RUDDER TRIM RIGGING (Typical Hardware Layout Shown) FIGURE 27−14...
Page 238 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL I. Attach one end of both springs to brackets on 27−41−00 − Stabilizer Trim System Troubleshoot- control tube bellcranks at Fuselage Stations 90.0 and 142.0. BINDING Check control tubes at bulk- J. Separate barrels and eyes of both turnbuckles head grommets for rub and attach one eye of turnbuckle to forward spring;...
Page 239 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 7. Place torque tube/pitch trim servo assembly on The flap switch is located on center console. Flap posi- work bench for removal and replacement of bearing tion is indicated on the Garmin G1000 Engine/Airframe block.
Page 240 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL D. Adjust switch stack until Bottom Micro−Switch from full up position. just opens. 3. Wing Flap Indicator – Rigging A. Adjust flap potentiometer (8) (Fig. 27−15) on air- E. Top switch will be automatically adjusted.
Page 241 -NOTE- CONTROL SURFACE IS CORRECT If specified moments cannot be met (reference Fig. 27−18), heavier balance weights can be ob- tained through a Mooney Service Center. This CONTROL SURFACE STATIC BALANCE approach should be examined before reworking DIAGRAM any repair or restripping and repainting the af- FIGURE 27−19...
Page 242 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL C. Disconnect the two wires from switch. .070 MAX. 2. Stall Warning Switch Installation. ALLOWABLE DEFLECTION A. Connect electrical wires to switch. B. Position switch in opening of lower wing leading AILERONS edge;...
Page 243 LH bulkhead. A Precise Flight, Inc. SpeedBrake System is currently installed in M20V aircraft as standard equipment. The The schematic, located in the envelopes, and the elec- manufacturer can provide detailed parts and mainte-...
Page 244 Refer to structure, via a custom mounting bracket, and is re- Mooney M20V Service & Maintenance Manual Chap- sponsible for transferring the output torque of the GSA ter 22 for more detailed information.
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Page 250 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 28 FUEL TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 28-00-00 ......General ..........5 28-00-01 .
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Page 252 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 28-00-00 - GENERAL system on the engine. Fuel quantity indicators are elec- trically operated with 2 transmitters (inboard and out Internally sealed, integral fuel tanks are in the L & R, for- board) located in each tank.
Page 253 Replace O- Rings at 5 years or unusual wear part num- Sealants are safe only when handled with reason- ber #225 suffix #NBR70 (was FPM 75) Mooney Service able care. Avoid ingestion and all contact with the Parts now offers a O- Ring Kit # OHK3.
Page 254 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (3) For sealant application life, tack- free curing (3) Place small amount of mixture on a clean time, and curing rates (see following Cure Rate table). strip of aluminum and spread sealant. Visually examine sealant film to determine whether accelerator is visible B.
Page 255 -NOTE- CS3204 A- 1/2, A- 2) over all seams, rivets, nuts, and Refer to Mooney SB M20- 230 for proper applica- bolts. A one inch, stiff bristle brush is recommended for tion of sealant and drain holes that are to be left sealant application.
Page 256 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL are assembled. Access panels in wing walk area (3) Heavy Seep - A fuel leak that reappears im- should be sealed with PRC 1422, Class B filleting com- mediately after area is wiped clean.
Page 257 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL A. Temporary Repair of Fastener Leaks. General- 28-13-00 - SOAPLESS BUBBLE FLUID FORMULA ly, all leaks in enclosed areas and running leaks in open PREPARATION FOR LEAK CHECK areas constitute a flight hazard. Fastener leaks of this...
Page 258: Ignition
28-24-00 - ENGINE PRIMING Tank drains are recessed and spring loaded closed. An There is no separate priming system on the M20V air- O- ring at lower flange seals drain valve seat. Check craft. Operating the Low boost pump switch in the cock- the tank drain valves after each use to verify the O- ring pit turns auxiliary fuel pump - ON.
Page 259 (3) Remove six screws attaching transmitter to For fuel system calibration, refer to Garmin “G1000 rib doubler. Post Installation Checkout” Mooney M20 Revision B or (4) Remove transmitter from rib. later. 2. REINSTALLATION - Reverse the fuel quantity Fuel transmitter test ohms (Rochester Gauges, Inc.) transmitter removal procedure.
Page 260 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 28-91-00 - TROUBLE SHOOTING - FUEL SYSTEM TROUBLE PROBABLE CAUSE REMEDY Fuel gauge not indicating. Broken wire. Check and repair. Faulty transmitting unit. Replace and adjust. Open circuit breaker. Check and reset.
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Page 262 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 30 ICE PROTECTION...
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Page 266 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 30 ICE PROTECTION TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 30- 00- 00 ......General ..........5 30- 10- 00 .
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Page 268 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 30-00-00 - GENERAL 30-11-01 - WASHING The M20V aircraft incorporates an alternate air system -CAUTION- that is designed to open automatically any time the air induction system becomes blocked. This system Do not use MEK (Methyl Ethyl Ketone) to clean should be inspected to assure that no heated air is en- titanium panels.
Page 269 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (2) When system pressure is obtained, the 4. Operate Windshield Spray bar on each windshield “Anti- Ice” LED should extinguish and the “De- Ice LED pump to ensure proper operation and absence of should show steady GREEN.
Page 270 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL OVERSHOE, RUBBER ENGINE BAFFLE, BULKHD. FTG. HOSE, FIREPROOF SPRAYBAR, WINDSHIELD FIREWALL, BULKHD. FTG. STALL STRIPS STALL STRIPS PANELS, POROUS, L/W PANELS, POROUS, R/W PROPORTIONING UNIT, R/W PUMPS, WINDSHIELD STALL WARN SWITCH, HEATED...
Page 271 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Windshield system does not operate. Pump(s) inoperative Replenish Fluid in tanks Inadequate Fluid content Check Pump(s) and Pump(s) wiring Solenoid Valve(s) Inoperative Check power to Solenoid Valve(s) Check Solenoid Valve(s) High pressure warning – LED illumi- OAT - COLD nates during operation.
Page 272 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CONTROL PANEL FAULT LED malfunction = AMBER (High Does not operate: Pressure Warn). Check Power to Control Panel. Depress High Pressure Reset: Illuminates =Check Auto Dimmer setting. Does not illuminate =Repair or replace Control Panel.
Page 273 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Press windshield De- Ice Switch. Check that de- icing fluid is discharged from spraybars. Check that wing ice inspection lamp functions. If night flight. Switch off electrical power if no longer required.
Page 274 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Press Windshield De- Ice switch. Check that de- icing fluid is discharged from spraybars. Check that no holes are blocked. Switch electrical power OFF. Level III Annual Inspections At Level III, it is recommended that all Level II Inspections are complied with and that the following inspections are added/included.
Page 275 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Check Low Pressure Warn Switch. 1. Remove empennage fairing for access. Disconnect Nylon tube from outlet of suspect pressure switch. Con- NOTE: nect a pressure gauge (0 - 5 lbf/in ) (0 to 3 bar) to the...
Page 276 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Level IV Maintenance Practice (con’t.) Procedures Check Porous Panels 1. Remove Access panels for access to applicable Pro- portioning Unit. Disconnect Nylon tube connecting sus- pect panel from outlet of Proportioning Unit. Connect suitable pressureable supply of filtered fluid to this tube.
Page 277 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Check Control Panel. (cont’d) (2) As (1) but with MAXIMUM selected. All pins zero volts except: NOTE: C1 - 3, & - 5 to be aircraft voltage. Voltages specified in Procedures are based on a C1 - 2 to be 7.5 volts* initially, changing to zero as...
Page 278 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 30-12-03 - FLUID LEVEL CALIBRATION To adjust fluid level reading at A/C instrument panel TKS Control Head: 1. Level aircraft to flight level attitude. 2. Switch electrical power ON. 3. Locate TKS fluid filler tube accessible through ac- cess panel on right side aft fuselage.
Page 279 30-31-00 - STALL WARNING VANE - HEATED The stall warning vane is heated when the optional TKS flight into known icing system is installed on the M20V (See Figure 30- 1). The Stall Warning Vane heat is acti- vated when the Pitot Heat switch is selected ON.
Page 280: Landing Gear
MOONEY INTERNATIONAL CORPORATION M20V SERVICE MAINTENANCE MANUAL CHAPTER 32 LANDING GEAR...
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Page 286 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 32-00-00 - GENERAL actuator unit. The disengage controls are located aft and between front seats. The landing gear is operated by an electrical, motor driven, actuator. Travel during the extend and retract...
Page 287 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 32-10-00 - MAIN LANDING GEAR AND DOORS 12. DO NOT attempt to repair any heat treated com- ponent of main landing gear assembly. 32-10-01 - MAIN GEAR REMOVAL 32-10-02 - MAIN GEAR INSTALLATION 1.
Page 288 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 32-10-03 - MAIN GEAR DOOR RIGGING C. Raise gear electrically to full UP position. D. Forward leading edge and aft trailing edge of 1. Raise aircraft on jacks. See Section 7- 10- 00.
Page 289 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL EXAMPLE: If inboard gear door is closed with landing able to move the Rod by finger pressure or rotation. If gear in DOWN position, but open a small amount with load on the Rod is indicated, or no Bellcrank to Stop landing gear in UP position.
Page 290 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL D. Repeat steps B and C for other side’s landing 3. Retract gear. gear. 4. Pull gear down with emergency extension until E. Continue to Step 4 of Inboard Gear Door Rig- main retract bellcrank and rod end bungee line up.
Page 291 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL a. With Aircraft on jacks, push in the Gear actuator Circuit Breaker. b. Place the landing gear switch in the up position. c. Turn the master switch on. d. Push in the “Red” gear safety bypass switch and hold it into retract the landing gear, then release the switch.
Page 292 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 8. Check nose gear overcenter preload as follows: BUNGEE A. Measure nose gear bungees. (No load) (Fig. 32- 11). B. Extend gear manually (See Section 32-30-07) stopping extension the moment the GREEN Gear Down Light comes ON.
Page 293 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL FUS. STA. 33.0 DETAIL “B” DETAIL “A” 1.56 IN. (APPROX.) LANDING GEAR ACTUATOR ADJUSTMENTS FIGURE 32-12 32-30-02 - MAIN LANDING GEAR SYSTEM RIG- by loosening nut (Y). Disconnect retraction tube (V) GING from bellcrank C (Fig.
Page 294 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 14. PUSH landing gear actuator C/B – IN. 15. Turn MASTER Switch – ON. LEGEND FOR FIGURE 32- 13 16. Extend main gear actuator to fully extended posi- tion. Make certain lugs on main retract bellcrank do not A.
Page 295 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 30. Place 10 inch torque wrench (R) on rigging tool (T) as shown in Figure 32- 1 and apply an unlocking force to retraction truss. 31. When joint at (4) breaks open slightly, insert shim stock (.005 to .008 in.
Page 296 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 7. Push RED GEAR SAFETY BY- PASS SWITCH – -CAUTION- IN and hold IN to partially retract landing gear; release The eccentric bushing, on either or both sides, switch. may be countersunk and have a flush head 8.
Page 297 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 32-30-04 - EMERGENCY GEAR EXTENSION SYS- system to verify that it is fully disengaged by pulling “T” TEM RIGGING handle; no resistance should be felt. If a resistance is felt check cable routing through pulleys (3 & 4) (Fig.
Page 298 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 9. Remove actuator from aircraft. -NOTE- DISASSEMBLY – EATON ACTUATOR When clutch spring is properly seated, large in- 1. Remove two nuts, (1) (Fig. 32- 16) that retain the put gear (6) can be rotated in either direction and...
Page 299 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL properly fit the flats on the input gear shaft to use the 1/4 IMPORTANT – Recheck proper installation of springs. inch drive, 0 to 15 inch lbs., Torque Driver. -NOTE- 12. When correct rotational torque has been ob-...
Page 300 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 4. Pull RED lever back and upward (engaging manu- -CAUTION- al extension system). DO NOT continue to pull T- Handle after 5. Pull “T” handle UP and return to original position; GEAR DOWN light is ON. Actuator may bind continue until GREEN, gear- down indicator light on on Down Stops.
Page 301 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 32-31-00 - TROUBLESHOOTING – LANDING GEAR SYSTEM TROUBLE PROBABLE CAUSE REMEDY Incomplete Retraction. Gear re- Bind in gear retraction system be- Refer to landing gear rigging pro- tracts to an intermediate position cause gear is out of rig.
Page 302 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL SCREW (TYP. 3 PLCS.) GEAR DOOR DUST SHIELD SCREW SPACER MAIN WHEEL COTTER PIN SCREW SPACER MAIN TIRE MAIN GEAR LEG ASSY. NOSE TIRE NOSE GEAR LEG ASSY. COTTER PIN NOSE WHEEL...
Page 303 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 9. Replace bearing cones that show signs of wear or 32-40-03 - NOSE WHEEL DISASSEMBLY/AS- bearing fretting. SEMBLY The standard brand, tube- type, 5:00 x 5, Type III, nose 10. Repack wheel bearings and lubricate seals with wheel tire is six- ply rated.
Page 304 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL NOSE WHEEL ASSY. MAIN WHEEL ASSY. WHEEL ASSEMBLIES FIGURE 32-20 E. Remove pressure plate assembly (Fig. 32- 19) -CAUTION- (5) sliding it off the anchor bolts (6). Note the condition of the anchor bolts. If they are nicked or gouged they...
Page 305: Exhaust
(11) Inspect push rod for scoring, grooves, nicks E. To disassemble master cylinder (Parker- Hanni- and scratches. fin, See Fig. 32- 21) Refer to M20V Illustrated Parts (12) Inspect spring (4) for free height - .500 in. Catalog for Master Cylinder part numbers: Call an +/- .030.
Page 306 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL F. Reinstall master cylinder in reverse sequence of (7) Clean all parts with cleaning solvent. removal. (8) Replace all “O” rings (9). G. Bleed brake system (refer to Section (9) Reassemble brake valve in reverse se- 12- 20- 05).
Page 307 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL gap between 720095-15 arm assy and 720095-17 -NOTE- shaft assembly, record measurement. Check for full left Check nose gear leg assembly for towing dam- travel between rudder and nose gear assembly. age. Replace if any dent exceeds 1/32 inch.
Page 308 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL The gear switch operates the landing gear actuator re- lay. Pulling the wheel- shaped knob out and moving it to the upper detente raises the gear. COLLAR The up- limit switch will stop the gear in its retracted po- sition.
Page 309 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL WARNING DO NOT BE IN POSITION BETWEEN COMPRESSOR TOOL AND FLOOR 030011- 14 PAD WHEN COMPRESSOR TOOL IS IN PLACE IN END OF SHOCK LINK OPERATION. FOR GUIDING SHOCK LINK INTO HOLE IN LEG COMPRESS UNTIL HOLES ALIGN IN SHOCK LINK &...
Page 310 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 32-82-00 - RECOMMENDED HARD LANDING IN- -NOTE- SPECTIONS Dimension (T), (Fig. 32- 28), is critical to properly The following are areas recommended to be inspected locate nose wheel position. Leg assemblies can when a “hard landing”...
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Page 316 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 33 LIGHTS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 33- 00- 00 ......General - Description and Operation ....5 33- 10- 00 .
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Page 318 High intensity strobe lights are standard equipment on and is controlled by momentary switches (magnet) M20V aircraft. The lights are located adjacent to the mounted in both cabin door frames. The switch is ener- wing tip navigation lights and incorporated in the rudder gized when any door is opened.
Page 319 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL BAGGAGE COMPARTMENT LIGHT EXTERIOR LIGHTS O/H SWITCH PANEL SONALERTS (UNDER COVER) FRONT SEAT PASSENGER LIGHTS FRONT AIRCRAFT INVERTER (MOUNTED READING LIGHT REAR SEAT SWITCH SPEAKERS ON BACKSIDE PASSENGER LIGHTS FRONT SEAT (UNDER COVER)
Page 320 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 4. Re- install headliner panel; secure with two (2) BAGGAGE COMPARTMENT SWITCH screws. 1. Switch is located at rear of baggage door at front, top of hat rack opening. (Figure 33- 1) 2.
Page 321 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 33-23-00 - GEAR DOWN INDICATOR LIGHT assembly. (FLOORBOARD) 2. Remove and replace bulb. 33-23-01 - LIGHT BULB REPLACEMENT 3. Check for proper operation. 1. Remove lower belly panel to gain access to light 4.
Page 322 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL LANDING LIGHTS, NAVIGATION LIGHTS AND TAILLIGHT Lamp burned out. Replace lamp. Lamp fails to light. Loose connection or Tighten connections and check wire defective wire. circuit continuity. Replace or repair wire if necessary.
Page 323 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 33-41-02 - POWER SUPPLY(IES) UNIT INSTALLA- cap head screw and tighten firmly. Confirm proper gas- TION ket fit. F. When necessary, waterproof the light base to air- The installation of power supply(ies) is reverse se- craft.
Page 324 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 2. Place four target crosses (+) on vertical wall at the following positions: A. Measure 36.5 inches UP on vertical wall from same ground plane aircraft is resting on. B. At 9.85 feet, left and right, of nose wheel center line.
Page 325 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL -NOTE- When handling the optional xenon bulbs (Ref. Fig. 33- 7), wear clean cotton or latex gloves. Af- ter installation of the bulb(s), gently wipe bulb with a small amount of isopropyl alcohol to re- move any residual oil from your hands or other maintenance processes.
Page 326 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 34 NAVIGATION AND PITOT STATIC...
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Page 330 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 34 NAVIGATION AND PITOT STATIC TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 34- 00- 00 ......General ..........5 34- 10- 00 .
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Page 332 The Mid- Continent model MD302 series Standby Atti- tude Module (known as the SAM) is a self- contained M20V aircraft are equipped with a GARMIN G1000 In- situational awareness instrument that provides aircraft tegrated Avionics System utilizing two Garmin 10XX...
Page 333 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 34-10-00 - PITOT & STATIC AIR PRESSURE SYS- -CAUTION- Release air pressure slowly by unrolling rub- Static pressure instruments are extremely sensitive to ber tubing. A sudden release of the air pres- pressure changes;...
Page 334 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL The airspeed tape is a vertical scale along the left mar- Refer to Garmin G1000 Line Maintenance and Config- uration Manual for service and troubleshooting infor- gin of the display. The current airspeed is always in the mation.
Page 335 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL The altitude window displays the current, barometric adjusted altitude. The indicated digits of the display are ALTITUDE BAROMETER TAPE/SCALE VALUE every ten (10) units and the window is expanded over this portion of the number to display a minimum of (20) ALTITUDE units.
Page 336 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 34-20-00 - G1000 HORIZONTAL SITUATION ment is provided to prevent overly sensitive response INDICATOR (HSI) and comply with regulatory requirements. The G1000 Horizontal Situation Indicator (HSI) dis- The slip indicator background becomes semi- trans-...
Page 337 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 30 is found at any cardinal heading, proceed to G. Again, hold compass in place and compare demagnetize cockpit as outlined in Step 3. If error is headings. If heading error has not reduced sufficiently less than ...
Page 338 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Liquid leakage. Loose bezel screws. Tighten screws. Broken cover glass. Replace instrument. Defective sealing gaskets. Replace instrument. Discolored luminous markings or Replace instrument. discolored damping liquid. Defective light. Burnt out lamp or broken circuit.
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Page 344 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 35 OXYGEN TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 35- 00- 00 ......General Precise Flight Oxygen System ....5 35- 00- 01 .
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Page 346 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 35-00-00 - GENERAL 5. A center console panel display and System actua- tion switch -WARNING- 6. An overhead distribution manifold with low pres- Proper safety measures must be employed sure transducer and integrated interior LED dome light...
Page 347 The Fixed Oxygen System consists of a few simple tion signal to drive the latching solenoid. components for supplying sufficient oxygen to the crew and passengers for the Mooney M20V aircraft (see Fig- Breathing Equipment ure 35- 3). These components follow: 1.
Page 348 Maintain aircraft structure and wiring in accordance The filler port requires cleaning periodically, and prior to with Mooney electrical schematics and FAA AC43.13. filling, to keep clean of dirt, dust, and oils to prevent fire. 35-00-03 - PRECISE FLIGHT BOTTLE REMOVAL...
Page 349 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL k. Purge the line of AK- 225 by passing clean dry air 3. Switch the Oxygen System ON at the oxygen con- through the line. trol panel and verify that the Oxygen System quantity display indicates the same oxygen pressure shown at l.
Page 350 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL RH FUSELAGE PANEL OXYGEN FILLER VALVE PURITAN BENNETT CONNECTION OXYGEN TANK OXYGEN FILLER DOOR PRECISE FLIGHT OXYGEN SYSTEM - FILL VALVE FIGURE 35-6 MOUNTING HARDWARE GROUND STRAP AND HARDWARE BAND CLAMP TAILCONE ASSY...
Page 351 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Oxygen System Bleed- Down (Purging) Use the following procedure to bleed- down the oxygen system should any of the hard lines, nonconductive line be opened, or bottle removed and re- installed/re- placed. This procedure is required to prevent contami- nation, or moisture inside the system.
Page 352 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Ground Test (Method B) Method B for checking the calibration is by ground test. The ground test requires the removal of copilots side Center Console Trim Panel to gain access to the Dis- play Logic it Controller (DLA).
Page 353 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL b. If the indication is outside of this range, re- verify -CAUTION- the indication. If the DLA fails a second time, remove the DLA and replace, or contact PFI for re- adjustment.
Page 354 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Installation Complete, Purging and Leak Check Complete. System Fully Charged for Service Turn ON Aircraft Power Cycle Aircraft Power or Cycle Oxygen System Re-Fill Oxygen Turn ON Oxygen System to Over 1500...
Page 355 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Steady Check that Each Cycle Aircraft Solenoid Wire Solenoid Wire to Fault Light Power or Oxygen to Ground OK? Ground is Repeatable? System CB and 11.3 VDC Reset Check System Voltage to the DLA is >14.6VDC...
Page 356 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Check that Each Solenoid Wire to Solenoid Wire to Ground OK? Ground is >11.3 VDC Solenoid Failure Remove and Replace the Regulator Bottle Assembly Purge the Oxygen System per Section 2.4.6 Mart Regulator/...
Page 357 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Fix Wiring * - Voltage measured at the low pressure transducer between the Check Low connector with the Transducer Connected Display-Logic- Pressure PIN 1 - Supply (8-12 VDC) Wiring OK? Assembly and the...
Page 358 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL PRECISE FLIGHT OXYGEN SYSTEM - WIRING SCHEMATIC (TYPICAL) FIGURE 35-18 35-00-04 Page 17 MAR 2017 Date Rev Date...
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Page 364 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 37 VACUUM TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 37- 00- 00 ......General ..........5...
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Page 366 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 37-00-00 - GENERAL Garmin G1000 equipped aircraft are all electric with no vacuum system requirements on the standard aircraft. 37-00-00 Page 5 MAR 2017 Rev Date Date...
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Page 368 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 39 ELECTRICAL PANELS...
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Page 372 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 39 ELECTRICAL PANELS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 39- 00- 00 ..General ..............6 39- 00- 00 .
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Page 374 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL GARMIN 1000 INSTRUMENTS AND CONTROL PANEL (TYP.) FIGURE 39-1 39-00-00 Page 5 MAR 2017 Rev Date Date...
Page 375 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 39-00-00 - GENERAL See Chapter 91 for Electrical System Hardware Identi- fication Charts and Schematics. The G1000 Integrated Avionics System (Figure 39- 1 & 39-10-00 - INSTRUMENT AND CONTROL Figure 39- 2) is a fully integrated flight, engine, commu-...
Page 376 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL timeter consists of four parts; Altitude Window, 12. STROBE LIGHT SWITCH Altitude Tape, Barometric Setting Window and Strobe light switch turns wing tip and tail strobe optional Altitude Trend Bar. lights ON.
Page 377 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 19. RUDDER TRIM SWITCH -CAUTION- Spring loaded momentary switch to position rud- Pushing LOW BOOST pump switch ON der into trimmed condition to reduce rudder pedal when engine is operating properly at idle forces during take off, climbs or descents.
Page 378 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ward to enrich mixture. Pull control full aft to close ducts in the front of glareshield area. Optimum idle cut off, shutting down engine. Control is a use of the defrost control is described in the Cab- vernier type and fine adjustments of mixture can in Environment Section.
Page 379 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 48. PILOT, CO- PILOT’S HEADSET JACKS, MIC B. Refer to the Garmin Installation and Mainte- JACK (Hand Held Microphone) and USB nance Instructions for each Garmin component to be removed/installed. PORT (If installed) (NOT SHOWN) Plug hand held microphone jack into this plug C.
Page 380 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL RACK, AUXILIARY, AVIONICS EQUIPMENT GRS 77 BECKER ADF (IF EQIUPPED) GTX 33 GDU 10(XX) PFD GIA 63 #1 GIA 63 #2 GDL 69A TAILCONE AREA GEA HARNESS PITCH SERVO PITCH TRIM SERVO...
Page 381 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 39-10-02 - CIRCUIT BREAKER PANEL Turn master switch - OFF. The Circuit Breaker Panel (Figure. 39- 3) is an assem- 1. To Remove (Figure. 39- 4) bly that can be removed for increased access to com- A.
Page 382 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL C/B (EL) PANEL RACK ASSEMBLY MAIN CONNECTOR ASSEMBLY UPPER SCREW (1) MAIN CONNECTOR ASSEMBLY TRAY ASSEMBLY SCREW (x2) WASHER (x2) SPACER (x2) C/B (EL) PANEL LOWER SCREW (1) CIRCUIT BREAKER PANEL REMOVAL FIGURE 39-4 3.
Page 383 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL and through left or right grip of Control Wheel. Solder Master Switch, which control most systems of aircraft. connections at switch terminals, where applicable, Refer to Figures 39- 1. should be covered with heat shrink tubing.
Page 384 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL -CAUTION- Activation of gear safety override switch while aircraft is on ground may cause landing gear to retract. 1. Disconnect wire connector (Figure 39- 9), approxi- mately 10 inches from switch. 2. Loosen nut on stem and hold nut located inside mounting bracket.
Page 385 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL must be in place for the “G” switch to activate the unit. Transmitter Test The jumper is installed on the mating half of the connec- Always perform the tests within the first 5 minutes of the tor so that when the connector is installed, the beacon hour.
Page 386 SCREWS Maintenance and Troubleshooting information. 39-20-00 - ELECTRICAL/ELECTRONIC EQUIP- MENT RACK The electrical equipment rack for the M20V aircraft is BATTERY REPLACEMENT (ELT - ARTEX ME- 406) located in tailcone just aft of baggage compartment FIGURE 39-13 bulkhead. Access is gained through large access door NOTE: in tailcone aft of left wing trailing edge.
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Page 392 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 51 STRUCTURES TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 51-00-00 ......General ..........5 51-10-00 .
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Page 394 The vertical stabilizer is constructed around a fabri- cated main spar assembly with ribs connecting main The Mooney M20V is an all metal, low wing airplane. and rear spar. A stretch formed, aluminum skin wraps The fuselage cabin area is constructed of welded 4130 around leading edge ribs and is riveted to rear spar on chrome- molybdenum steel tube.
Page 395 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL recommendations when the preceding instructions are Huckbolt collar. The combined thickness of any two inadequate to accomplish repair. washers shall not exceed .098 inch. Huckbolts or coni- cal Keystone Lock blind rivet heads may be cocked no To compensate for material thickness tolerances, more than .004 inch.
Page 396 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL B. REPLACEMENT- STANDARD SIZE RIVETS, of the next standard size larger diameter rivet, it will be HOLE AND COUNTERSINK OR DIMPLE OVERSIZE. permissible to rework the smaller countersink or dimple This repair applies only to original countersunk head...
Page 397 MIL- F- 5632- A, class 2, or AWS A5.18- 69, placement can be purchased from one of our Author- class E705- 2 are recommended for inert- gas, ized Mooney Service Centers. Visit our ’Support’ sec- shielded- arc welding (Heliarc). Use AISI 4130 condi- tion of our website www.mooney.com.
Page 398 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 1/2A SLEEVE ORIGINAL 1/2A REPAIR TUBE ROSETTE WELD TUBE REPLACEMENT INSIDE TUBE LEAVE 1/8 IN. GAP FOR WELDING ROSETTE WELD SLEEVE REPAIR TUBE 1/2A 1/2A INSIDE INNER SLEEVE SPLICING FIGURE 51- 6 WELD HERE FIRST 1/4 IN.
Page 399 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 4. TENSION FITTING REPLACEMENT (Figure A. Small holes up to a #20 drill may be closed by 51- 8). welding with the inert gas, shielded arc method. A. Cut tubes (A) and (B) loose from tension fitting B.
Page 400 FIGURE 51- 9 3. NONSTRUCTURAL SKIN REPAIR. The skin cov- parts, check control system travel and rigging as out- ering the M20V aircraft tubular fuselage structure is lined in Chapter 27. Before returning aircraft to service, considered nonstructural. Patches in nonstructural flight test aircraft for proper control system rigging.
Page 401 If huckbolt is too long, the huck collar will not lined in AC 43.13- ( ), consult Mooney International swage properly; if the huckbolt is too short, the shank Corporation, Product Support Department personnel will not completely fill hole.
Page 402 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL SPLICE ANGLE MATERIAL: 7075- T6 .875 .160 (4 MIN. EACH SIDE) .130 .688 .813 ALPPH- TP (4 MIN. EACH SIDE) VIEW LOOKING UP VIEW LOOKING DOWN SPAR CAP REPAIR FIGURE 51- 11 51-13-03 - STUB SPAR REPAIR (Stub spar splice at wing STA 34.5 +/- 3.0)
Page 403 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL - 505 PLATE (REF) 210054- 7 1.66 WEB (REF) 1.07 - 501 (REF) - 507 20.0 - 501 FLAT PATTERN (.091 AISI C 130, COND. ”N” STEEL) 210055 CAP (REF) SECT B- B...
Page 404 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 51-13-04 - REAR SPAR REPAIR 51-13-07 - WING SKIN PANEL REPAIR The rear spar may be spliced between ribs in accor- Repair wing skin panels as prescribed in AC 43.13- ( ), dance with AC 43.13- ( ) (Figure 51- 14).
Page 405 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 5.40 26 EQUALLY SPACED 32 EQUALLY SPACED .25 TYPICAL .25 TYPICAL RIVETS RIVETS ACCESS COVER REPAIR FIGURE 51- 16 ings with two- diameter edge distances in a circular pat- tern around cracked dimple.
Page 406 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL C. Countersink dimple hole in skin allowing coun- skin, and 22 AD4 rivets through splice angle and spar tersink to extend into substructure. web. D. Install conical washer, use next oversize rivet .070...
Page 407 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (4 MIN. PER SIDE) .040 (3 MIN. PER SIDE) .040 CR 2248 CHERRY LOCK (4 MIN. PER SIDE) .040 2024T- 3 CLAD SPAR REPAIR (STA. 48.5 APPROX.) FIGURE 51- 21 (10 EACH SIDE OF CRACK)
Page 408 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 51-15-00 - FIBERGLASS LAMINATES, REPAIR 2. Remove any loose particles and frayed fiberglass PROCEDURES strands from the cracked portion. 3. Prepare surface for repair as shown in Figure Despite the fact that fiberglass laminates are designed 51- 27, Figure 51- 28, and Figure 51- 29.
Page 409 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 2. Remove damaged areas. repair area. If necessary, attach the patch tool in place using clamps, tape, or temporary rivets. A. Cut back to 1” beyond visible damage, taking 8. Mix the resin according to the manufacturer’s data...
Page 410 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL panel shape, then the repair to the panel will have to 7. Apply one additional overlapping layer of #181 fi- proceed in stages. berglass cloth on non- finished surface and bond in place.
Page 411 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL #181 FIBERGLASS CLOTH .025 T- 3 ALUM. (SEE SECTION .375” 2.0” 51- 15- 03, 2) LAMINATE .03” CRACK .025 T- 3 ALUM. 2.75” (SEE SECTION 51- 15- 03, 2) #181 FIBERGLASS CLOTH OVERLAP (1) LAYER FIBERGLASS ALUM.
Page 412 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL STOP DRILL 0.5” CRACK CHAMFERED SURFACE & GLASS PATCH OUTLINE 1.5” 1.5” NON- FINISHED SURFACE CRACK LAMINATE THICKNESS FINISHED SURFACE CHAMFER EACH SIDE (TYP.) THICKNESS .02 TO .04 0.50 0.50 (FIBERGLASS- RESIN COMBINATION)
Page 413 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 2. Low Pressure, Plastic, or Rubber Line Splices. 3. Shortening and Lengthening of Tubing, Hoses, Static system lines may be lengthened, shortened, or and Flexible Ducting. Mooney manufactured assem- spliced to allow the replacement of sections of dam- blies of plumbing, tubing, hoses, and flexible ducting aged lines.
Page 414 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 52 DOORS...
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Page 418 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 52 DOORS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 52- 00- 00 ......General ..........5 52- 10- 00 .
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Page 420 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 52- 00- 00 - GENERAL inner and outer heat treated, aluminum shell, fastened together by rivets. It has dual pin latches that extend Both cabin doors are constructed of an inner and outer...
Page 421 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL LATCH JAWS SLIDE CAM MOUNTING SCREWS ADJUSTMENT ANCHOR POINT PLATE LATCH REF: MOUNTING INNER DOOR BOLTS CONTROL SHELL CABLE BRACKET REF: OUTER DOOR SHELL ILLUSTRATION SHOWS BOTH HALVES APART FOR CLARITY DOOR HINGES...
Page 422 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 52-10-01 - CABIN DOOR(S) REMOVAL 52-10-04 - CABIN DOOR(S) LATCHING MECHANISM NEW DOORS - A new door will require proper posi- REMOVAL: tioning and trimming to obtain proper sealing. A new door bulb seal will need to be installed to help door A.
Page 423 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL INSTALLATION: 52-10-05 - CABIN DOOR RIGGING/ADJUSTMENT PROCEDURES A. If not installed, locate and bond actuator magnet approximately 1.5”  .5” from upper door latch opening The cabin door latching mechanism has several adjust-...
Page 424 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 52- 30- 00 - BAGGAGE COMPARTMENT DOOR - -NOTE- MAINTENANCE PRACTICES Hinge mounting area should be clean of old 1. Removal. sealant and debris. The baggage compartment door may be removed to B.
Page 425 BAGGAGE DOOR LATCH MECHANISM FIGURE 52- 5 52- 60- 00 - ENTRANCE STEPS There two type of entrance steps installed on the M20V aircraft. One type is a fixed step which is permanently attached, and the other is an (optional) removeable type that can be removed and stowed.
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Page 432 53-00-00 - GENERAL fixture and assembled into the aft fuselage assembly. All air ducts, control brackets, tubes and bellcranks, The Mooney M20V forward fuselage is constructed electrical harnesses and antennas are installed into from 4130 chrome molybdenum, tubular steel covered tailcone during this assembly process.
Page 433 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL STRIKER STRIKER PLATE PLATE (LOWER LH SHOWN) (LH SHOWN) VIEW LOOKING LH SIDE COMPOSITE SHELL FIGURE 53- 2 53-20-00 - PLATES/SKINS The fuselage assembly and tailcone have panels, cov- ers or doors at various locations to provide access to The fuselage tubular structure is covered with a com- interior for inspection or maintenance purposes.
Page 434 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 6, 6A 1. CABIN DOORS 2. ENGINE COMPARTMENT 3. BAGGAGE DOOR 4. ELEVATOR/RUDDER CONTROL STOPS 5. EMPENNAGE ATTACHMENT 16, 17, 18 6. AVIONICS BLACK BOXES, BATTERY, ELT ACCESS 6A. BATTERY ACCESS 7. STABILIZER TRIM JACK SCREW 8.
Page 435 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 53-30-00 - FIREWALL The forward cabin structure (1) is bolted to tailcone with eight structural bolts (8). The tailcone skin (2) is an inte- The firewall is .016 stainless steel (Figure 53- 4), at- gral load bearing portion of tailcone assembly.
Page 436 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 53-50-00 - ATTACH FITTINGS using structural hardware; (Figure 53- 5). Various types of fittings are used to properly distribute load between 53-50-01 - WING ATTACH FITTINGS wing and fuselage. The wing assembly is attached to fuselage assembly...
Page 437 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 53-50-02 - EMPENNAGE ATTACH FITTINGS two top hinges. The bottom attach point on empennage assembly secures stabilizer trim jack screw. Lateral The empennage assembly is manufactured as a unit, stability of empennage assembly is controlled with an...
Page 438 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL HINGE PIN NOTE: THERE ARE SMALL SHIMS, THESE MUST GO BACK IN THE SAME WAY UPON ASSEMBLY BOLT BOLT WASHER WASHER BUSHING SAFETY WIRE COTTER PIN AS REQUIRED BOTH PLACES TRIM LINK...
Page 439 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 53-50-03 - ENGINE MOUNT ATTACH POINTS and are used in conjunction w/ attachment of nose landing gear lower truss assembly (Figure 53- 8). AN6 The engine mount is attached to hard points built into bolts are installed at this location.
Page 440 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 55 STABILIZERS...
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Page 446 55-00-00 - GENERAL horizontal stabilizer has a stub spar that spans a por- tion of stabilizer. The model M20V empennage assembly is a variable incidence tail- plane consisting of a horizontal and ver- The elevator and rudder are constructed from an ex-...
Page 447 55-20-01 - ELEVATOR - REMOVAL Remove AN3 bolts from each control horn and push- Elevators on the model M20V consist of left and right pull tube bearing, then remove AN3 bolts and hardware hand assemblies attached, through ball bearing fittings from each hinge fitting on both elevators.
Page 448 Skins (10) are stretch- formed in 2 sections and riveted 55-40-00 - RUDDER to ribs and spar. The rudder on the model M20V is of similar construc- The rudder attach fittings (11) are mounted to rear spar tion as the elevator with stamped- formed skins (1) extrusion to attach rudder (12).
Page 449 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL DETAIL A DETAIL B RUDDER ASSEMBLY FIGURE 55- 4 55-40-02 Page 8 MAR 2017 Date Rev Date...
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Page 454 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE CHAPTER 56 WINDOWS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 56-00-00 ......General ..........5 56-00-01 .
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Page 456 If after removing dirt and grease no great The windshield for the model M20V is .188 inch thick amount of scratching is visible, finish the plastic with a acrylic, heat formed to contour. The LH/RH cabin doors good grade of commercial wax.
Page 457 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE ed along the perimeter of the windshield, in between -CAUTION- the windshield and the composite shell, by gently tap- ping on the wedge with a plastic hammer. (See Figure Exercise care during this operation to avoid 56-3) scratching acrylic.
Page 458 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE S Other panel hardware as required, to loosen panels enough to access windshield (along top and front of PUSH FROM door frame) INSIDE 2. Clean Mating Surfaces -NOTE- DO NOT USE CHEMICALS OR SOLVENTS. Dam-...
Page 459 CARBON FIBER RODS ATTACH CARBON FIBER RODS FIGURE 56-6 b. Apply 70-03A elastic bonding adhesive/sealant (reference Mooney Spec. 20, Section XII) with a INSTALL WINDSHIELD sealant gun around the inside rim of the windshield. FIGURE 56-8 c. Smooth the line of sealant with a wooden tongue depressor.
Page 460 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE j. Let the sealant dry according to the application directions on the sealant tube. SECURE WINDSHIELD WITH STRAPS, TAPE, ETC. k. Remove the metal spacers. l. Apply a second coat of sealant with a sealant gun around the rim of the windshield.
Page 461 Apply a thick, uniform thickness of CS3204-B2 (B), or 56- 50- 00 - ACRYLIC DRILLING equivalent sealant (reference Mooney Spec. 20, Sec- tion XII), to both window and skin areas where window Drill bits for acrylic should be ground per Figure 56- 12.
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Page 467 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 57 WINGS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 57- 00- 00 ......General ..........5 57- 00- 01 .
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Page 469 M20V SERVICE AND MAINTENANCE MANUAL 57-00-00 - GENERAL (i) Belly skin stringer splice angles. The M20V all metal wing is a one piece assembly at- (j) Airspeed indicator line, pitot lines and pitot tached to the fuselage at structural hard points with heater wires (if installed).
Page 470 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL AN4- 17A BOLT (1) TUBULAR STRUCTURE (REF.) NAS1149F0463P WASHER (2 QTY ON HEAD) NAS1149F0432P WASHER AN4- 20A BOLT (1) (NOTE WASHERS ON DISASSEMBLY) NAS1149F0463P WASHER (2 QTY ON HEAD) MS21045L4 NUT NAS1149F0432P WASHER...
Page 471 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL SHIM/HARDWARE TABLE SHIM DASH NO. BOLT WASHER NO. WASH- WASHER NO. NUTS BOLTS ERS REQD. REQD. PER (ADDITIONAL) PER SHIM PER SHIM SHIM 310136- 7 AN4- 5A AN960- 416 AN960- 416L AN363- 428...
Page 472 FIGURE 57-3 57-20-02 - WING TIPS NAVIGATION/STROBE LIGHT ASSY. The M20V wing tips are non- structural, fiberglass com- ponents. They are riveted to upper and lower wing skins during final assembly of wing structure (Figure 57- 4). 1. Wing tip removal.
Page 473 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL B. Secure wing tip and drill holes to match existing The wing access and inspection covers shown in (Fig- wing skins. Use clecoes as holes are drilled into new ure 57- 5) provide maintenance access to components, tip.
Page 474: Time Limits/Maintenance Checks
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 57-40-00 - ATTACH FITTINGS Grease fittings (8) are installed at pivot points of main landing gear assembly for lubrication per Chapter 5. Refer to Section 57-00-01 for wing fuselage attach- ment. The steerable nose gear mounts to the cabin tubular steel frame.
Page 475 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL COTTER PIN LOCKNUT FLATWASHER FLATWASHER BOLT FLATWASHER DETAIL C LOCKNUT FLATWASHER FLATWASHER DETAIL D BOLT 4 PLACES FLAP ASSEMBLY FIGURE 57-7 57-50-21 - AILERON REMOVAL AND INSTALLATION Refer to Section 27-10-00 for removal, installation &...
Page 476 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL WASHER (SEE NOTE 1) WASHER COTTER PIN BOLT WASHER FAIRING BOLT SCREW WASHER WASHER (SEE NOTE 1) WASHER BOLT DETAIL A WASHER WASHER NAS70CL261-500 DETAIL B DETAIL C NOTE: COUNTERSINK TOWARDS HEAD OF BOLT...
Page 477 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 61 PROPELLERS...
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Page 481: General
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 61 PROPELLERS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 61- 00- 00 ......General ..........5 61- 00- 10 .
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Page 483 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 61-00-00 - GENERAL 2400 hours. Refer to Hartzell Propeller Owner’s Manu- al 115N (provided with each propeller) for mainte- The Hartzell propeller is a constant speed, non- coun- nance, inspection procedures and time intervals.
Page 484 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 1. Cut and remove the safety wire (if installed) on the HARTZELL 3 BLADE PROPELLER INDEXING propeller mounting studs. FIGURE 61- 2 The propeller flange has six 1/2 inch studs configured in -WARNING- a four inch circle (Figure 61- 2).
Page 485 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 7. Install the propeller spinner dome in accordance CAUTION with Spinner Installation. Mounting hardware must be clean and dry to prevent excessive preload of the mounting SPINNER INSTALLATION flange. -CAUTION- CAUTION All torques listed are dry torque.
Page 486 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL tended after evaluation of previous propeller overhauls -CAUTION- with regard to bearing wear and internal corrosion. Grease must be applied to all blades of a pro- -NOTE- peller assembly at the time of lubrication.
Page 487 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL To determine amount of rework needed, use the following formula: On the leading and trailing edge of the blade, measure the depth of the damage, and multiply this number x 10 (see Example 2, above). Rework the area surrounding the damage 10 times the depth of the damage.
Page 488 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 61-20-90 - PROPELLER TROUBLESHOOTING (Refer to Hartzell Owner’s Manual 115N for detailed Troubleshooting Instructions) TROUBLE SYMPTOM POSSIBLE CAUSE/REMEDY Hunting and Surging: Hunting is characterized by a cyclic Licensed repair facility should check:...
Page 489 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL TROUBLE SYMPTOM POSSIBLE CAUSE/REMEDY Loss of Propeller Control: Propeller goes to Uncommanded 1 - Governor pressure relief valve Low Pitch (High RPM). for proper operation. 2 - Governor drive for damage. 3 - Adequate engine oil supply.
Page 490 Propeller Balancing Equipment, therefore details of The propeller/spinner combination assembly is dynam- proper operation and procedures should be taken from ically balanced at Mooney Aircraft Company, Inc. Any manuals of the specific manufacturer for equipment be- maintenance action to be accomplished on any compo- ing used.
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Page 497 71-00-00 - GENERAL 5. Remove propeller (refer to section 61-00-10). 6. Drain engine oil sump. The M20V aircraft has a Continental Motors Incorpor- ated (CMI) TSIO- 550- G( ) series engine installed. This 7. Disconnect the following: is a six cylinder, 280 H.P., fuel injected, twin turbo- A.
Page 498 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CROSSOVER PIPE ASSY. WASTEGATE OIL INLET LINE WASTEGATE ASSEMBLY FORWARD SLIP JOINT TAILPIPE TAILPIPE V- BAND CLAMP CONNECTION WASTEGATE TO BREATHER TAILPIPE TUBING ATTACHMENT ENGINE LEFT SIDE FIGURE 71- 2 From engine right side (Fig. 71- 1): gate to the engine to protect it from damage during en- gine removal.
Page 499 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL From engine right side (Fig. 71- 1): 5. Oil sump is filled to eight quarts. 6. Spark plugs are tight and ignition harness is prop- 1. Install crossover pipe. Leave crossover pipe stabi- erly installed.
Page 500 It is recommended that the TSIO- 550- G( ) engine down engine and troubleshoot oil system. Refer to CMI installed on the Mooney M20V aircraft be set up ac- maintenance publications for procedures. cording to the following instructions and in conjunction I.
Page 501 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL H. Connect the Porta-Test Manifold Pressure and H. Torque all connections according to Appendix B Upper Deck Pressure hose to the engine according to specifications of the CMI TSIO-550 Service and Main- the Porta-Test instructions.
Page 502 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL A. Operate engine at 1500 to 1800 RPM until CHT -NOTE- instrument indicator is GREEN BAND and oil tempera- ture is 160 to 180 F. The Best Power setting will develop the maximum horsepower and speed for a particular B.
Page 503 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL (HIGH) FUEL PRESSURE ADJUSTMENT INCREASE SLOPE (LOW) UNMETERED CONTROL FUEL PRESSURE ADJUSTMENT ADJUSTMENT INCREASE INCREASE IDLE MIXTURE ADJUSTMENT IDLE SPEED ADJUSTMENT ENRICHEN MIXTURE INCREASE ENGINE SET- UP AND ADJUSTMENT POINTS FIGURE 71- 3...
Page 504 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL METERED FUEL PRESSURE UMTD UNMETERED FUEL PRESSURE UPPER DECK PRESSURE UMTD UNMETERED FUEL PRESSURE METERED FUEL PRESSURE UPPER DECK PRESSURE ENGINE SET- UP AND ADJUSTMENT POINTS FIGURE 71- 3 71-00-51 Page 12...
Page 505 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 71-00-52 - ENGINE SET- UP - CONTROL RIG- 71-00-60 - FUEL INJECTION SYSTEM MAINTE- GING NANCE For specific injection system inspection and overhaul Check all fuel lines, reference lines, gauge lines and...
Page 506 71-20-00 - ENGINE MOUNTS Start at right rear (RR), then left rear (LR), left front (LF), and right front (RF). The M20V engine mount is a welded, bed type, dyna- focal mount assembly constructed of 4130 -NOTE- chrome- moly steel tubing.
Page 507 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 590052- 517 590052- 515 NAS-6607-48 NAS-6607-48 BOLT 600532-1 BOLT 600532-1 HEAT SHIELD HEAT SHIELD J-9613-76 J-9613-76 600364-7 600364-7 WASHER WASHER J-9612-44 J-9612-44 LORD MOUNT LORD MOUNT J-9612-43 Y-16440-2-497 LORD MOUNT Y-16440-2-497 SPACER...
Page 508 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ISOLATOR MOUNT SEATED REMOVE - "DUMMY" BOLTS TIGHTEN "DUMMY" BOLTS (NAS6607-15 OR EQUIVALENT) TO COMPRESS RUBBER MOUNTS APPLY LUBE TO MOUNTS SCREWDRIVER OR PRY BAR ENGINE MOUNT REPAIR FIGURE 71- 6 71-30-00 - FIRESEALS Normal engine operating temperatures are at optimum to facilitate engine efficiency.
Page 509 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL operated in extreme dusty conditions. Air filter assem- into the length of each pleat. It may be necessary to ap- bly must be replaced after 25 cleanings or sooner if any ply oil on filter material that has not received oil from the deterioration or damage is found during pre- flight, post wicking action.
Page 510 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ANNNCIATOR MEASURE OUTBOARD LIGHT ANNNCIATOR 4.5 TO 7.5 LBS. SWITCH LIGHT TO OPEN DOOR (REF.) SWITCH HERE (REF.) (APPROX.) REQD. TO ALLOW FOR MAX. TRAVEL GAP REQD. OF LEVER ASSY BETWEEN ACTUATOR ROD &...
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Page 515 MOONEY AVIATION COMPANY, INC. M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 72 ENGINE TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 72- 00- 00 ......General ..........5...
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Page 517 Refer to Continental Motors Incorporated (CMI), TSIO- 550- G( ) engine Maintenance and Overhaul Manual M- 18 and Installation and Operation Manual OI- 18 for detailed information on the TSIO- 550- G( ) engine installed in the Mooney M20V. 72-00-00 Page 5 MAR 2017...
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Page 519 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 73 ENGINE FUEL SYSTEMS...
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Page 525 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 73-00-00 - GENERAL cate. Refer to Continental Motors Incorporated (CMI) Maintenance & Operators Manual or Overhaul Manual The engine and its accessories are certificated under for specific instructions. Continental Motors Incorporated (CMI) Type Certifi-...
Page 526 A turbine type fuel flow transducer and signal compat- I. Locate and disconnect fuel lines attached to ible, interpretive indicators are installed on the M20V adapter fitting and elbow on the inlet and outlet ports of aircraft. the fuel flow transducer. Note position (orientation) of...
Page 527 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL I. When all adjustments have been made and all -WARNING- connections checked for security, install cowling per Allow no smoking or open flames within 50 Section 71- 10- feet of the engine compartment area during fuel 73-40-00 - FUEL INJECTOR - GENERAL leak testing.
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Page 535 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 74-00-00 - GENERAL BOTH to START position; push forward on key while in START and starter relay is energized. Release of key, The Continental Motors TSIO- 550- G ( ) series en-...
Page 536 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ENGINE FIRING ORDER UPPER UPPER SPARK PLUGS SPARK PLUGS MAGNETO FIRING ORDER RIGHT MAG LEFT MAG IGNITION WIRING DIAGRAM FIGURE 74- 1 magneto cases, spark plugs, cables and connections -NOTE- are shielded to prevent radio interference.
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Page 543 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 76-00-00 - GENERAL 3. Loosen hardware from attaching clamps. Remove clamps. Loosen hardware attaching cable assembly to 76-10-00 - ENGINE CONTROLS RIGGING throttle switch bracket. See SECTION 71- 00- 52 for Engine Controls Rigging/ 4.
Page 544 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL ENGINE THROTTLE MIXTURE BODY CONTROL PROPELLER CONTROL HOUSING NUT (TYP) GROMMET (TYP) THROTTLE CONTROL BULKHEAD FITTING, LOCKWASHER & NUT (TYP) CLAMP THROTTLE ALTERNATE SWITCH/ BRACKET CONTROL (REF.) HEIM ROD END BEARING ALTERNATE DUCT (REF.)
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Page 551 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 77-00-00 - GENERAL For Operation, Maintenance and Troubleshooting, re- fer to Garmin publications. Engine indicating instruments and their sending units, 77-20-02 - CYLINDER HEAD TEMPERATURE transducers, probes, etc., must be operating properly to prevent engine damage.The G1000 displays the in-...
Page 552 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL For Operation, Maintenance and Troubleshooting, re- A. RED - 0 to 10 PSI (Idle) fer to Garmin publications. B. YELLOW - Caution 10 to 30 PSI C. GREEN - Normal 30 to 100 PSI 77-30-00 - PRESSURE INDICATING D.
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Page 559 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 78-00-00 - GENERAL Garmin G1000 equipped M20V aircraft utilize six cylin- der EGT probes and one system TIT probe to monitor The exhaust system’s headers, turbochargers and ex- exhaust gas temperatures. Refer to Probe manufac- haust pipes are manufactured by Continental Motors turer’s service literature for recommended mainten-...
Page 560 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL C. INTERNAL EROSION - Examine bends and Do not reuse gaskets. low spots for thinning or pitting. Insure that attach bolts are properly torqued. Exhaust D. STANDOFFS (PINS) AND HEAT TRANSFER flange stud nuts are to be torqued to 100- 110 inch lbs.
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Page 567 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 79-00-00 - GENERAL -NOTE- The oil system is a wet sump, pressure type system. Continental Motors Recommends a new, reman- The engine sump has an 8 quart (U.S.) capacity. Ser- ufactured or newly overhauled engine should...
Page 568 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 79-30-00 - INDICATING er and this signal interfaces with the Garmin G1000 GEA 71 Engine/Airframe unit to indicate oil pressure. 79-30-01 - OIL PRESSURE Refer to 79-50-00 Oil System Troubleshooting chart Oil pressure indicating is provided through a pressure...
Page 569 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Refer to the Garmin G1000 service literature for trou- bleshooting. 79-50-00 - OIL SYSTEM TROUBLESHOOTING Troubleshooting chart is provided as a guide. Review probable causes, compare other troubleshooting charts for inter- related symptoms. Items are presented in sequence of complexity, not necessarily in order of probability. Refer to Garmin System Maintenance Manual for additional system description, service and troubleshooting instructions.
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Page 577 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 80-00-00 - GENERAL The airplane is equipped with a 24 volt starter supplied WASHER with engine package. The starter is located on engine case at rear of engine. MOUNTING PAD When ignition switch is placed in “START” position, cur-...
Page 578 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL -NOTE- Cranking should be limited to 30 seconds, and several minutes allowed between cranking peri- ods to permit starter to cool. STARTER RELAY STARTER RELAY (TYP.) FIGURE 80- 3 80-10-00 Page 6...
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Page 585 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 81-00-00 - GENERAL 81-10-02 - ALTERNATE AIR SYSTEM - TURBO- CHARGER OPERATION TURBOCHARGER OPERATION The turbocharger increases the power output and effi- The turbocharger system will continue to operate when ciency of the engine by supplying compressed air to the the primary air source is obstructed.
Page 586 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 81-20-00 - TURBOCHARGER TROUBLESHOOTING TROUBLE PROBABLE CAUSE CORRECTION Engine lacks power, reduction in Improperly adjusted controller Refer to CMI Maintenance and maximum manifold pressure or Overhaul Manual M- 18 section re- critical altitude garding Post Maintenance Adjust- ment and Test to adjust controller.
Page 587 Chapter 04- 00- 00 of this Service & or your nearest Authorized Mooney Service Center for Maintenance Manual. Complete Form QA 1027M P/N). Pay particular attention to the “Hi-Lok” pin areas for V- Band clamp installation and insert into on the clamp.
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Page 589 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 91 ELECTRICAL WIRING DIAGRAMS, SCHEMATICS AND HARNESSES...
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Page 591 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 91 ELECTRICAL WIRING DIAGRAMS AND SCHEMATICS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 91- Effectivity ....... .
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Page 593 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 91 ELECTRICAL WIRING DIAGRAMS AND SCHEMATICS/HARNESS DRAWINGS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 91- 00- 00 ......General ..........5 91- 00- 01 .
Page 594 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK...
Page 595 FIGURE 91- 1 91- 00- 02 - WIRING IDENTIFICATION SYSTEM The Mooney Aircraft Corporation wiring/equipments identification system used in current production aircraft deletes the Model Number annotation. The purpose of this is to standardize the identification of a system function/compo- nent for all model of aircraft.
Page 596 MOONEY INTERNATIONAL CORPORATION M20V SERVICE & MAINTENANCE MANUAL CODE/COMPONENT OR SYSTEM CIRCUIT FUNCTION LEGEND - 800416 SCHEMATIC DRAWING AC - AIR CONDITIONER JM - IGNITION, MAGNETO AH - ARTIFICIAL HORIZON JV - IGNITION, VIBRATOR AT - ACTUATOR, SWITCH AV - AVIONICS...
Page 597 MOONEY INTERNATIONAL CORPORATION M20V SERVICE & MAINTENANCE MANUAL WD - WARNING, START POWER WM - WARNING, MASTER WE - WARNING, ELECTRIC GEAR WN - WARNING, PRESSURIZATION WF - WARNING, FUEL QUANTITY WP - WARNING, PITOT HEAT WG - WARNING, TACHOMETER...
Page 598 800458 ....WIRING SCHEMATIC, FIREWALL TO ENGINE ..33- 0001 AND ON 800459 ....ELECTRICAL HARNESS INSTALL, M20U- M20V ..33- 0001 AND ON 810528 .
Page 751 L162C R9A1 R9A2...
Page 752 L13D L58B L13H R15B...
Page 753 L13A L58B R15B L66A R37A...
Page 754 L31B R15D L13H L16B L162C...
Page 755 R15B L31B L13F R15D L13C...
Page 756 L13E R41A L16A L162C...
Page 757 R15C R15B L58A R41A L22B L31B...
Page 758 R15C L22B R15C...
Page 759 L31B R15B L162C...
Page 760 R15B L58B L13H L22A L162C R41A L58A...
Page 761 L13D R15B...
Page 762 L13F R9A2 R15B L162C...
Page 763 L13A L162B L31A R37A R15B L31B R15C L162C L13E...
Page 764 L16A L114A R15B L13E L13C...
Page 765 L13A L58A R15B L15A L38A L156B...
Page 766 L156B L156C R15B L66A L13B...
Page 767 L13B L66A R15B L58B R9A2 L13G R15B...
Page 768 L114A L16A R11A...
Page 769 L22B L58A R15C L13A L13E R9A1 R15B L38A...
Page 770 L31A L38A L13A L58A L16A...
Page 771 L162C L22B L13E L13F L16B L31B...
Page 772 R41A R15C R9A1 L22A...
Page 773 R15B R15C L162D L13E...
Page 774 L13F R9A1 R15B...
Page 775 R11A R15B L114A...
Page 776 R37A...
Page 777 L162B L162A R9A2 L162C...
Page 778 L13H R9A1 L58B R15B...
Page 779 R15B L13F L58B R15C R9A2...
Page 780 R15B L13D L13A R15E R15F L156B L156C L58A L13B R11A L16A...
Page 781 L13D L13F L13E L58A L66A L156B L156C R41A L162B L16B...
Page 782 L13F L16A R37A L16A L13C R15D R11A L31A R15B L22B R15C...
Page 783 L31B L31C L162C L16A R15C R15A...
Page 784 R9A1 L66B R41B...
Page 785 R9A1 R15G R15G R15G R15G...
Page 786 R9A1 R41A L58A R41B L66B L13H...
Page 787 R9A2 L58B R15B L156A L162A L13F...
Page 788 R15A R15A L31B L15G...
Page 789 R15F R15G L22B R15E L22A L13H L31C L31B R9A2 R9A1 R15D L13G L31A L13A R11A L13F R15B L13B L13C L38A L13D R15C R37A L58A L58B L13E L16A L15A L16B L66B L66A R41A R41B L114A L114 L156C L156 L156B L156A L162B L162C L162 L162A...
Page 801 L16A L114A R15B L31B...
Page 802 CERT...
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Page 871 120.00 0.00 53.00 100.00 120.00 0.00...
Page 873 0.00 53.00 91.36 100.00 120.00 142.00 19.00 0.00 19.00...
Page 874 R15G R15F L22B R15E L22A L13H L31C L31B R9A2 R9A1 R15D L13G L31A L13A R11A L13F R15A R15B L13B L13C L38A L13D R15C R37A L58A L58B L13E L16A L15A L16B L66A R41A R41B L114A L114 L156C L156 L156B L156A L162B L162C L162 L162A...
Page 878 BOSE PHONE BOSE PHONE...
Page 879 VIEW B-B VIEW A-A...
Page 880 DETAIL P VIEW A-A...
Page 882 120.00 100.00 0.00...
Page 884 VIEW LOOKING INBD LH...
Page 896 VIEW LOOKING INBOARD ON TAILCONE...
Page 897 VIEW LOOKING INBOARD...
Page 898 176.0 149.5 159.0 142.0 VIEW LOOKING INBD 120.0...
Page 899 142.0 0.00 VIEW G-G VIEW H-H...
Page 900 0.00 -2.00 VIEW J-J...
Page 901 VIEW E-E...
Page 902 VIEW D-D...
Page 903 VIEW K-K...
Page 904 VIEW LOOKING DOWN ON TAILCONE/EMPENAGE...
Page 905 VIEW M-M VIEW L-L VIEW LOOKING INBOARD AT TAILCONE/EMPENAGE...
Page 913 91.36 100.00...
Page 930 FLT PNL #3 WIRES GROUND BLOCK G1000 WIRING CONNECTOR CONTROL WHEEL GEA INTERFACE GDC74 GMA1347 ROLL SERVO MKR/A ANTENNA CABLE GCU476 KEYPAD AUDIO INTERFACE...
Page 951 VIEW LOOKING DOWN...
Page 996 FORWARD...
Page 997 FORWARD VIEW LOOKING OUTBOARD, RIGHT HAND SIDE CABLE LOOP DETAIL...
Page 1000 FORWARD VIEW LOOKING INBOARD, LEFT HAND SIDE...
Page 1004 0.00 VIEW LOOKING INBD R/H SIDE 110.47 TAILCONE (NO SKIN)
Page 1005 OUTBD...
Page 1006 (TOP VIEW) OUTBD VARIOUS PARTS NOT SHOWN FOR CLARITY MAGNETOMETER BRACKET RING ASSEMBLY 820355-3 SHELF NOT SHOWN FOR CLARITY VIEW S...
Page 1038 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 95 SPECIAL TOOLS...
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Page 1040 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 95 SPECIAL TOOLS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 95- Effectivity ....... .
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Page 1042 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 95 SPECIAL TOOLS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 95- 00- 00 ......Special Tools ........5...
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Page 1044: Towing
MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL 95-00-00 - SPECIAL TOOLS CHAPTER/SECTION PART NUMBER DESCRIPTION 1 - INTRODUCTION 5 - TIME LIMITS 6 - DIMENSIONS 7 - LIFTING MAC 010000- 000 MAIN JACK POINT 7- 10- 00 MAC 010038- 001...
Page 1045 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER/SECTION PART NUMBER DESCRIPTION 27 - CONTROLS (cont’d) GSE 030035- 501 SPRING EXTENDER 27- 40- 02 GSE 030035- 005 SPACER GSE 030035- 503 SPRING EXTENDER GSE 0300005 RUDDER TRAVEL BOARD 27- 50- 00...
Page 1046 MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER/SECTION PART NUMBER DESCRIPTION 72 - ENGINE M- 18 CMI MAINTENANCE AND OVER- HAUL MANUAL 72- 00- 00 IO- 18 CMI INSTALLATION AND OP- ERATION MANUAL 73 - ENGINE FUEL 74 - IGNITION...
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