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Mooney 33-0001, Service And Maintenance Manual

The Mooney 33-0001 Service And Maintenance Manual is a comprehensive guide for maintaining and servicing your aircraft. This manual covers all aspects of the Mooney 33-0001, with detailed instructions for proper care and maintenance. Download this manual for free from manualshive.com and keep your aircraft in top condition.

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MOONEY AVIATION COMPANY, INC.

M20V SERVICE AND MAINTENANCE MANUAL

Date

MAR 2017

Rev Date

CHAPTER 9

TOWING AND TAXIING

LIST OF EFFECTIVE PAGES

CHAPTER

SECTION

SUBJECT

PAGE

DATE

9- Effectivity

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9- Contents

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9- EFFECTIVITY

Summary of Contents for 33-0001

Page 1: ...AL MOONEY P N MAN185 ISSUED MARCH 2017 MOONEY INTERNATIONAL CORPORATION Copyright 2017 All Rights Reserved MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road Kerrville Texas 78028 tel 830 896 6000 ww...

Page 2: ......

Page 3: ...led on the Mooney Aircraft Model s addressed in this pubication This warning applies to placards manufactured at Mooney Aviation Company Inc facility WARNING Manufactured with 1 1 1 Trichlorethane sub...

Page 4: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK...

Page 5: ...revised pages Revision Date Affected Pages Description of Revision INTRODUCTION OI ALL Pages Original Issue Chapter 4 AIRWORTHINESS OI ALL Pages Original Issue Chapter 5 TIME LIMITS OI ALL Pages Origi...

Page 6: ...Pages Original Issue Chapter 39 ELECTRICAL PANELS OI ALL Pages Original Issue Chapter 51 STRUCTURES OI ALL Pages Original Issue Chapter 52 DOORS OI ALL Pages Original Issue Chapter 55 STABILIZERS OI...

Page 7: ...sue Chapter 80 STARTING OI ALL Pages Original Issue Chapter 81 TURBOCHARGER OI ALL Pages Original Issue Chapter 91 ELECTRICAL WIRING SCHEMATICS AND HARNESSES OI ALL Pages Original Issue Chapter 95 SPE...

Page 8: ...bulletins are normally incorporated When a subsequent Service Bulletin is issued afterthe delivery date MooneyInternational Corporationwill postthem onthe www mooney com website for owner s concerning...

Page 9: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Page Date 5 Rev Date MAR 2017 S B NUMBER DATE DESCRIPTION OF BULLETIN COMPLETED BY LOG OF REVISIONS SERVICE BULLETINS...

Page 10: ...f this publication is organized at four lev els Group Chapter System Section Sub system Subject Unit GROUP These are primary divisions of the manual that enable broad separation of content ie Airframe...

Page 11: ...lable they will be added to the list below VENDOR ADDRESSES PUBLICATIONS ENGINE PUBLICATIONS Continental Motors Aircraft Products P O Box 90 Mobile Alabama USA 36601 Attn Accounts Receivable Prepaid o...

Page 12: ...rich Avionics Systems Inc 5353 52nd Street SE P O Box 873 Grand Rapids MI 49588 0873 Telephone 800 253 9525 NAVIGATION LIGHTS STROBES Whelen Engineering Co Route 145 Winthrop Road Chester CT 06412 068...

Page 13: ...ND AREAS 00 GENERAL 7 LIFTING AND SHORING 10 JACKING 8 LEVELING AND WEIGHING 00 LEVELING 9 TOWING AND TAXIING 00 GROUND HANDLING 10 TOWING 20 WARM UP AND TAXIING 30 EMERGENCY PROCEDURES 10 PARKING AND...

Page 14: ...TION 25 EQUIPMENT FURNISHINGS 00 GENERAL 10 FLIGHT COMPARTMENT 50 CARGO COMPARTMENT 60 EMERGENCY EQUIPMENT 27 FLIGHT CONTROLS 00 GENERAL 10 AILERON SYSTEM 20 RUDDER SYSTEM 30 ELEVATOR SYSTEM 40 STABIL...

Page 15: ...LIGHTS MAINTENANCE PRACTICES 40 EXTERIOR LIGHTS MAINTENANCE PRACTICES 34 NAVIGATION 00 GENERAL 10 PITOT STATIC AIR PRESSURE SYSTEM 30 DIRECTIONAL GYRO COMPASS 90 MISCELLANEOUS INSTRUMENTS 35 OXYGEN 00...

Page 16: ...ABILIZER 20 ELEVATOR 30 VERTICAL STABILIZER 40 RUDDER 56 WINDOWS 00 GENERAL 10 20 WINDSHIELD CABIN WINDOWS 50 ACRYLIC DRILLING 57 WINGS 00 GENERAL 10 MAIN FRAME 20 AUXILIARY STRUCTURE 30 PLATES SKINS...

Page 17: ...IGNITION 00 GENERAL 10 POWER CONTROL 20 ENGINE FIRING ORDER 30 SWITCHING 76 ENGINE CONTROLS 00 GENERAL 10 ENGINE CONTROLS RIGGING 20 MAINTENANCE 77 ENGINE INDICATING 00 GENERAL 10 POWER 20 TEMPERATUR...

Page 18: ...Date 9 MAR 2017 Rev Date CHAPTER SECTION TITLE 81 TURBINES 00 GENERAL 20 TROUBLESHOOTING 30 SERVICING 40 PERIODIC REPLACEMENT COMPONENTS 91 SCHEMATICS AND HARNESSES 00 GENERAL 20 ELECTRICAL SYSTEM HAR...

Page 19: ...MOONEY AVIATION COMPANY INC M20V SERVICE AND MAINTENANCE MANUAL Page Date 10 MAR 2017 Rev Date INTENTIONALLY LEFT BLANK INTRODUCTION...

Page 20: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS...

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Page 22: ...V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 4 AIRWORTHINESS LIMITATIONS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 4 Effectivity 1 03 17 4 Contents 3 03 17 4 00 00 5...

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Page 24: ...ICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 4 AIRWORTHINESS LIMITATIONS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 4 00 00 Airworthiness Limitations 5 4 10 01 Replacement Schedule 5...

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Page 26: ...rance Form QA1027M must be filled out Tailpipe V band clamps shall be replaced with a new clamp after it has been removed the second time The V band clamp shall also be replaced with a new clamp at ea...

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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 30: ...03 17 5 Contents 3 03 17 5 00 00 5 03 17 5 10 00 6 03 17 5 10 01 7 03 17 5 10 01 8 03 17 5 10 01 9 03 17 5 20 00 10 03 17 5 20 01 11 03 17 5 20 01 12 03 17 5 20 01 13 03 17 5 20 02 14 03 17 5 20 05 15...

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Page 32: ...5 00 07 Fuel System 5 5 10 00 Time Limit Components 6 5 10 01 Overhaul Maintenance and Replacement Schedule 6 5 10 01 G1000 Servicing Information 8 5 20 00 Scheduled Maintenance Checks 10 5 20 01 Ins...

Page 33: ...M20V SERVICE AND MAINTENANCE MANUAL MOONEY INTERNATIONAL CORPORATION INTENTIONALLY LEFT BLANK...

Page 34: ...are controlled by a spring loaded up off down switch on the center console 5 00 04 ELECTRIC POWER SYSTEM The Master Switch and power relay control the electri cal power system comprised of a 100 AMP...

Page 35: ...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...

Page 36: ...lid Green Kevlar Bottle P N 026N2001 3 Hydrostatic Test Required 3 year intervals A C with Striped Green Carbon Bottle P N 026N2003 3 Hydrostatic Test Required 5 year intervals Oxygen Bottle return to...

Page 37: ...PFD Remove Replace On Condition GDU 1042 MFD Remove Replace On Condition GMA 1347 Remove Replace On Condition GIA 63 IAU Qty 2 Remove Replace On Condition GEA 71 EAU Remove Replace On Condition GTX 33...

Page 38: ...M Description Procedure Interval TVS Unit Replacement Replace the voltage suppressor unit Refer to G1000 GFC700 Wiring Diagram The Standby Attitude Indicator Voltage Suppres sor is located behind inst...

Page 39: ...ween systems and the engine shall be torqued to 25 inch pounds Hose clamp installations on blast tubes air ducts drain and vent lines shall be torqued to 15 inch pounds 4 Pipe Threads Tightening and t...

Page 40: ...ropriate class is intended to provide an assembly capable of being tightened to the bolt proof load without thread stripping occurring The torque value to be set for a particular size of screw is depe...

Page 41: ...95 70 135 99 160 118 M14 X 1 5 150 110 210 154 250 184 M16 X 1 5 225 165 315 232 380 280 M18 X 1 5 325 239 460 339 550 405 M20 X 1 5 460 339 640 472 770 567 M22 X 1 5 610 449 860 634 1050 774 M24 X 2...

Page 42: ...M16 X 1 5 210 154 295 217 350 258 M18 X 1 5 305 224 425 313 510 376 M20 X 1 5 425 313 600 442 720 531 M22 X 1 5 570 420 800 590 960 708 M24 X 2 720 531 1000 737 1200 885 METRIC CONVERSION FACTOR One N...

Page 43: ...review includes inspection of the Air plane Flight Manual Aircraft Log Book Engine Log Book Registration Certificate Airworthiness Certifi cate Weight Balance Record Engine Service Infor mation Aircra...

Page 44: ...e rial E Service engine oil sump with proper type grade and amount of lubricating oil F Inspect engine intake and exhaust systems for evidence of leakage looseness or damage G Inspect ignition leads h...

Page 45: ...nual To verify correction of malfunctions and abnor malities perform a second runup and flight test after the 100 hour annual inspection engine set up A Complete a differential hot engine compres sion...

Page 46: ...spinner bulkhead for snug fit between propeller hub cylinder and rear bulkhead Use shims as necessary for snug fit 3 LANDING GEAR and RETRACTION SYSTEM INSPECTION A Inspect tires for proper inflation...

Page 47: ...door lock mechanisms for lu brication and proper engagement See Section 52 11 00 for rigging procedures I Inspect baggage door and baggage compart ment for damage corrosion warpage hinge security con...

Page 48: ...ube with 2 wide Y9265 polyure thane tape 1 2 tape overlap Trim tubes without tape which show signs of abrading bulkhead grommet should be wrapped See Service Bulletin M20 185 MAX TUBE WEAR 007 in wall...

Page 49: ...operly the GREEN PROP DE ICE switch lamp is illuminated and the G1000 shows no annunciation Amber PROP DE ICE if the PROP DE ICE switch is in ON position with Green PROP DE ICE switch lamp illuminated...

Page 50: ...tings 100 Retraction Tube Rod End Bearings Bellcranks Bungees 100 100 100 Gear Door Rod End Bearings 50 4 Main Gear Grease Fittings 100 Retraction Tube Rod End Bearings Bellcranks Bungees 100 100 100...

Page 51: ...nt Stabilizer Trim Chain Gear 100 16 Elevator Rudder Controls Control Tube Rod End Bearings 100 Bellcranks 100 Guide Blocks 100 Flap Indicator Cable 100 Electric Flap Actuator Gear Box 500 Electric Fl...

Page 52: ...ote Battery Duracell DL1 3NB 3 volt Lithium Battery ELT ME 406 Batteries ME406 Series LiMnO2 Battery Pack 100 100 AR 100 100 34 Seat Belt Restraints Standard Inflatable Restraints Optional refer to Ch...

Page 53: ...CM Spec MHS 24 Oil Specifications Oil Specification or Oil Grade First 25 Engine Hours Non dispersant mineral oil conforming to SAE J1966 shall be used during the first 25 hours of flight operations H...

Page 54: ...NANCE MANUAL Page Date 25 MAR 2017 Rev Date 7 27 19 27 33 25 24 27 27 17 12 32 11 12 2 10 13 14 30 29 3 23 1 21 20 22 15 16 27 27 26 27 19 6 14 4 18 28 5 12 13 10 7 11 12 32 31 8 9 21 ACCESS COVER IDE...

Page 55: ...L CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Page Date 26 MAR 2017 Rev Date A copy of this form can be found in the Support Section of our website at www mooney com QUALITY ASSURANCE FORM QA1027M...

Page 56: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 6 DIMENSIONS AND AREAS...

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Page 58: ...AL Date MAR 2017 Rev Date CHAPTER 6 DIMENSIONS AND AREAS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 6 Effectivity 1 03 17 6 Contents 3 03 17 6 00 00 5 03 17 6 00 01 6 03 17 6 00 02 7 03...

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Page 60: ...Date MAR 2017 Rev Date CHAPTER 6 DIMENSIONS AND AREAS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 6 00 00 Dimensions and Areas 5 6 00 01 Specifications 5 6 00 02 Dimensions 8 6 00 03 Wing Station R...

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Page 62: ...6 1 Liters 22 7 Liters Spark Plugs Champion AC 273 18m m or equivalent RHB32E Two Prong Plug Gap 016 0 41mm 021 0 53mm RHB32S Fine Wire Iridium Plug Gap 016 0 41mm 021 0 53mm Oil Grade Normal Service...

Page 63: ...l PHC J3YF 1RF F7498 B Note B Indicates W Boots Installed Pitch Angle 30 in Sta LOW 17 0o 0 2o HIGH 38 0o 1 0o Diameter Min Max 74 76 188 0 193 0 cm Governor Hartzell Governor Hartzell AIRFRAME WEIGHT...

Page 64: ...table Operation Electrical Wheel Track 9 2 279 4 cm Wheel Base 6 7 1 2 201 9 cm Tire Size Nose 6 Ply Rating 5 00x5 Tire Size Main 6 Ply Rating 6 00x6 Tire Pressure Nose 49 Lbs Sq In Tire Pressure Main...

Page 65: ...Rev Date 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 1112 5 cm 279 4 cm 76 193 04 cm 201 9 cm 6 7 1 2 9 2 358...

Page 66: ...ate 9 MAR 2017 Rev Date STA FUSELAGE STATIONS 211 50 STA 176 00 STA 142 00 STA 100 00 STA 21 80 STA 53 00 STA 5 00 STA 5 375 3 68 STA WING STATION RIBS 103 50 210 97 STA 193 50 STA 147 75 STA STA 24 5...

Page 67: ...INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Page Date 10 MAR 2017 Rev Date STA 25 75 STA 5 25 STA 52 50 STA 70 0 STA 42 25 STA 4 43 STA 42 25 STA 70 0 EMPENNAGE STATIONS FIGURE 6 3 6...

Page 68: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 7 LIFTING AND SHORING...

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Page 70: ...M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 7 LIFTING AND SHORING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 7 Effectivity 1 03 17 7 Contents 3 03 17 7 10 00 5 03...

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Page 72: ...NTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 7 LIFTING AND SHORING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 7 10 00 Jacking 5 7 10 00 Jacking 6 7 C...

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Page 74: ...tact jack point 3 To raise engine remove top cowling and support the engine using an A Frame with chain hoist or hy draulic Cherry Picker and hook into the engine lifting hook LYCOMING engine mounted...

Page 75: ...TIE DOWN RING WARNING DO NOT USE AS A JACK POINT ADJUSTABLE JACKSTANDS ENGINE LIFT POINT A FRAME WITH CHAIN HOIST LYCOMING ENGINE WARNING DO NOT USE PROPELLER JACKS OR PROPELLER STANDS ENGINE LIFT POI...

Page 76: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 8 LEVELING AND WEIGHING...

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Page 78: ...MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 8 LEVELING AND WEIGHING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 8 Effectivity 1 03 17 8 Contents 3 03 17 8 00 00 5 03 17 8 00 01 6 0...

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Page 80: ...IONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 8 LEVELING AND WEIGHING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 8 00 00 Leveling 5 8 00 01 Weight and Balanc...

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Page 82: ...e fuel to each tank see Pilot s Oper ating Handbook for proper quantity of unusable fuel 5 Fill oil to capacity 8 quarts 6 Position a 2000 pound capacity scale under each of the three wheels 7 Level a...

Page 83: ...PTY WEIGHT 950 2100 1000 1050 2200 2300 1100 Kg 2400 2500 LBs 1150 1050 CENTER OF GRAVITY F S Inches 2363 2344 19 42 42 15 209 5 x x 43 98810 102791 3981 44 45 503 CENTER of GRAVITY F S mm ON or ABOVE...

Page 84: ...MAINTENANCE MANUAL Page Date 7 MAR 2017 Rev Date REF POINT NOSE GEAR TRUNNION STA 13 Lm n Lm r Lc g Wn Lm Wr Wl L M N M R L MEASUREMENTS DATUM STA 0 REFERENCE LEVELING SCREWS LEVEL REF INCHES CM INCHE...

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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: ...0V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 9 TOWING AND TAXIING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 9 Effectivity 1 03 17 9 Contents 3 03 17 9 00 00 5 03 17...

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Page 90: ...ERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 9 TOWING AND TAXIING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 9 00 00 Ground Handling 5 9 10 00 Towing 5 9 20 00 Warm up Taxiing 5 9...

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Page 92: ...g turns for acknowledgement of maneuvers refer to Garmin G1000 Cockpit Reference Guide for detailed description of flight display features 5 Check Garmin G1000 Multi Function Display MFD for any slugg...

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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: ...V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 10 PARKING AND MOORING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 10 Effectivity 1 03 17 10 Contents 3 03 17 10 00 00 5 0...

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Page 98: ...MANUAL Date MAR 2017 Rev Date CHAPTER 10 PARKING AND MOORING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 10 00 00 General 5 10 10 00 Parking 5 10 10 01 Storage Flyable 5 10 10 02 Storage Prolonged...

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Page 100: ...rotec tion 1 Refer to paragraph 10 20 00 for mooring instruc tions 2 Tape or cover all openings 3 Remove batteries charge fully and store in a cool place 4 Raise aircraft to remove weight from tires a...

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Page 102: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS...

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Page 104: ...SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 11 PLACARDS AND MARKINGS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 11 Effectivity 1 03 17 11 Contents 3 03 17 11 00 00 5...

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Page 106: ...ERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 11 PLACARDS AND MARKINGS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 11 00 00 General 5 11 10 00 Markings Exterior Paint 5 11 20 30 00 P...

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Page 108: ...PAINT Exterior paint schemes are depicted in M20V Illus trated Parts Catalog 11 20 30 00 PLACARDS EXTERIOR INTERIOR All required placards and their locations both interior and exterior are listed in S...

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Page 110: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 12 SERVICING...

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Page 112: ...ANCE MANUAL Date MAR 2017 Rev Date CHAPTER 12 SERVICING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 12 Effectivity 1 03 17 12 Contents 3 03 17 12 00 00 5 03 17 12 10 04 6 03 17 12 20 02...

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Page 114: ...ing 5 12 00 01 Servicing Intervals 5 12 10 00 Replenishing 5 12 10 01 Fuel Tanks 5 12 10 02 Fuel Drains 5 12 10 03 Engine Oil 5 12 10 04 Oxygen System Precise Flight 6 12 20 00 Scheduled Servicing 6 1...

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Page 116: ...draining until free of water or contamina tion WARNING After servicing aircraft with fuel wait at least five minutes for moisture and sediment to settle before draining and checking both the fuel tan...

Page 117: ...YGEN SYSTEM PRECISE FLIGHT SYSTEM OPTIONAL The oxygen cylinder when fully charged contain approximately 77 cubic feet of aviators breathing oxy gen Specifications No MIL O 27210 Recharging of this oxy...

Page 118: ...aled lead acid batteries are factory permanently sealed and require no additional electrolyte or water Service wet cell batteries with distilled water to main tain electrolyte above plates After addin...

Page 119: ...containing MIL H 5606 fluid 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 craft s...

Page 120: ...e immediately with water Treat exposed area with bicarbon ate of soda solution followed by thorough washing with a mild aircraft detergent solution F Blow moisture away from areas that may trap accumu...

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Page 122: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES AIRFRAME...

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Page 124: ...HAPTER 20 STANDARD PRACTICES AIRFRAME LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 20 Effectivity 1 03 17 20 Contents 3 03 17 20 00 00 5 03 17 20 00 01 6 03 17 20 00 02 7 03 17 20 00 02 8...

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Page 126: ...CONTENTS CHAPTER SECTION SUBJECT PAGE 20 00 00 General 5 20 00 01 Skin Specifications 5 20 00 02 Corrosion Detection Prevention 7 20 00 03 Painting 9 20 00 04 Intumescent painting FireFree 10 20 00 0...

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Page 128: ...50 STA 59 25 STA 103 50 STA 147 75 STA 193 50 STA 210 97 STA 19 17 13 12 11 10 14 9 16 8 15 7 1 18 2 3 4 5 6 INDEX SKIN MATERIAL INDEX SKIN MATERIAL NO THICKNESS NO THICKNESS 1 0 063 2024 T 3 CLAD 12...

Page 129: ...1 5 INDEX SKIN MATERIAL NO THICKNESS 1 0 025 2024 T 3 CLAD 2 0 032 2024 T 3 CLAD 3 Polyester Glass Fiber Reinforced 4 0 025 2024 T 3 CLAD Right side only 5 0 020 2024 T 3 CLAD 6 0 025 2024 T 3 CLAD 7...

Page 130: ...used Paint removing sub stances left in metal crevices will cause further corro sion Turco 6898 Turco Products Inc 6135 South Central Ave Los Angeles California will remove cor rosion from aluminum a...

Page 131: ...exterior surface dry after washing down E Hangar aircraft when not in use F If battery acid is spilled on any part of the aircraft immediately wash the area with a solution of sodium bi carbonate in w...

Page 132: ...ylon pads or aluminum wool may be done dry or wet with one of the wipe solvents listed above After the old paint grime etc has been loosened and removed the scoured area should be wiped with a tack ra...

Page 133: ...p900 catalyst no c916 or approved alternate for composite substrates ensure substrate surface is clean prior to prime paint 3 Use only manufacturer approved reducer for thin ning respective paints if...

Page 134: ...t if applicable Use caution not to damage sur rounding area 2 Sand using 180 grit or finer sandpaper around the damaged portion Sanding should extend for each ply removed plus a 1 border for the addit...

Page 135: ...d spacing will be determined by the size of the repair See Figures 20 8 and 20 9 PATCH WITH HYSOL APPLY ALUMINUM PATCH TO INNER SURFACE OF SHELL FIGURE 20 8 PATCH SECURED CLECO AND CLAMP ALUMINUM PATC...

Page 136: ...PLY APPLY PLIES APPLY COATED PLIES AND SQUEEGEE FIGURE 20 12 12 Coat rubber gasket on caul plate with petroleum jelly as a release agent Place caul plate over fiberglass plies with rubber gasket facin...

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Page 138: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 21 ENVIRONMENTAL SYSTEMS...

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Page 140: ...T PAGE DATE 21 Effectivity 1 03 17 21 Contents 3 03 17 21 00 00 5 03 17 21 50 00 6 03 17 21 51 00 7 03 17 21 51 01 8 03 17 21 52 00 9 03 17 21 52 02 10 03 17 21 53 00 11 03 17 21 53 03 12 03 17 21 54...

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Page 142: ...ompressor Drive Belt Inspection Maint 12 21 54 01 Belt Removal 12 21 54 02 Drive Belt Replacement Procedure 12 21 54 03 Drive Belt Alignment Procedure 13 21 54 04 Drive Belt Tensioning Procedure 14 21...

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Page 144: ...be made at regular intervals to en sure proper operation 21 40 00 HEATING Heat is extracted from the high pressure temperature flow between the compressor and intercooler through flexible hoses conne...

Page 145: ...is then directed to the evaporator module expansion valve where the high pressure liquid is expanded to a low pressure The expansion process creates a super cool gas which passes through the evaporato...

Page 146: ...D AIR103A FRONT EVAP BLOW 4 2 3 1 AIR11A14 AIR08A14 AIR17A14 AIR04A14 PL02A 2 1 TAILCONE CL37A AIR02A14 8 AIR COND TAILCONE AIR01A14 SUPPLIED VENDOR AIR01A14 AIR BR20 CONDR 20 CL04A PL04A RC04A CL04A...

Page 147: ...FIGURE 21 4 21 51 01 SPECIAL TOOLS AND OR EQUIPMENT REQUIRED The following tools and or equipment are required to leak check a refrigerant plumbing system 1 Gaseous dry nitrogen regulated source 0 500...

Page 148: ...ply soapy leak check fluid to each connection to locate leaks CAUTION Do not use any leak dye in R 134a system or damage to system may result 13 Use thread sealant on all male fitting threads sparingl...

Page 149: ...s tem is ready for refrigerant charging NOTE Excessive water and or air in the system will cause pressure to rise expansion valve freeze up 21 52 03 REFRIGERANT CHARGING PROCE DURE Charging the system...

Page 150: ...the expansion valve is trying to stabilize to the pre set suction pressure value CAUTION Do not overcharge system or component and system damage may occur Full system charge is approximately 2 2 lbs o...

Page 151: ...nce with but not limited to the following 1 Verify that system leak check and refrigerant charging has been performed and system is operating at typical values as outlined in Section 21 52 03 13 2 Rem...

Page 152: ...t size and part number see Illustrated Parts Catalog before installing or damage may result 2 Place new belt or inspected and cleaned belt over compressor pulley idler pulley and drive pulley CAUTION...

Page 153: ...r sheave assembly and place as many 0 020 shims CMI P N 643956 20 between idler sheave and bearing as required to achieve correct alignment between idler and compressor sheave outer pulley When alignm...

Page 154: ...elt for cracks wear and ex cessive oil 9 Clean all oil and other contaminates from belt with clean shop rag NOTE Checking compressor oil quantity is required only if an excessive amount of oil is obse...

Page 155: ...he fol lowing procedure to add the required oil to the system CAUTION Only an E S I approved oil may be used in this type of compressor Do not overfill compressor with oil or system performance will b...

Page 156: ...ack wire ground and resistor red wire also run straight through clamp no splice G Run all wires through wire clamp and secure with mounting screw and washer H Connect power leads to blower assembly an...

Page 157: ...ailed 4 Replace 5 Failed pressure switch 5 Replace 6 Failed power contactor 6 Replace 7 Failed motor drive 7 Replace 8 Vented system 8 Pressure check evacuate charge 9 Low ambient temperature 9 Normal...

Page 158: ...eed OK 1 Failed switch 1 Replace 2 Failed resistor 2 Replace 3 Failed relay 3 Replace G Compressor Condenser will not operate 1 C B failed or OFF 1 Turn ON or replace 2 Relay s failed 2 Replace 3 Pres...

Page 159: ...SERVICING AND OR MAINTENANCE SCHEDULES 1 SCHEDULED MAINTENANCE TABLE CHAPTER 5 normally lists the maintenance and replacement time frames for components However since specific air conditioning compone...

Page 160: ...handling Always wear eye and hand protection when servicing an air conditioning system Liquid refrigerant can cause frostbite and or blindness 2 Recovery of refrigerant Do not discharge R 134a refrige...

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Page 162: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 22 AUTOPILOT SYSTEMS...

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Page 164: ...OPILOT SYSTEMS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 22 Effectivity 1 03 17 22 Contents 3 03 17 22 00 00 5 03 17 22 00 00 6 03 17 22 10 00 7 03 17 22 10 02 8 03 17 22 10 02 9 03 17...

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Page 166: ...vos and Servo Mounts 7 22 10 01 Roll Servos and Servo Mount 7 22 10 02 Pitch Trim Servos and Servo Mount 8 22 10 03 Pitch Servos and Servo Mount 10 22 10 04 Servo Clutch Adjustment 11 22 10 05 Flap Di...

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Page 168: ...mode annunciations are sent to the PFD through a high speed Ethernet connection for dis play The Flight Director operates independently of the Autopilot and allows the pilot to hand fly the air craft...

Page 169: ...ION HARNESS ASSY MAGNETOMETER OAT HARNESS ASSY INBOARD MAGNETOMETER GMU 44 OAT PROBE HARNESS ASSY GTP 59 OAT ROLL SERVO CABIN AREA GDC 74 AIR DATA FORWARD HARNESS ASSY FORWARD AFT DISCONNECT AFT HARNE...

Page 170: ...rvo output gear using a lint free cloth NOTE It is not necessary to remove all of the grease from the output gear only the excess grease DO NOT USE SOLVENTS TO CLEAN THE OUTPUT GEAR 2 Removal of Roll...

Page 171: ...and test per the G1000 Line Maintenance and Configuration Manual 190 00303 04 Rev F and or later FAA ap proved revision for more detailed information J Install center console panels and belly fairing...

Page 172: ...s are not settable once manufactured 4 Installation of Pitch Trim Servo and Servo Mount A Install Pitch Trim servo mount to bracket with original 4 bolts Refer Figure 22 9 Torque Chart for Specificati...

Page 173: ...NTER BALL CABLE GUARD COVER DOWEL SCREWS AND BRIDLE CABLE PITCH SERVO BRIDLE CABLE CENTER FIGURE 22 8 C Remove Pitch Servo Mount 4 attaching bolts and remove from Aircraft 3 Pitch Servo Mount Clutch A...

Page 174: ...lutch for the engaged axis by moving the appropriate control move yoke or stick forward and back for pitch through its range of motion The controls should move with some resistance through their range...

Page 175: ...cable relative 1 6 to front face of GSM 85 A reference Grease for GSA 8X gear see section 3 3 for regreasing Aeroshell 33MS instructions It is recommended to follow the practices of AC43 13 1B section...

Page 176: ...trim should immediately run in the DOWN direc tion 5 The flap discrete input check is complete 22 20 00 TROUBLESHOOTING Troubleshooting the GFC 700 system per the G1000 Line Maintenance and Configura...

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Page 178: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER...

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Page 180: ...24 Effectivity 1 03 17 24 Contents 3 03 17 24 00 00 5 03 17 24 31 02 6 03 17 24 31 02 7 03 17 24 31 02 8 03 17 24 31 02 9 03 17 24 31 03 10 03 17 24 31 03 11 03 17 24 31 04 12 03 17 24 33 00 13 03 17...

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Page 182: ...rnator Troubleshooting Tests 8 24 31 03 Charging System Maintenance Standby Alternator 10 Post Installation Test Procedure Standby Alt 10 Troubleshooting Voltage Regulator Standby Alt 10 Troubleshooti...

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Page 184: ...intenance Manual 190 00907 00 24 30 00 D C GENERATION 24 31 01 CHARGING SYSTEM MAINTENANCE MAIN ALTERNATOR 1 Alternator Systems Servicing When the ammeter Garmin G1000 MFD display shows a discharge at...

Page 185: ...ll turn off the APAC taking the alternator offline Alternator Off Line Sensor AOS Indicator AOI The AOI will come on under these conditions The ALT switch is OFF OPEN while battery switch is ON The fi...

Page 186: ...condition of the alternator APAC system A Red TSL with the Bat Alt switches on means there is an internal or external ground short in the alter nator field circuit Some alternator s field short to gro...

Page 187: ...e POST INSTALLATION TEST PROCEDURE 1 Turn On the Alt Bat switches observe that the AOI light is on 2 On the APAC the TSL should be Green If the TSL is Red the Field is shorted to ground 3 If the TSL i...

Page 188: ...ease with increasing Buss load Poor connection between the load shunt and the ammeter may also give false load indication Buss voltage drops with load increase See Alternator carries only about half i...

Page 189: ...verify primary alternator operation The Stby Alt On annunciator should be OFF 10 Return the engine to idle RPM TROUBLESHOOTING VOLTAGE REGULATOR STANDBY ALTERNATOR 1 Turn all switches off Use the lowe...

Page 190: ...current sensor in the standby alternator output lead 10 If the measurements in Steps 8 and 9 are satis factory prepare to monitor the voltage between termi nals 3 and 7 of the regulator with the engin...

Page 191: ...nting area and flush battery with mixture Do not allow soda water to enter battery cells permanent damage will result if soda mixes with electrolyte C Rinse thoroughly with clear water dry the area D...

Page 192: ...d the G1000 shows no annunciation AMBER PITOT HEAT if the PITOT HEAT switch is in ON position with Green PITOT HEAT switch lamp illuminated but Pitot Heat system has failed STEADY AM BER PITOT HEAT OF...

Page 193: ...NCIATIONS AND WARNING LIGHTS CONT D GEAR DOWN ALERT ANNUNCIATION FIGURE 24 4 GEAR UNSAFE MASTER WARNING FIGURE 24 5 GEAR UNSAFE ALERT ANNUNCIATION GEAR DOWN FIGURE 24 6 GEAR UNSAFE ALERT ANNUNCIATION...

Page 194: ...IATIONS AND WARNING LIGHTS CONT D ALTERNATE AIR ALERT ANNUNCIATION FIGURE 24 10 PROP DE ICE FAIL MASTER CAUTION FIGURE 24 11 PROP DE ICE FAIL ALERT ANNUNCIATION FIGURE 24 12 PITOT HEAT FAIL MASTER CAU...

Page 195: ...ANNUNCIATIONS AND WARNING LIGHTS CONT D ALTERNATOR FAIL ALERT ANNUNCIATION FIGURE 24 16 START POWER ALERT ANNUNCIATION FIGURE 24 17 EMERGENCY BUS ALERT ANNUNCIATION FIGURE 24 18 DOOR OPEN MASTER WARNI...

Page 196: ...TS CONT D HIGH BOOST PUMP ALERT ANNUNCIATION FIGURE 24 22 LOW FUEL WARNING LEFT OR RIGHT MASTER WARNING FIGURE 24 23 LOW FUEL LEFT CAUTION ALERT ANNUNCIATION FIGURE 24 24 LOW FUEL LEFT WARNING ALERT A...

Page 197: ...recommended prior to flight CAUTION When either battery voltage is low inspec tion should be conducted to determine con dition of battery and or reason for battery being low Replacement or servicing...

Page 198: ...36 00 LANDING GEAR CIRCUITS 1 Limit switches and relays operate the reversible landing gear actuator motor A landing gear air pres sure safety switch actuated by pitot air pressure pre vents landing...

Page 199: ...refers to the Garmin Flight Management System FMS Controller used in a Garmin Integrated Flight Deck The GCU 478 Line Replaceable Unit LRU provides alpha numeric softkey and flight planning function...

Page 200: ...lts Charging rate too high Reduce charging rate by adjusting voltage regulator Electrolyte runs out of vent plugs Too much water added to battery and charging rate too high Drain battery and keep at p...

Page 201: ...ails to operate Contd After seating thoroughly clean brushes and commutator to pre vent excessive wear Keep motor bearing free from sand or metal particles Dirty commutator If commutator is rough or d...

Page 202: ...and from the se lected battery through the battery relay The batteries negative leads attach to a structural ground on the air frame The Master Switch ON closes the relay and supplies power to the ai...

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Page 204: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT AND FURNISHINGS...

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Page 206: ...EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 25 Effectivity 1 03 17 25 Contents 3 03 17 25 00 00 5 03 17 25 10 00 6 03 17 25 10 03 7 03 17 25 10 03 8 03 17 25 10 03 9 03 17 25 10 03 10 03 17 25 1...

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Page 208: ...ABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 25 00 00 General 5 25 00 01 Interior Surfaces 5 25 10 00 Flight Compartment 6 25 10 01 Seats 6 25 10 02 Seat Belts Restraints 6 25 10 03 Seat Belts Restra...

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Page 210: ...Leather Care Instructions 1 Gently dust surface area regularly with a dry soft cloth Due to the natural characteristics of leather scratches and marks may appear on the surface over time This appearan...

Page 211: ...or bolts forward and aft push seat forward to lift up front of seat structure then aft to lift up rear rollers of seat structure Installation is the reverse of removal 25 10 02 SEAT BELTS RESTRAINTS...

Page 212: ...source B Inflatable Airbag Restraint System Cleaning Optional Restraint System CAUTION INFLATABLE AIRBAG RESTRAINT SYSTEMS Do not immerse the airbag belt assembly into water Moisture may damage intern...

Page 213: ...points AAIR V23 SYSTEM COMPONENTS AND PARTS The AAIR V23 System consists of these core compo nents S Seatbelt Airbag Assembly SAA S Inflator Assembly S Electronics Module Assembly EMA S Cable Interfac...

Page 214: ...as its power source which is user replaceable To perform properly the SDT needs to be re calibrated yearly by the OEM Refer to program specific Am Safe s Supplemental Maintenance Manual for return in...

Page 215: ...MING THOROUGHLY FAMILIAR WITH ALL WARNINGS CAUTIONARY STATEMENTS AND DIRECTIVES CONCERNING THE AAIR SYSTEM AS FOUND IN AMSAFE S SUPPLE MENTAL MAINTENANCE MANUAL OR AIR CRAFT OEM MAINTENANCE MANUAL FAI...

Page 216: ...SEAT LED illuminates 4 Unbuckle seatbelt 5 Repeat Step 3 for next seat position 6 Unbuckle seatbelt Turn SDT ON OFF switch to OFF If finished testing all seat positions in aircraft replace the diagnos...

Page 217: ...dge S The amount of fray exceeds 10 of the width of the webbing and exceeds 8 inches in length S Webbing with more than 15 broken yarns in loca tions other than the edge Webbing that is frayed or dist...

Page 218: ...G COVER OR GAS HOSE MATERIAL When cleaning non metallic parts except airbag cov er use warm water and household soap laundry de tergent Care should be taken to use only enough cleaning agent to produc...

Page 219: ...Set Hex Drive Standard Issue Torque Wrenches In Lb Type to accommo date 5 to 130 In Lbs of torque Standard Issue Thread Locking Com pound Loctite 242 Loctite Corporation 1 800 LOCTITE 562 8483 Remova...

Page 220: ...MES IN THE VICINITY OF THE EMA DEPLOYMENT OF THE SYSTEM MAY OCCUR 1 Before replacing new Inflator s Assy s unscrew the Shipping Cap from the Inflator hose fitting Figure 25 2 Do not discard Shipping C...

Page 221: ...on each passenger s arm rest excluding front seat passenger can now activate On Off or DIM in dividual reading lights Front seat passenger s light switch is located forward of cabin door hinge on sid...

Page 222: ...thorough examina tion of the extinguisher covering mechanical parts ex tinguishing agent and expelling means It is intended to give maximum assurance that an extinguisher will op erate effectively an...

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Page 224: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS...

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Page 226: ...SUBJECT PAGE DATE 27 Effectivity 1 03 17 27 Contents 3 03 17 27 00 00 5 03 17 27 20 00 6 03 17 27 20 00 7 03 17 27 20 00 8 03 17 27 30 00 9 03 17 27 30 03 10 03 17 27 40 02 11 03 17 27 40 02 12 03 17...

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Page 228: ...ting 13 27 42 00 Electric Trim System Opt 13 27 50 00 Wing Flap System Rigging 14 27 60 00 Aileron Rudder Interconnect System 15 27 90 00 Miscellaneous 15 27 91 00 Control Surface Static Balancing 15...

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Page 230: ...ubes and bellcranks Lead counter weights static balance the ai lerons 1 Aileron Removal and Installation A Remove control tube attaching bolt nut and washer at aileron horn B Remove bolts nuts and was...

Page 231: ...TROL TUBE BOB WEIGHT YOKE CONTROL SHAFT CONTROL TUBE CONTROL YOKE H YOKE CONTROL SHAFT JACKSHAFT ASSY CONTROL TUBE BELLCRANK ASSY E BELLCRANK ASSY YOKE CONTROL SHAFT H C JACKSHAFT ASSY B CONTROL TUBE...

Page 232: ...ADJUSTMENT FIGURE 27 4 2 Rudder Rigging and Adjustment A Raise aircraft nose wheel off ground See Sec tion 7 10 00 B Set stabilizer trim control in neutral position sta bilizer parallel with aircraft...

Page 233: ...R TUBE ELEVATOR TUBE R R P M RUDDER ELEVATOR STOP ADJUSTMENT FIGURE 27 7 K After setting stops re tighten all jam nuts bolts and secure recheck all travel limits L Center nose wheel by removing nut wa...

Page 234: ...all elevators in reverse sequence of remov al Recheck attaching hardware for security and safety Set elevators RH LH to be level with horizontal stabi lizer Adjust rod end bearings 9 Fig 27 9 at eleva...

Page 235: ...aircraft centerline Fig 27 11 CAUTION An incorrect hardware installation may cause scoring of the Stabilizer Trim Torque Tube as a result of the bolt thread contacting the Stabiliz er Trim Torque Tube...

Page 236: ...ct with trim screw nut F Tighten setscrew NOSE UP stabilizer trim control rigging is now complete 2 Stabilizer Trim Indicator Rigging The indicator is connected to the trim control wheel as sembly to...

Page 237: ...if desired F Electrically run actuator for left rudder deflection depress left sides of both RUDDER TRIM split switches until limit switch turns OFF actuator motor Aft limit switch is for LEFT rudder...

Page 238: ...ten an additional 25 to 38 inch extension of forward spring Secure forward turnbuckle E Complete log book entry and return aircraft to service or complete remaining maintenance action 27 41 00 Stabili...

Page 239: ...at inter vals with lubricants prescribed in CHAPTER 5 The flap system incorporates a preselect feature which allows flaps to be activated as desired UP TAKEOFF or DOWN The flap switch is located on c...

Page 240: ...hen input separately 1 Aileron Rudder Interconnect System Rigging Fig 27 18 A With controls in neutral position locate bracket on center aileron control tube so that the end of bell crank assembly wil...

Page 241: ...ed with the Con trol Horn pointing upward 4 All control surfaces are balanced with the hinge center line and the tip rib chord line level Two tooling holes are located in the tip ribs and are on the r...

Page 242: ...ne is test flown at the factory Should it require readjusting proceed as follows A Locate switch installation on under surface of left wing leading edge and loosen the two phillips head screws one on...

Page 243: ...f the electrical circuitry wiring relays circuit breakers etc are installed from Mooney drawings Components for these are available through your Mooney Service Center The relay for the Electric SpeedB...

Page 244: ...se Flight Inc into wings in accordance with SEC TION 27 96 01 Every 5000 hours 1 Remove the SpeedBrake cartridges in accor dance with SECTION 27 96 01 A Return SpeedBrake cartridges to Precise Flight...

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Page 246: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 28 FUEL...

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Page 248: ...R 28 FUEL LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 28 Effectivity 1 03 17 28 Contents 3 03 17 28 00 00 5 03 17 28 00 01 6 03 17 28 11 00 7 03 17 28 12 00 8 03 17 28 13 00 9 03 17 28 1...

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Page 250: ...rmula Preparation for Leak Check 10 28 14 00 Fuel Additives 10 28 20 00 Distribution 10 28 21 00 Fuel Boost Pump Removal Install 10 28 22 00 Gascolator Screen Cleaning 11 28 23 00 Fuel Injection Syste...

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Page 252: ...s routed back through the fuel selector valve and returned to the source fuel tank FUEL CHECK VENT OUTBOARD OUTLET SCREEN DRAIN LEFT FUEL TANK SELECTOR VALVE FIREWALL INDICATOR FUEL FLOW FUEL FLOW TRA...

Page 253: ...are fully understood Refer to Service Bulletin SB M20 230 for a general concept on resealing tanks 1 Approved Materials A Sealants WARNING Sealants are safe only when handled with reason able care Av...

Page 254: ...continue mixing operation If course particles of accel erator persist after mixing thoroughly reject entire mixed batch CURE RATES a Brushable Type Sealants CLASS A Tack Free Time HOURS Cure Rate HOUR...

Page 255: ...ng an extrusion gun hold gun per pendicular to seam so that extruded sealant will pack tightly 2 Use a spatula to pack sealant firmly in place while working out air pockets Shape each fillet evenly C...

Page 256: ...ncrease in intensity has occurred C A running leak and any leak in a confined area that is not exposed to the air stream should be repaired before the next flight 3 Leak Detection A External Leak Dete...

Page 257: ...leaned area by blowing fil tered air over immediate area until there is nopossibility of solvent or fuel entrapment under adjacent sealant 5 Apply sealant as required for repair See Fig ure 28 4 Repai...

Page 258: ...connect outlet lines at valve body 4 Disconnect both fuel return lines at valve body 5 Remove handle above floorboard in fuel selector pan 6 Remove screws that mount valve to tubular struc ture 7 Remo...

Page 259: ...mitters B Snug each screw then torque each screw to 20 25 IN LBS in a cross flange random order C The torque and screw clamp load will naturally relax as the gasket flows to a normal condition NEVER R...

Page 260: ...lace or rebuild pump Inspect fuel lines and connections for leakage and dam age Fuel selector not in proper position Select proper position Air leak in system Repair leak Refer to Garmin G1000 service...

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Page 262: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 30 ICE PROTECTION...

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Page 264: ...OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 30 Effectivity 1 03 17 30 Contents 3 03 17 30 00 00 5 03 17 30 12 00 6 03 17 30 12 01 7 03 17 30 12 01 8 03 17 30 12 02 9 03 17 30 12 02 10 03 17...

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Page 266: ...0 Servicing Airframe Ice Protection 5 30 11 01 Washing 5 30 11 02 Lubrication 5 30 11 03 Electrical 5 30 12 00 Maintenance Airframe Icing Protection 5 30 12 00 Airframe Ice Protection Electrical Schem...

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Page 268: ...nd retains moisture Residual fluid that is not washed from the aircraft at recom mended intervals can get into skin laps and other fay ing surfaces and hold moisture This may eventually dissolve lubri...

Page 269: ...EEN 3 Repeat procedure with both metering pumps 4 Operate Windshield Spray bar on each windshield pump to ensure proper operation and absence of leaks 5 Filter is located at baggage floor stiffener In...

Page 270: ...AIRFRAME ICING PROTECTION FLUID SCHEMATIC FIGURE 30 2 30 12 01 TROUBLESHOOTING AIRFRAME ICING PROTECTION TROUBLE PROBABLE CAUSE REMEDY Airframe Propeller system does not operate Tank contents inadequ...

Page 271: ...ch With no pressure applied continuity should exist through connections in use LOW PRESSURE WARNING LEDs FLASH RED When system selected ON Check System for proper operation Connect Pin 2 of connector...

Page 272: ...ed to determine the immediate serviceability of the equipment without recourse to the use of tools or special procedures Maintenance Practice Notes Check security and condition of visible components S...

Page 273: ...isplay illuminated and stabilizes at a sensible value within 1 5 minutes Replenish tank contents if necessary If in doubt regarding accuracy of indication make cal ibration check Indicator is electron...

Page 274: ...vel IV Component Checks The following checks are detailed for use in conjunction with SECTION 30 12 01 TROUBLESHOOTING In cases where components can be checked on the aircraft as an alternative to ben...

Page 275: ...ssure at which each operates This pressure should not be greater than 1 5 lbf in2 0 1 bar With the switch at a pressure above the operating pressure there is to be a circuit between Pins 1 2 with a re...

Page 276: ...components be checked out prior to further troubleshooting of Solenoid Valves 1 Check Windshield Pump as detailed above Recon nect Windshield Pump to Solenoid Valve Operate pump by pressing WINDSHIELD...

Page 277: ...tage C1 2 to be 7 5 volts All pins on connector C2 as 1 5 As 1 but with WINDSHIELD 2 selected All pins zero volts except C1 3 9 11 to be aircraft voltage C1 2 to be 7 5 volts All pins on connector C2...

Page 278: ...t side aft fuselage 4 Fill fluid tank to just at overflow with approved de icing fluid This level of fill tops off reservoirs to hold 6 3 gallons of fluid unusable volume of fluid is 0 10 gallon 6 3 g...

Page 279: ...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 30 60 00 PROPELLER DESCRIPTION OPERATION Propeller icing...

Page 280: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE MAINTENANCE MANUAL CHAPTER 32 LANDING GEAR...

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Page 282: ...3 17 32 10 00 6 03 17 32 10 03 7 03 17 32 10 04 8 03 17 32 10 06 9 03 17 32 20 02 10 03 17 32 30 00 11 03 17 32 30 02 12 03 17 32 30 02 13 03 17 32 30 03 14 03 17 32 30 04 15 03 17 32 30 05 16 03 17 3...

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Page 284: ...30 03 Nose Ldg Gear System Rigging 14 32 30 04 Emergency Gear Extension System Rigging 15 32 30 05 Landing Gear Actuator Clutch Spring R R 16 32 30 06 Ldg Gear Act Recoiler Cable Drum R R 18 32 30 07...

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Page 286: ...sengage controls are located aft and between front seats LANDING GEAR WARNING SYSTEM The landing gear warning system provides pilot with a gear warning Voice alert Check Gear that landing gear is not...

Page 287: ...nter mix right and left gear components 12 DO NOT attempt to repair any heat treated com ponent of main landing gear assembly 32 10 02 MAIN GEAR INSTALLATION 1 Lubricate wheel bearings retraction link...

Page 288: ...nnect outboard and mid gear doors and check that doors are faired with wing skin wheel well opening and that there is no binding or distortion where links attach to door Adjust linkage spacers if requ...

Page 289: ...tend or retract landing gear until points A B and C are in alignment as shown in Figure 32 6 Verify that Stop Bolt of Stop just contacts Arm on Bell crank A If contact puts no load on Rod A then proce...

Page 290: ...AN3 bolt at rod end and AN4 bolt at block remove bungee assembly INSTALLATION 1 Raise aircraft on jacks See Section 7 10 00 2 Compress replacement bungee 250 lbs to align installation rig pin holes In...

Page 291: ...be properly rigged prior to gear door rigging see Section 32 30 01 2 Adjust gear door link rods RH and LH Fig 32 10 to insure snug closure with zero preload CAUTION Nose gear overcenter preload must...

Page 292: ...ht comes ON Gear switch in DOWN position C Measure nose gear bungee springs Fig 32 11 Deflection from zero load condition in A above must be 030 to 070 inches for each bungee D If spring deflection is...

Page 293: ...ect springs On inboard door bellcranks disconnect springs Loosen jamb nut X on retraction tube V Fig 32 1 and back off pressure on spring W by loosening nut Y Disconnect retraction tube V from bellcra...

Page 294: ...0252 011 Shims with 560252 009 Stop to achieve proper clearance Use 063 longer screws with each additional shim Secure screw with Blue Loctite 83 31 Grade C 18 Run actuator down and recheck retraction...

Page 295: ...t 4 breaks open slightly insert shim stock 005 to 008 in thickness between retraction link and truss at P then release force on torque wrench 32 While applying a pulling force on the shim stock exert...

Page 296: ...partially retract landing gear release switch 8 Turn Master Switch OFF 9 Pull landing gear actuator C B OUT 10 Screw each nose gear retraction tube F Fig 32 8 IN clockwise looking toward the front of...

Page 297: ...erify manual extension system is engaged Resistance should be felt at once 6 Replace T handle under RED lever and return RED lever to disengage position down and latched Manual extension system is now...

Page 298: ...r 6 can be rotated in either direction and small output gear 10 will follow rotation direc tion 5 Lubricate output gear teeth 10 with MIL G 81322 and install clutch housing gear and spring assembly in...

Page 299: ...and previously re moved spacers 4 Install new recoiler springs placing a spacer be tween each spring and over top spring IMPORTANT Recheck proper installation of springs NOTE When looking at recoiler...

Page 300: ...anding gear actuator C B will pop out CAUTION DO NOT continue to pull T Handle after GEAR DOWN light is ON Actuator may bind on Down Stops 32 30 08 FINAL CHECKS 1 Raise and lower landing gear through...

Page 301: ...al DOWN STOPS Gear may have been extended manually ball nut is jammed tight against STOPS on motor use wrench on ball nut flat to move from STOPS Gear will not retract and gear ac tuator C B trips Man...

Page 302: ...N NUT TYP 3 PLCS MAIN TIRE SPACER DUST SHIELD LANDING GEAR WHEEL REMOVAL FIGURE 32 18 WARNING Do not loosen wheel half retaining nuts be fore tire is completely deflated Failure to ob serve this warni...

Page 303: ...2 Remove nose wheel 3 Installation is in reverse sequence of removal Nose wheel disassembly 1 Completely deflate tire by removing valve core 2 Remove nuts washers and wheel half retaining bolts 15 Fig...

Page 304: ...le to use compressed air applied to the brake line fitting to re move the piston 10 from the brake cylinder CAUTION Do not spin bearing cones with compressed air G Clean parts in cleaning solvent and...

Page 305: ...ISASSEMBLY Fig 32 21 NOTE Aircraft have large capacity Master Cylinders installed A Remove left hand lower fuselage skin aft of fire wall and exhaust cavity B Disconnect hydraulic cylinder from pedal...

Page 306: ...4 10 11 9 O RING P N 9 10 11 MS28775 012 N507 90 006 MS28775 010 REF PARKING BRAKE VALVE FIGURE 32 22 5 Shuttle Valve Maintenance A No maintenance authorized Remove and re place shuttle valve assembly...

Page 307: ...d nose gear assembly 720095 15 arm should not contact 720095 17 shaft in full left travel It is cause for rejection if binding occurs Next Run nose gear assembly through full right travel and hold mea...

Page 308: ...ower detente low ers the gear The down limit switch will stop the gear ac tuating motor when the proper force is exerted to hold the gears in the down and locked position Refer to Section 32 30 02 for...

Page 309: ...sc replacement tool C P N GSE 030038 501 Green color to remove and install main gear shock discs Use removable pad from tool as a guide on top of shock link to align discs as they are be ing compresse...

Page 310: ...GEAR SHOCK DISC REPLACEMENT FIGURE 32 28 32 82 00 RECOMMENDED HARD LANDING IN SPECTIONS The following are areas recommended to be inspected when a hard landing or overweight landing has oc curred Sinc...

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Page 312: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 33 LIGHTS...

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Page 314: ...Rev Date CHAPTER 33 LIGHTS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 33 Effectivity 1 03 17 33 Contents 3 03 17 33 00 00 5 03 17 33 10 00 6 03 17 33 10 01 7 03 17 33 23 00 8 03 17 33...

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Page 316: ...n Light Switch Replacement 7 33 22 00 Instrument Flight Panel and Glareshield Lights 7 33 22 01 Light Bulb Replacement 7 33 23 00 Gear Down Indicator Light Floorboard 8 33 23 01 Light Bulb Replacement...

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Page 318: ...tch in either the ON AND OFF position and is controlled by momentary switches magnet mounted in both cabin door frames The switch is ener gized when any door is opened This light will automati cally t...

Page 319: ...he O H switch panel to the headliner Figure 33 1 2 Switches are a snap fit and may be removed by pressing snap tabs and pushing switch through cover 3 Disconnect wires from Electroluminescent panel ha...

Page 320: ...h assembly into mounting hole BAGGAGE COMPARTMENT SWITCH 1 Switch is located at rear of baggage door at front top of hat rack opening Figure 33 1 2 Remove one screw inboard of switch on door frame tri...

Page 321: ...EDY STROBE LIGHTS Lights inoperative Circuit breaker switch tripped Check for short circuit Reset circuit breaker Loose connection Check and tighten electrical con nections Battery defective Replace b...

Page 322: ...hen check for shorted power leads blown inline fuses or circuit breaker If input voltage is present disconnect connector to flashtube 400 500VDC should be pres ent across Pin 1 and 3 of power supply I...

Page 323: ...mately 1 2 and lift upwards to remove CAUTION Do not touch the LED lens surface with either fingers or sharp objects This could soil and or damage the lens and affect the optical per formance of the L...

Page 324: ...f nose wheel 7 ft 6 in from wall Position L H R H main landing gear at exact distance from vertical wall i e parallel to wall 2 Place four target crosses on vertical wall at the following positions A...

Page 325: ...l from your hands or other maintenance processes Failure to wear clean gloves or wiping the bulb off may result in pre mature bulb failure due to hot spots that will build up from any grease residue o...

Page 326: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 34 NAVIGATION AND PITOT STATIC...

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Page 328: ...ev Date CHAPTER 34 NAVIGATION LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 34 Effectivity 1 03 17 34 Contents 3 03 17 34 00 00 5 03 17 34 10 00 6 03 17 34 12 00 7 03 17 34 20 00 8 03 17 3...

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Page 330: ...d Indicator G1000 7 34 12 00 Vertical Speed Indicator 7 34 13 00 Altimeter 7 34 13 00 Altimeter SAM 7 34 13 00 Altimeter G1000 7 34 13 01 Altimeter Troubleshooting 7 34 20 00 Horizontal Situation Indi...

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Page 332: ...MD302 series Standby Atti tude Module known as the SAM is a self contained situational awareness instrument that provides aircraft attitude altitude airspeed and slip indication in an ad vanced 2 inc...

Page 333: ...he INSTRUMENT panel to do so will serious ly damage instruments When blowing back through line from instrument panel make sure that no air is blown into instruments 4 Static system leak test The stati...

Page 334: ...nots Speed indication starts at 20 knots with 60 knots of airspeed viewable at any given time The actu al airspeed is displayed inside a black pointer The pointer remains black until reaching never ex...

Page 335: ...with a simple turning of the control knob while in Flight Mode When adjusting the barometric pres sure the window will increase in size and the digits will turn green When finished setting the pressur...

Page 336: ...ISPLAY G1000 The G1000 Slip Skid indicator a component of the Atti tude Indicator screen display resides beneath the roll pointer The indicator moves with the roll pointer and moves laterally away fro...

Page 337: ...E F and G H When heading error is reduced to less than 15 install compass and proceed to Step 4 Compass Swinging 4 Compass Swinging A Run engine at 1200 to 1500 RPM and proceed to swing compass with r...

Page 338: ...of graduations representing pitch angles of every 5 with every 10 graduation extended and numbered The unit is oper able and usable in a continuous and unlimited pitch range of 360 A series of chevro...

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Page 340: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 35 OXYGEN...

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Page 342: ...APTER SECTION SUBJECT PAGE DATE 35 Effectivity 1 03 17 35 Contents 3 03 17 35 00 00 5 03 17 35 00 01 6 03 17 35 00 02 7 03 17 35 00 03 8 03 17 35 00 03 9 03 17 35 00 03 10 03 17 35 00 03 11 03 17 35 0...

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Page 344: ...ABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 35 00 00 General Precise Flight Oxygen System 5 35 00 01 Precise Flight Oxygen System Components 6 35 00 02 Precise Flight Oxygen System Maintenance 7 35...

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Page 346: ...verhead distribution manifold with low pres sure transducer and integrated interior LED dome light located just aft of the pilots seats and in front of the passenger seats in the overhead panel 7 Brea...

Page 347: ...selection of oxygen in the aircraft cabin Oxygen Distribution Manifold 1 Allows the crew and passengers to connect to the Oxygen System with four 4 quick disconnect fittings with the capability of se...

Page 348: ...egulator assembly aft end of the bottle first 7 Installation is opposite of removal Tighten wing nuts until snug and then two more turns to ensure prop er tension on clamp bolt 8 Perform a functional...

Page 349: ...ns before applying air craft battery power 2 Fill Oxygen System with aviators oxygen 3 Switch the Oxygen System ON at the oxygen con trol panel and verify that the Oxygen System quantity display indic...

Page 350: ...SELAGE PANEL OXYGEN FILLER VALVE OXYGEN TANK PURITAN BENNETT CONNECTION PRECISE FLIGHT OXYGEN SYSTEM FILL VALVE FIGURE 35 6 TAILCONE ASSY BAGGAGE WALL BOTTLE ASSY BAND CLAMP NUT MOUNTING HARDWARE GROU...

Page 351: ...altitudes SpO2 decreases due to less oxygen available because of the decrease in air pressure Physical exertion at high altitude may be difficult because of the reduced oxygen level DISPLAY LOGIC CON...

Page 352: ...ation check 1 Remove the Pilot Seat if not already removed as part of the annual maintenance check cabin group 2 Remove the RH Center Trim Panel if not already removed as part of the annual maintenanc...

Page 353: ...lashing amber LED Note the altitude which this oc curred 9 Verify the altitude where the indication first oc curred a If indication is between 11 500ft PA and 12 500ft PA then proceed to the next step...

Page 354: ...s Greater than 700 Yes Blinking Yes 2 PRECISE FLIGHT OXYGEN SYSTEM TROUBLE SHOOTING FLOW CHART 1 FIGURE 35 12 Re Fill Oxygen System to Over 1500 psig Re Adjust All Flowmeters to Correct Setting No Yes...

Page 355: ...nstalled at the Solenoid the reading should be 0 75 ohm at the DLA D Sub Connector No Yes PRECISE FLIGHT OXYGEN SYSTEM TROUBLE SHOOTING FLOW CHART 3 FIGURE 35 14 Install a New Mark the Bottle Yes Yes...

Page 356: ...oid Wire to Ground is 11 3 VDC Solenoid Wire to Ground OK Solenoid Failure Remove and Replace the Regulator Bottle Assembly Purge the Oxygen System per Section 2 4 6 Mart Regulator Bottle Assembly wit...

Page 357: ...r will engage the latching solenoid and turn on the Oxygen flow 2 6 6 6 4 Wiring OK Check Low Pressure Transducer Wiring Fix Wiring between the Display Logic Assembly and the Low Pressure Transducer T...

Page 358: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date Page 17 PRECISE FLIGHT OXYGEN SYSTEM WIRING SCHEMATIC TYPICAL FIGURE 35 18 35 00 04...

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Page 360: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 37 VACUUM...

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Page 362: ...ON M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 37 VACUUM LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 37 Effectivity 1 03 17 37 Contents 3 03 17 37 00 00 5 03 17 37...

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Page 364: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 37 VACUUM TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 37 00 00 General 5 37 CONTENTS...

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Page 366: ...ONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date Page 5 37 00 00 GENERAL Garmin G1000 equipped aircraft are all electric with no vacuum system requirements on the standard a...

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Page 368: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 39 ELECTRICAL PANELS...

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Page 370: ...T OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 39 Effectivity 1 03 17 39 Contents 3 03 17 39 00 00 5 03 17 39 00 00 6 03 17 39 10 00 7 03 17 39 10 00 8 03 17 39 10 01 9 03 17 39 10 01 10 03 17...

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Page 372: ...1 Flight Instruments 9 39 10 02 Circuit Breaker Panel 11 39 10 03 Control Wheels 12 39 11 00 Flight Instrument Panel 13 39 11 01 Landing Gear Switch 13 39 11 02 Landing Gear Safety Override Switch 13...

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Page 374: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date Page 5 GARMIN 1000 INSTRUMENTS AND CONTROL PANEL TYP FIGURE 39 1 39 00 00...

Page 375: ...lide Slope signals The primary function of the GPS portion of the system is to acquire signals from the GPS satellites recover orbital data make range and Doppler measurements and process this informa...

Page 376: ...lashing pull 90A BAT circuit breaker and PUSH EMERG BUS switch ON to bring Stand by Alternator online 12 STROBE LIGHT SWITCH Strobe light switch turns wing tip and tail strobe lights ON 13 NAVIGATION...

Page 377: ...h altitude conditions Low boost may also be used as an engine starting aid Con tinuous operation of the low boost is permitted Never run the boost pump without fuel in the sys tem CAUTION Pushing LOW...

Page 378: ...of cabin heat control is described in the Cabin Environment Section 38 DEFROST CONTROL Pull defrost control to decrease air flow to lower cabin area and increase air flow to windshield ducts in the fr...

Page 379: ...e wire dis connects for glareshield lights Disconnect wires and lift glareshield off B Refer to the Garmin Installation and Mainte nance Instructions for each Garmin component to be removed installed...

Page 380: ...RVO CABIN AREA GEA HARNESS AREA TIT EGT CHT INSTALLATION LOOM HARNESS GDC 74 AIR DATA FORWARD HARNESS ASSY FWD TO GDC74A AFT TO GRS77 FORWARD AFT DISCONNECT GRS77 WX500 FORWARD AFT DISCONNECT AFT HARN...

Page 381: ...center 2 screws These 2 screws have 2 spacers that will re lease and be reused upon assembly see Figure 39 4 E Remove lower 1 screw from rear lower corner face of circuit breaker panel Note a clip nut...

Page 382: ...ilot seat Each Control Wheel may contain controls for Trim Adjust Identifica tion Transponder Autopilot Disconnect Control Wheel Switches Speed Brake Microphone Switch Map Light and Stormscope Refresh...

Page 383: ...d by removing two attachment screws and pushing switch forward through panel or by sliding it aft from panel There is a common bus bar on some switches that will require loosening or removal for switc...

Page 384: ...1000 Avionics System 39 12 00 EMERGENCY LOCATOR TRANSMIT TER ELT SWITCH ARTEX ME 406 ELT The Artex ME 406 remote ELT switch Figure 39 12 is located on the Instrument Panel The location is de termined...

Page 385: ...the COSPAS SARSAT satellites Transmitter Test Always perform the tests within the first 5 minutes of the hour Notify any nearby control tower of your intentions in accordance with AC 43 13 1B Section...

Page 386: ...chassis The battery cells components and connectors should be free of corrosion Inspect flex circuit for broken con nections or damage Ensure the battery housing is free of cracks or other visible dam...

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Page 388: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 51 STRUCTURES...

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Page 390: ...17 51 Contents 3 03 17 51 00 00 5 03 17 51 10 01 6 03 17 51 11 00 7 03 17 51 12 01 8 03 17 51 12 01 9 03 17 51 12 02 10 03 17 51 12 03 11 03 17 51 13 02 12 03 17 51 13 03 13 03 17 51 13 03 14 03 17 51...

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Page 392: ...pair 13 51 13 04 Rear Spar Repair 15 51 13 05 Rib Repair 15 51 13 06 Wing Tip Repair 15 51 13 07 Wing Skin Panel Repair 15 51 14 00 Horizontal Stabilizer Vertical Fin Repair 17 51 14 01 Leading Edge S...

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Page 394: ...h are at tached to floorboard and structure beneath floorboard The M20V features two rear passenger seat configura tions a split type rear seat using seat cushions in molded wells over wing spars and...

Page 395: ...E 51 2 2 RIVET REMOVAL AND REPLACEMENT A REPLACEMENT STANDARD SIZE RIVETS HOLE OVERSIZE This repair applies only to original aluminum alloy steel or monel rivets of 1 16 3 32 1 8 and 5 32 inch diamete...

Page 396: ...470AD3 or AN426AD3 40 0 098 dia 0 108 in AN470AD4 or AN426AD4 30 0 1285 dia 0 141 in MAXIMUM ALLOWABLE DIAMETRIC DIMENSIONS FIGURE 51 4 3 When a hole becomes enlarged beyond ac ceptable diametric limi...

Page 397: ...es weld hole or dent and file repaired surface smooth Form a patch that will cover twice the diameter of tube from both edges of damaged area and twice the circumferential area of damage as shown in F...

Page 398: ...epair a damaged tube when parts on each side of the damage cannot be separated to insert an in ner sleeve Figure 51 7 A Form split sleeve from steel tube or sheet steel when outside diameter of origin...

Page 399: ...that will clean up with a 20 drill may be drilled and repaired per item A C The repair of weld beads on heat treated as semblies may be accomplished without reheat treat ment within the following limi...

Page 400: ...ged primary control system compo nent with a new part Repairing primary control system components is not recommended Use only new hard ware when installing new parts After installation of new parts ch...

Page 401: ...lt is too short the shank will not completely fill hole Repair scratches on spar caps that are not deeper than 003 inch by sanding with No 400 abrasive paper Re move no more than 005 inch of material...

Page 402: ...STUB SPAR REPAIR Stub spar splice at wing STA 34 5 3 0 1 Cut stub spar halfway between existing rivets as required by damage incurred Figure 51 13 2 Smooth all rough or sharp edges and prime area to b...

Page 403: ...AD 050 503 PLATE 18 AN 470 AD5 RIVETS EACH SIDE OF SPLICE 503 REF W S 43 5 20 0 COND N STEEL 503 FLAT PATTERN 040 AISI 4130 COND N STEEL 501 FLAT PATTERN 091 AISI C 130 28 0 1 56 74 1 07 1 66 SECT A A...

Page 404: ...k CR 2248 blind rivets in places inaccessible for rivet bucking Add one extra counter sunk blind rivet between every other pair of cherrylock rivets 51 13 07 WING SKIN PANEL REPAIR Repair wing skin pa...

Page 405: ...Cracks that extend through face of dimple into surrounding skin can be repaired as fol lows A Stop drill crack with No 60 bit B Cut doubler from same material as skin to be re paired Allow for six ri...

Page 406: ...SAME LENGTH AS 75 070 050 SPAR REPAIR SAT 9 0 OUTBD FIGURE 51 20 2 Repair main spar cap damage between STA 34 and STA 48 5 by forming a splice angle from 3 4 inch by 3 4 inch 050 2024 T3 sheet aluminu...

Page 407: ...GE SET 5 6 STRAIGHT HUCK STUMP STUMP DRIVE HUCK STEP 1 SWAGE SET RIVET GUN SWAGE SET BENT 5 HUCK COLLAR RIVET GUN INSTALL STEP 2 COLLAR BUCKING BAR COLLAR SWAGE STEP 3 REMATING HORIZONTAL STABILIZER T...

Page 408: ...te chamfer and size will vary based on accessibility shape of part and the ex tent of damage 51 15 01 CRACKS IN SURFACE AREAS 1 Stop drills all cracks per standard aircraft proce dure 2 Remove any loo...

Page 409: ...amps tape or temporary rivets 8 Mix the resin according to the manufacturer s data sheet for proper mix ratio the effective working pot life the normal cure temperature cure parameters and other instr...

Page 410: ...rivets Flush heads to be on fin ished surface side Number of rivets and spacing will be determined by size of repair 7 Apply one additional overlapping layer of 181 fi berglass cloth on non finished s...

Page 411: ...the repaired area while still wet This prevents adhesion to the pressure clamp application paragraph 6 6 Place rigid aluminum plates on both sides of repair area and clamp into place with C clamps Per...

Page 412: ...an dard practices 51 16 00 CARBON FIBER REPAIR The upper and lower cowl assembly base material is preimpregnated fiber reinforced composite laminate carbon fiber prepreg Superficial damage may be buff...

Page 413: ...es following the illustration depicting the as sembly or component in question If splices are made the system must be checked for leaks 3 Shortening and Lengthening of Tubing Hoses and Flexible Ductin...

Page 414: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 52 DOORS...

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Page 416: ...NUAL Date MAR 2017 Rev Date CHAPTER 52 DOORS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 52 Effectivity 1 03 17 52 Contents 3 03 17 52 00 00 5 03 17 52 10 00 6 03 17 52 10 01 7 03 17 52...

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Page 418: ...bin Door s Maintenance Practices 5 52 10 01 Cabin Door s Removal 7 52 10 02 Cabin Door s Seal 7 52 10 03 Cabin Door s Installation Trimming 7 52 10 04 Cabin Door s Latching Mechanism 7 52 10 05 Cabin...

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Page 420: ...losed properly The auxiliary exit handle is located inside baggage door This handle can be operated from inside even if outer handle is locked A cam mechanism allows a cle vis pin to bypass outer hand...

Page 421: ...INSIDE DOOR HANDLE DOOR HINGES INNER DOOR SHELL REF OUTER DOOR SHELL REF 11 ILLUSTRATION SHOWS BOTH HALVES APART FOR CLARITY RIVETS CLEVIS PIN WASHER COTTER PIN BRACKET MOUNTING SCREWS CONTROL CABLE...

Page 422: ...ges of door shell carefully while door is test fitted in place opening and closing It may take several trimmings to establish the door fit ment Door should have even spacing and flush fit around door...

Page 423: ...is pin into position on bellcrank install washer and new cotter key K Install upper door link and secure with removed clevis pins washers and new cotter pins on both sides of link assembly 52 10 05 CA...

Page 424: ...an of old sealant and debris B Push in on door assembly at top while door is in latched position to properly locate door and seal in door frame C While door is held in place mark holes in new hinge us...

Page 425: ...p is removed or replaced REMOVABLE STEPS IF INSTALLED Aircraft equipped with removable steps may have it removed or installed by a certified aircraft mechanic If the steps are installed decrease the t...

Page 426: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 53 FUSELAGE...

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Page 428: ...Rev Date CHAPTER 53 FUSELAGE LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 53 Effectivity 1 03 17 53 Contents 3 03 17 53 00 00 5 03 17 53 20 00 6 03 17 53 20 00 7 03 17 53 30 00 8 03 17 53...

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Page 430: ...S CHAPTER SECTION SUBJECT PAGE 53 00 00 General 5 53 10 00 Main Frame 5 53 10 01 Tubular Structure Frame 5 53 30 00 Plates Skins 6 53 10 02 Tailcone Structure 8 53 20 00 Firewall 8 53 40 00 Attach Fit...

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Page 432: ...r corrosion protection The tailcone bulkheads formers skins etc are formed from sheet aluminum on either a hydro press or drop hammer These components along with string ers clips brackets etc are posi...

Page 433: ...integral part of tail cone structure Repair or replacement of these skins should be according to AC 43 13 1 Chap 2 Sect 3 The fuselage assembly and tailcone have panels cov ers or doors at various lo...

Page 434: ...RUDDER CONTROLS ELEVATORS RUDDER BELLCRANKS 11 BRAKE MASTER CYLINDERS ELECTRIC FUEL PUMPS 12 LANDING GEAR ACTUATOR GASCOLATOR FUEL SELECTOR VALVE 13 LANDING GEAR RERACT TUBES 14 ELECTRIC FLAP ACTUATO...

Page 435: ...onocoque construction The internal structure is shown on Figure 53 4 The forward cabin structure 1 is bolted to tailcone with eight structural bolts 8 The tailcone skin 2 is an inte gral load bearing...

Page 436: ...5 NAS1149F0463P WASHER 5 NAS1149F0432P WASHER 5 NUTS TO BE ON OUTBOARD SIDE TYP BOTH SIDES AN4 20A BOLT 1 NAS1149F0463P WASHER NAS1149F0432P WASHER MS21045L4 NUT 1 AN4 17A BOLT 1 AN3 4A BOLT 8 MS21045...

Page 437: ...structural bolts bushings and nuts passing through two top hinges The bottom attach point on empennage assembly secures stabilizer trim jack screw Lateral stability of empennage assembly is controlled...

Page 438: ...D BOTH PLACES HINGE PIN COTTER PIN TRIM LINK WASHER SHIM NUT WASHER WASHER BUSHING BOLT BOLT WASHER NUT BOLT WASHER WASHER NUT REF MOUNTING CLIP REF VARIABLE DOWN SPRING ROD NOTE THERE ARE SMALL SHIMS...

Page 439: ...igure 53 8 are for NAS1304 bolts installed for ten sion loads Lower hard points 3 are for shear loads and are used in conjunction w attachment of nose landing gear lower truss assembly Figure 53 8 AN6...

Page 440: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 55 STABILIZERS...

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Page 442: ...MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 55 STABILIZERS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 55 Effectivity 1 03 17 55 Contents 3 03 17 55 00 00 5 03 17 55 10 01 6 03 17...

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Page 444: ...5 55 10 01 Horizontal Stabilizer Removal 6 55 10 02 Horizontal Stabilizer Installation 6 55 20 00 Elevator 6 55 20 01 Elevator Removal 6 55 20 02 Elevator Installation 6 55 30 00 Vertical Stabilizer...

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Page 446: ...der have balance weights per manently installed for stabilization during flight 9 9 8 7 9 8 9 8 5 9 8 8 7 11 12 7 6 4 3 2 9 1 10 9 HORIZONTAL STABILIZER FIGURE 55 1 55 10 00 HORIZONTAL STABILIZER The...

Page 447: ...tor There are no ribs in ele vator between inboard and outboard ribs The skins are attached to leading edge extrusion 5 and ribs 6 with blind rivets Each formed corrugation is matched on top and botto...

Page 448: ...ed together at trailing edge The rudder lower skins 3 are drop hammer formed left and right halves riveted to upper skins rib assembly 4 and at leading and trailing edge A stiffener 5 is to support lo...

Page 449: ...ONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date Page 8 DETAIL B DETAIL A 5 6 22 7 4 3 5 7 16 2 12 1 12 12 14 13 10 11 8 9 7 RUDDER ASSEMBLY FIGURE 55 4 55 40...

Page 450: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 56 WINDOWS...

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Page 452: ...ND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 56 WINDOWS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 56 Effectivity 1 03 17 56 Contents 3 03 17 56 00 00 5 03 17 56 21 02 6 03 17 5...

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Page 454: ...CT PAGE 56 00 00 General 5 56 00 01 Cleaning Acrylic 5 56 20 00 Windshield and Cabin Windows 5 56 21 00 Windshield 5 56 21 01 Windshield Removal 5 56 21 02 Windshield Installation 6 56 22 00 Cabin Win...

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Page 456: ...visible finish the plastic with a good grade of commercial wax Apply the wax in a thin even coat and bring to a high polish by rubbing lightly with a soft cloth 3 Polishing Do not attempt hand polishi...

Page 457: ...WITH PLEXIGLASS SCRAPER FIGURE 56 2 c Remove both dash panels 2 Removal of Windshield a Have one person inside the cockpit to gently push outward on the windshield while two other people on the exter...

Page 458: ...HEMICALS OR SOLVENTS Dam age may result if drops of solvents come in con tact with either exterior paint composite shell interior trim or acrylic surfaces It is permissible to use isopropyl alcohol a...

Page 459: ...re 56 11 and Figure 56 7 APPLY SEALANT WITH SEALANT GUN APPLY SEALANT TO CHANNEL FIGURE 56 7 e Smooth the line of sealant with a wooden tongue depressor f Using two people lower the windshield onto th...

Page 460: ...lant with a sealant gun around the rim of the windshield m Smooth the line of sealant with a wooden tongue depressor n Let the sealant dry according to the application directions on the sealant tube A...

Page 461: ...er bonding rod This rod is used to create a uniform sealant gap and to allow acrylic glass to be flush with outer shell Sufficient sealant should be used so excess sealant is extruded from all edges o...

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Page 463: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 57 WINGS...

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Page 465: ...Rev Date CHAPTER 57 WINGS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 57 Effectivity 1 03 17 57 Contents 3 03 17 57 00 00 5 03 17 57 10 00 6 03 17 57 10 00 7 03 17 57 20 00 8 03 17 57 3...

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Page 467: ...stallation 5 57 00 02 Stall Strip Installation 5 57 10 00 Main Frame 5 57 20 00 Auxiliary Structures 8 57 20 01 Jack Points 8 57 20 02 Wing Tips 8 57 30 00 Plates Skin 9 57 40 00 Attach Fittings 10 57...

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Page 469: ...der control tubes f Elevator control tube g Elevator and rudder push pull tubes h Floorboards at rear attach points i Belly skin stringer splice angles j Airspeed indicator line pitot lines and pitot...

Page 470: ...F0463P WASHER NAS1149F0432P WASHER MS21045L4 NUT 1 AN4 17A BOLT 1 AN3 4A BOLT 8 MS21045L3 NUT 8 NAS1149F0363P 8 TYP BOTH SIDES TUBULAR STRUCTURE REF STUB SPAR REF MAIN SPAR REF TUBULAR STRUCTURE REF M...

Page 471: ...140 AN 7 450 500 WING ATTACHING HARDWARE CHART FIGURE 57 2A LEFT WING SHOWN RIGHT WING OPP STA 43 5 RIB RIVET LINE STA 60 12 FWD 2 0 A SKIN STALL STRIP A AN520 6 7 SCREW AN345 6 NUT AN960 6 WASHER FWD...

Page 472: ...24 5 WS 43 5 WS 59 25 WS 74 0 WS 88 75 WS 103 5 WS 118 25 WING STRUCTURE FIGURE 57 3 57 20 02 WING TIPS The M20V wing tips are non structural fiberglass com ponents They are riveted to upper and lowe...

Page 473: ...ntervals are secured with screws Any access covers that are riveted in place are required for manufacturing only and NOT for routine inspections 4 1 2 3 5 8 10 9 6 13 15 14 12 11 18 20 17 16 7 7 7 7 7...

Page 474: ...repairs are approved for the main landing gear assembly NOTE Heat treated components should NOT be re paired replace them 57 50 00 FLIGHT SURFACES Refer to Section 27 90 00 for flight control surface...

Page 475: ...4 3 4 FLAP ASSEMBLY FIGURE 57 7 57 50 21 AILERON REMOVAL AND INSTALLATION Refer to Section 27 10 00 for removal installation balancing procedures NOTE The following rivets are to be used when replac...

Page 476: ...8 7 10 DETAIL B BOLT NAS70CL261 500 WASHER WASHER SEE NOTE 1 WASHER NUT BOLT WASHER SEE NOTE 1 WASHER NUT WASHER BOLT WASHER COTTER PIN WASHER DETAIL A NUT DETAIL C NOTE COUNTERSINK TOWARDS HEAD OF BO...

Page 477: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 61 PROPELLERS...

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Page 479: ...ev Date CHAPTER 61 PROPELLERS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 61 Effectivity 1 03 17 61 Contents 3 03 17 61 00 00 5 03 17 61 00 20 6 03 17 61 10 00 7 03 17 61 10 10 8 03 17 6...

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Page 481: ...UBJECT PAGE 61 00 00 General 5 61 00 10 Spinner Dome and Propeller Removal 5 61 00 20 Propeller Installation 6 61 10 00 Propeller Assembly 7 61 10 10 Minor Propeller Blade Repair 8 61 20 00 Propeller...

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Page 483: ...e nance inspection procedures and time intervals CAUTION Refer to Hartzell Service Letter 61 for most current overhaul Time Between Overhaul limits NOTE Approved propeller shops ONLY are authorized fo...

Page 484: ...4 HARTZELL 3 BLADE PROPELLER INDEXING FIGURE 61 2 The propeller flange has six 1 2 inch studs configured in a four inch circle Figure 61 2 Two dowel pins are also provided to transfer torque and inde...

Page 485: ...he spinner is installed 1 Examine the interior of the spinner dome The spinner dome has an internal support Figure 61 1 that encircles the propeller cylinder The cylinder may need to be wrapped with o...

Page 486: ...n accordance with the applicable Hartzell overhaul manual CAUTION Over lubricating may cause the grease to enter the hub cavity leading to excessive vibration and or sluggish operation The propeller m...

Page 487: ...to be used for final finishing Refer to Figure 61 5 3 Repaint area per propeller manufacturer s recom mendations to reduce corrosive action 61 20 00 PROPELLER CONTROLLING 61 20 10 PROPELLER GOVERNOR C...

Page 488: ...e at least three times to purge air from the pro peller hydraulic system and to introduce warmed oil to the cylinder NOTE Pitch change response on the first operation from low to high blade pitch may...

Page 489: ...f vibration in creasing with RPM Vibration problems that occur in a narrow RPM range are a symptom of res onance which is potentially harmful to the propeller Avoid op eration until the propeller can...

Page 490: ...OTE Hartzell recommends that new or newly overhauled propellers be lu bricated after the first one or two hours of operation because centrif ugal loads will pack and redistrib ute grease which may res...

Page 491: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 71 POWERPLANT...

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Page 493: ...CHAPTER SECTION SUBJECT PAGE DATE 71 Effectivity 1 03 17 71 Contents 3 03 17 71 00 00 5 03 17 71 00 20 6 03 17 71 00 40 7 03 17 71 00 50 8 03 17 71 00 50 9 03 17 71 00 50 10 03 17 71 00 51 11 03 17 71...

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Page 495: ...p 8 71 00 52 Engine Set Up Control Rigging 13 71 00 60 Fuel Injection System Maintenance 13 71 00 70 Starter System Maintenance 13 71 00 80 Engine Mixture Control Rigging 13 71 00 90 Starter Trouble S...

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Page 497: ...nected 1 Make sure all cockpit switches are OFF 2 Turn fuel selector valve OFF 3 Remove engine cowling see Section 71 10 00 4 Disconnect battery ground cables 5 Remove propeller refer to section 61 00...

Page 498: ...e required to slide the crossover pipe assembly rearward off of the slip joints to prevent binding at the slip joints 21 Slide crossover pipe off of wastegate A slip joint is located between the cross...

Page 499: ...inch lbs 1 4 inch lower mount bolt torque 50 to 70 inch lbs Re inspect to see that 1 Propeller and spinner are properly torqued 2 Engine mounting bolts are properly torqued 3 Engine controls are prope...

Page 500: ...return Magneto Start Switch to BOTH Retard throttle Slowly advance mix ture to FULL RICH Adjust as needed for elevation 6 Hot Starts Same procedure as Normal Starts except A Mixture IDLE CUT OFF B Pr...

Page 501: ...tion side hose the the tee installed in the upper deck pressure line installed in Step F H Torque all connections according to Appendix B specifications of the CMI TSIO 550 Service and Main tenance Ma...

Page 502: ...ma tion Directive SID97 3 G or latest revision M O Stan dard practice Maintenance Manual and the M 18 Ser vice and Overhaul Manual for specific Engine Operating Limits NOTE Mixture and propeller contr...

Page 503: ...17 Rev Date Page 11 H FORWARD LOW UNMETERED FUEL PRESSURE SLOPE CONTROL ADJUSTMENT HIGH FUEL PRESSURE ADJUSTMENT ADJUSTMENT ENRICHEN MIXTURE INCREASE INCREASE INCREASE INCREASE IDLE SPEED ADJUSTMENT I...

Page 504: ...UAL Date MAR 2017 Rev Date Page12 MAN MAP UMTD UNMETERED FUEL PRESSURE TBD UPPER DECK PRESSURE MTD METERED FUEL PRESSURE UMTD UNMETERED FUEL PRESSURE TBD UPPER DECK PRESSURE MAN MAP MTD METERED FUEL P...

Page 505: ...cap an plug on throttle body and manifold valve and conduct a leak check of all connec tions Ensure all hoses are correctly reconnected Re move footwell fitting adapter and replace with footwell cover...

Page 506: ...s at all four locations Keep heat shield and mounting hardware lift engine to allow removal of all four upper engine isolator mounts and hardware Inspect Heli Coils in engine legs for any damage i e c...

Page 507: ...6 LORD MOUNT J 9612 44 HEAT SHIELD 600532 1 WASHER 600364 7 BOLT NAS 6607 48 WASHER 600364 7 HEAT SHIELD 600394 7 WASHER Y 13748 532 WASHER 600364 5 LORD MOUNT J 7763 53 LORD MOUNT J 7763 53 KIT J 776...

Page 508: ...nderneath fireseal with Coast Pro Seal 700 or equivalent on engine side of firewall 71 60 00 AIR INTAKES The engine cooling air intakes and exits are calculated for optimum cooling requirements and mi...

Page 509: ...charger Kit P N CP 99 5050 containing oil red in color Begin re oiling the dry filter by applying a bead or line of red oil along the top only of each pleat of the filter The oil will soak into the le...

Page 510: ...N GAP REQD BETWEEN ACTUATOR ROD DOOR ASSY WITH CONTROL KNOB IN CLOSED POSITION 13 IN ANNNCIATOR LIGHT SWITCH MEASURE 4 5 TO 7 5 LBS TO OPEN DOOR HERE REF ANNNCIATOR LIGHT SWITCH REF APPROX RECHARGEABL...

Page 511: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 72 ENGINE...

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Page 513: ...ON M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 72 ENGINE LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 72 Effectivity 1 03 17 72 Contents 3 03 17 72 00 00 5 03 17 72...

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Page 515: ...MOONEY AVIATION COMPANY INC M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 72 ENGINE TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 72 00 00 General 5 72 CONTENT...

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Page 517: ...MAR 2017 Rev Date Page 5 72 00 00 GENERAL 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 i...

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Page 519: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 73 ENGINE FUEL SYSTEMS...

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Page 521: ...NTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 73 ENGINE FUEL SYSTEMS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 73 Effectivity 1 03 17 73 Contents 3 03 17 73 00 00 5 03 17 73 40 00 6 0...

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Page 523: ...APTER SECTION SUBJECT PAGE 73 00 00 General 5 73 10 00 Distribution 6 73 20 00 Controlling 6 73 30 00 Fuel Flow Indicating 6 73 31 00 Panel Mounted Instruments 6 73 31 01 Garmin G1000 6 73 31 02 Fuel...

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Page 525: ...IS ENGINE FUEL PUMP DECK PRESSURE FROM UPSTREAM OF ENGINE THROTTLE IDLE PRESSURE RELIEF VALVE CW TO INCREASE IDLE CUT OFF MIXTURE CONTROL FULL RICH FULL POWER FUEL PRESSURE ADJUSTMENT COUNTER CLOCKWI...

Page 526: ...Valve to OFF C Remove top cowling from aircraft See Section 71 10 00 for procedures D Remove 2 breeze clamps securing firesleeve on both sides of fuel flow transducer E Slide firesleeve off fuel lines...

Page 527: ...ion 71 00 50 be followed to as sure engine is set up for proper operation I When all adjustments have been made and all connections checked for security install cowling per Section 71 10 00 73 40 00 F...

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Page 529: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 74 IGNITION...

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Page 531: ...ON M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 74 IGNITON LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 74 Effectivity 1 03 17 74 Contents 3 03 17 74 00 00 5 03 17 7...

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Page 533: ...NANCE MANUAL Date MAR 2017 Rev Date CHAPTER 74 IGNITION TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 74 00 00 General 5 74 10 00 Electrical Power 5 74 10 01 Ignition System Troubleshooting 5 74 20 0...

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Page 535: ...properly timed to en gine Check magneto timing to engine Refer to Continental Motors Main tenance and Overhaul manual M 18 Shorted Condenser Replace Condenser Magneto internal timing incorrect or time...

Page 536: ...d magneto rotor turns counter clockwise passing in succession terminals of spark plug cables in engine firing order Cables are connected to magne tos so right magneto fires upper plugs on right side a...

Page 537: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 76 ENGINE CONTROLS...

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Page 539: ...20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 76 ENGINE CONTROLS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 76 Effectivity 1 03 17 76 Contents 3 03 17 76 00 00 5 03...

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Page 541: ...CE MANUAL Date MAR 2017 Rev Date CHAPTER 76 ENGINE CONTROLS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 76 00 00 General 5 76 10 00 Engine Controls Rigging 5 76 20 00 Engine Controls Maintenance 5...

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Page 543: ...s sembly to engine or propellor control component 3 Loosen hardware from attaching clamps Remove clamps Loosen hardware attaching cable assembly to throttle switch bracket 4 Loosen jamb nut connecting...

Page 544: ...KHEAD FITTING LOCKWASHER NUT ENGINE THROTTLE BODY PROPELLER GOVERNOR ENGINE FUEL CONTROL CONTROL CONTROL CONTROL TYP TYP TYP CLAMP CLAMP HEIM ROD END BEARING HEIM ROD END BEARING HEIM ROD END BEARING...

Page 545: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 77 ENGINE INDICATING...

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Page 547: ...0V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 77 ENGINE INDICATING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 77 Effectivity 1 03 17 77 Contents 3 03 17 77 00 00 5 03...

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Page 549: ...General 5 77 00 01 Ranges 5 77 10 00 Power Indicating 5 77 10 01 Tachometer 5 77 10 02 Manifold Pressure 5 77 10 03 Fuel Flow Indicating System 5 77 20 00 Temperature Indicating 5 77 20 01 Exhaust Gas...

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Page 551: ...77 20 01 EXHAUST GAS TEMPERATURE EGT INSTRUMENTATION Thermocouples attached to exhaust stacks send elec trical signals to GEA 71 Engine Airframe Unit Temper ature of hottest cylinder is displayed in d...

Page 552: ...le B YELLOW Caution 10 to 30 PSI C GREEN Normal 30 to 100 PSI D RED Warning 100 PSI COLD Refer to SECTION 79 30 01 7 6 8 2 3 4 5 9 10 1 EIS Display M20V Ammeter Voltmeter Cylinder Head Temperature Tur...

Page 553: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 78 EXHAUST...

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Page 555: ...ON M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 78 EXHAUST LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 78 Effectivity 1 03 17 78 Contents 3 03 17 78 00 00 5 03 17 7...

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Page 557: ...NTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 78 EXHAUST TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 78 00 00 General 5 78 10 00 Exhaust System Installation 5 78 30 00 Exhaust System Servicing 5 7...

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Page 559: ...EGT probes and one system TIT probe to monitor exhaust gas temperatures Refer to Probe manufac turer s service literature for recommended mainten ance and troubleshooting 78 30 00 EXHAUST SYSTEM SERVI...

Page 560: ...00 PERIODIC REPLACEMENT COMPONENTS It is recommended that all exhaust system pipes clamps and miscellaneous mounting hardware be re placed at engine overhaul time or as described in Chapter 5 Tailpipe...

Page 561: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 79 OIL...

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Page 563: ...AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 79 OIL LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 79 Effectivity 1 03 17 79 Contents 3 03 17 79 00 00 5 03 17 79 30 00 6 03 17 79...

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Page 565: ...TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 79 00 00 General 5 79 00 01 Oil Filter Removal 5 79 00 02 Oil Filter Installation 5 79 20 00 Distribution 5 79 30 00 Indicating 6 79 30 01 Oil Pressure...

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Page 567: ...roducts OIL SUCTION OIL THRU RELIEF VALVE OIL THRU OIL TEMPERATURE CONTROL VALVE OIL UNDER PRESSURE OIL FROM GOVERNOR OIL PRESSURE TEMPERATURE CONNECTION OIL TEMPERATURE CONTROL VALVE OIL PRESSURE REL...

Page 568: ...nual for additional system description service and trouble shooting instructions OIL PRESSURE TRANSDUCER MANIFOLD TRANSDUCER PRESSURE OIL PRESSURE TRANSDUCER FIGURE 79 2 79 30 02 OIL TEMPERATURE The o...

Page 569: ...emove oil cooler an flush thor oughly Thermostat damaged or held open by solid matter Remove clean valve and seat If still inoperative replace Oil viscosity too high Drain and refill with correct sea...

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Page 571: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 80 STARTING...

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Page 573: ...N M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 80 STARTING LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 80 Effectivity 1 03 17 80 Contents 3 03 17 80 00 00 5 03 17 8...

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Page 575: ...MANUAL Date MAR 2017 Rev Date CHAPTER 80 STARTING TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 80 00 00 General 5 80 00 01 Troubleshooting 5 80 00 02 Maintenance 5 80 00 03 Removal 5 80 00 04 Insta...

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Page 577: ...80 2 80 00 04 INSTALLATION 1 Before installation clean any rust corrosion or dirt from mounting surface of starter motor 2 Check all ground straps connections for tightness 3 Install new O ring on st...

Page 578: ...ERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date Page 6 NOTE Cranking should be limited to 30 seconds and several minutes allowed between cranking peri ods to permit starter to cool STARTER RELAY...

Page 579: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 81 TURBOCHARGER...

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Page 581: ...MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 81 TURBOCHARGER LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 81 Effectivity 1 03 17 81 Contents 3 03 17 81 00 00 5 03 17 81 20 00 6 03 17...

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Page 583: ...PTER SECTION SUBJECT PAGE 81 00 00 General 5 81 10 00 Turbocharger Control 5 81 10 01 Turbocharger Control System 5 81 10 02 Alternate Air System Turbocharger Operation 5 81 20 00 Turbocharger Trouble...

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Page 585: ...ROL 81 10 01 TURBOCHARGER CONTROL SYSTEM The turbocharger output is controlled through coordi nated action of the Density Differential Pressure Con troller system when set up properly CAUTION It is ma...

Page 586: ...for gas leakage gaskets at cylinder ex haust ports gaskets at turbine inlet flanges et and correct White smoke exhaust Turbo coking oil forced through turbine housing seal Clean and change turbocharge...

Page 587: ...URES Torque V Band coupling to 30 40 In Lbs Tap cou pling lightly around circumference with a non metallic hammer to equalize band tension and proper align ment make sure to align the flanges and torq...

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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: ...ND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 91 ELECTRICAL WIRING DIAGRAMS AND SCHEMATICS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 91 Effectivity 1 03 17 91 Contents 3 03 17 9...

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Page 593: ...Rev Date CHAPTER 91 ELECTRICAL WIRING DIAGRAMS AND SCHEMATICS HARNESS DRAWINGS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 91 00 00 General 5 91 00 01 Electrical Systems Notes 5 91 00 02 Wiring Id...

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Page 595: ...clockwise with a minimum of three 3 wraps per foot 10 F denotes ground through frame no wires 11 All knife disconnect splices to be insulated with PVC105 and securely string tied with Airtex no 417 c...

Page 596: ...INSTRUMENTS FUEL FLOW DW INSTRUMENTS ENGINE VACUUM EG GEAR ELECTRIC EL ELECTROLUMINESCENCE ET EMERGENCY LOCATOR BEACON FA ALT EMER FRENCH FH FUSE HOLDERS FN PHONES FU FUSES FW ALT EMER FIELD FRENCH GD...

Page 597: ...91 00 03 ABBREVIATIONS EQUIPMENT LIST The abbreviations to the electrical system hardware charts are necessary due to space limitations in the fields of the computer Airspeed A S Glareshield Glrshld R...

Page 598: ...LECTRICAL HARNESS FLOORBOARD 33 0001 AND ON 800454 ELECTRICAL HARNESS WING 33 0001 AND ON 800455 ELECTRICAL HARNESS OVERBOARD 33 0001 AND ON 800456 ELECTRICAL HARNESS FLIGHT PANEL 33 0001 AND ON 80045...

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Page 751: ...R2C R9A2 R9A1 R7A L162C...

Page 752: ...R2C L13D L58B L13H R4D R9F R15B...

Page 753: ...L13A L58B R7B R15B R2C L66A R37A R4D...

Page 754: ...L16B R2D R1A R9D R2E L31B R15D L13H L162C...

Page 755: ...R15B L31B R15D R1A R9D R2E L13C R9B L13F R9E...

Page 756: ...L13E R41A R4A L16A R2D L8A L162C...

Page 757: ...R15C R2E R15B L58A R41A L31B R4A L22B...

Page 758: ...L22B R2E R15C R15C L8A...

Page 759: ...R2A R15B R2E R2B L31B R4D L162C...

Page 760: ...L3A R2D R6B R15B L58B L22A R41A L58A L13H L162C...

Page 761: ...R2D R2C R15B L13D...

Page 762: ...L13F R15B R7B R7A R9A2 R2E R2D R9F R9D L162C...

Page 763: ...L8A R2D L13A L31A R37A R15B R6A L31B L13E L162B L162C R15C...

Page 764: ...L16A L13C R9B L13E 4D R2E R15B L114A R4C...

Page 765: ...L13A L15A L38A R4D L58A L8A 0A R2E R15B L156B...

Page 766: ...L66A R2D 0A R15B L13B R4D L156B L156C...

Page 767: ...L13B L58B L66A R15B R4D R2C L3A L13G R15B R9A2...

Page 768: ...L16A R11A L114A...

Page 769: ...L58A R15C L13A L13E R9A1 R15B L38A R2D L22B...

Page 770: ...R9B L38A L31A L8A L13A R2E L58A L16A R9D...

Page 771: ...L13F L31B R2A R2C L16B R6A L22B L8A L13E L162C...

Page 772: ...R15C R9A1 R41A R2D L22A...

Page 773: ...R4A R15B L13E R4B R2E R15C L162D...

Page 774: ...R9F R7B R7A R9A1 L13F R2E R15B R2C R2C...

Page 775: ...R11A R2E R15B L114A...

Page 776: ...R37A R4D L8A R2E...

Page 777: ...R2E R6B R6A L3A L8A R4D R9A2 R2D L8A L162B L162A L162C...

Page 778: ...L13H R9A1 L3A R2C L58B R9C R2E R15B L7A...

Page 779: ...R15B R4D L8A R7A L13F L58B L3A R15C R9A2 R2C...

Page 780: ...R15B R9D R4A R2E L13D R2B L58A L13B L16A R11A L13A L156C R15E R15F L156B...

Page 781: ...R2D L13D L13F L8A L13E L58A L3A L66A L16B R41A L162B L156B L156C...

Page 782: ...R2E L13F R9C R9F R37A R7A L13C R9D R1A R15D R4A R11A L31A R2A R6A R15C R15B L16A L16A L22B 0A...

Page 783: ...R9D R2A R1A L16A R15C L8A L31B R15A L162C L31C...

Page 784: ...L66B R41B R9A1...

Page 785: ...R9A1 R15G R15G R15G R15G...

Page 786: ...R9A1 R2C R41A R41B L58A L66B L13H...

Page 787: ...R9A2 R15B L58B L13F R2C L156A L162A...

Page 788: ...R15A R2A R4D R4D L31B R15A R6B L15G...

Page 789: ...15A R2E L16A R1A R2C R4D R7A R11A L16B R9A1 R9C R9F R2B R2A R9D R9B R15G R15F R15B R15C R15D R37A R41A R41B R7B 0 L13C R4A L156B L4A L66B L66A R15E R15A R4C L162D L22A L22B L114A L156C 0A L7A L13H R9E...

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Page 800: ......

Page 801: ...L16A L31B L4A R2E R15B L114A...

Page 802: ...4TH CERT...

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Page 821: ...2ND CERT...

Page 822: ...SHIELD LINE LOAD 4TH CERT...

Page 823: ...SHIELD LINE LOAD 4TH CERT...

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Page 871: ...BL 0 00 STA 0 00 STA 53 00 STA 100 00 STA 120 00 STA 120 00...

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Page 873: ...BL 0 00 STA 0 00 STA 53 00 STA 100 00 STA 120 00 STA 142 00 RBL 19 00 LBL 19 00 STA 91 36...

Page 874: ...15A R2E L16A R1A R2C R4D R7A R11A L16B R9A1 R9C R9F R2B R2A R9D R9B R15G R15F R15B R15C R15D R37A R41A R41B R7B 0 L13C R4A L156B L4A L66B L66A R15E R15A R4C L162D L22A L22B L114A L156C 0A L7A L13H R9E...

Page 875: ...10E 10E...

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Page 878: ...BOSE MIC PHONE BOSE MIC PHONE...

Page 879: ...B B VIEW B B VIEW A A...

Page 880: ...VIEW A A DETAIL P P...

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Page 882: ...STA 100 00 STA 120 00 WL 0 00...

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Page 884: ...VIEW LOOKING INBD LH...

Page 885: ...PRECIS E FLIGHT INC OXYGE N DISPLA Y LOGIC ASSY DRAWI NG LIST 100N00 00 REV AE PART NUMBE R 100N20 26 1 REV S N LRD006 85 INCLUD ED IN DISPLA Y LOGIC ASSY W BRACK ET DRAWI NG LIST 106N00 00 REV A PAR...

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Page 894: ...E D E D 25 10 10 5 5 5 10 10...

Page 895: ...N N...

Page 896: ...VIEW LOOKING INBOARD ON TAILCONE F...

Page 897: ...VIEW LOOKING INBOARD...

Page 898: ...VIEW LOOKING INBD J J H H STA 176 0 STA 159 0 STA 149 5 STA 142 0 120 0 STA...

Page 899: ...VIEW H H VIEW G G WL 0 00 142 0 STA G G...

Page 900: ...WL 2 00 0 00 WL VIEW J J...

Page 901: ...VIEW E E...

Page 902: ...VIEW D D 10 10 10 5 5 2 20 25 10 10 10 5 5 5 2 25 K 5 20...

Page 903: ...VIEW K K...

Page 904: ...VIEW LOOKING DOWN ON TAILCONE EMPENAGE...

Page 905: ...M L L M VIEW M M VIEW L L VIEW LOOKING INBOARD AT TAILCONE EMPENAGE...

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Page 930: ...ROLL SERVO GDC74 PFD PFD MFD GMA1347 MFD FAN FAN AUDIO INTERFACE MKR A ANTENNA CABLE GROUND BLOCK GEA INTERFACE G1000 WIRING CONNECTOR CONTROL WHEEL FLT PNL 3 GND WIRES GCU476 KEYPAD...

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Page 988: ...GDC47 PFD FAN PFD MFD FAN MFD GEA71 GEA71 GMA1347...

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Page 995: ...FORWARD INBD...

Page 996: ...S S FORWARD INBD...

Page 997: ...CABLE LOOP DETAIL VIEW LOOKING OUTBOARD FORWARD UP RIGHT HAND SIDE...

Page 998: ......

Page 999: ...T T...

Page 1000: ...VIEW LOOKING INBOARD FORWARD UP LEFT HAND SIDE...

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Page 1004: ...STA 110 47 VIEW LOOKING INBD R H SIDE TAILCONE NO SKIN WL 0 00...

Page 1005: ...OUTBD FORWARD...

Page 1006: ...S S TOP VIEW VIEW S MAGNETOMETER BRACKET RING ASSEMBLY 820355 3 SHELF NOT SHOWN FOR CLARITY OUTBD FORWARD VARIOUS PARTS NOT SHOWN FOR CLARITY...

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Page 1038: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL CHAPTER 95 SPECIAL TOOLS...

Page 1039: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK...

Page 1040: ...MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 95 SPECIAL TOOLS LIST OF EFFECTIVE PAGES CHAPTER SECTION SUBJECT PAGE DATE 95 Effectivity 1 03 17 95 Contents 3 03 17 95 00 00 5 03 17 95 00 00 6 03 1...

Page 1041: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK...

Page 1042: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date CHAPTER 95 SPECIAL TOOLS TABLE OF CONTENTS CHAPTER SECTION SUBJECT PAGE 95 00 00 Special Tools 5 95 CONTENTS...

Page 1043: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL INTENTIONALLY LEFT BLANK...

Page 1044: ...REFRIGERANT 30 LB CYLINDER R 134A CHARGING MANIFOLD W GAUGES ELECTRONIC LEAK DETECTOR ESTER RL 500S R 134A REFRIGERANT OIL LOCTITE 55431 THREAD SEALANT HOSE ADAPTER 1 2 MALE ACME TO 1 4 FEMALE FLARE V...

Page 1045: ...00 GSE 030038 501 SHOCK DISC REPLACEMENT TOOL GSE 030010 SHOCK DISC REPLACEMENT TOOL 33 LIGHTS 34 NAVIGATION 34 22 00 AOE 6054 ASSOCIATED GROWLER ARMA TURE TESTER 35 OXYGEN 35 00 01 MAC 870025 501 AV...

Page 1046: ...AND OP ERATION MANUAL 73 ENGINE FUEL 74 IGNITION 74 00 00 M 18 CMI MAINTENANCE AND OVER HAUL MANUAL 76 ENGINE CONTROLS 77 ENGINE INDICATING 190 00450 03 Rev A OR LATER GARMIN G1000 INTEGRATED FLIGHT...

Page 1047: ...MOONEY INTERNATIONAL CORPORATION M20V SERVICE AND MAINTENANCE MANUAL Date MAR 2017 Rev Date Page 8 INTENTIONALLY LEFT BLANK 95 00 00...

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