Mooney M20 B C D E IPC parts manual 1961 - 1964

SPARE PARTS MANUAL # 1701B--1939B # 1940C--2296C # 2297C--2622C # 2623C--2806C # 101D--200D # 201D--251D # 101E--469E Revised: October 15, 1963 Corrected: January 1966 1961, M-20B 1962, M-20C 1963, M-20C 1964, M-20C 1963, M-20D 1964, M-20D 1964, M-20E MOONEY AIRCRAFT, INC. Spare Parts Department P .00 Box 72 Kerrville, Texas 78028

INTRODUCTION This illustrated parts catalog is designed to assist in the identification of standard replacement parts for the Mooney M-20 series aircraft designated on the foregoing lead page. The catalog features three major sections: INTRODUCTION This section should be read carefully to become familiar with the catalog arrangement and the correct procedure in ordering parts. A GROUP ASSEMBLY INDEX is included to help locate figure illustrations in the catalog. GROUP ASSEMBLY PARTS LISTING The body of the catalog lists standard replaceable parts. Each illustration is accompanied by an assembly breakdown in its adjacent text. EFFECTIVITY LIST The effectivity list in the catalog appendix tabulates all four--digit Mooney numbers with their corresponding six-digit cross reference numbers in additon to part effectivity listings. Six-digit numbers I in the first column toward the end of the effectivity list I are those having no analogous four-digit cros s reference numbers. All Mooney parts manufactured prior to March 1962 were identified by four-digit numbers r whereas I subsequent parts were assigned six-digit numbers. Analgous numbers in the cross reference columns denote parts that are similar or inter- changeable when their dash numbers (as indicated in the body of the catalog) are the same; consequently I this table will be helpful in discerning effectivity extensions of Mooney parts manufactured prior to March 1962. NOTE All "and On" deslgnations in the effectIvIty lists are limited to the serial number categories tabulated in the SERIAL NUMBER INFORMATION c01umn on the lead page. TO LOCATE A PART Refer to the GROUP ASSEMBLY INDEX to find the figure number where the part will be portrayed. Locate the part in the illustration and note its index number which corre- sponds to those in the accompanying text. The part number column identifies the item by its part or assembly number; this is the part number to be used in making an order. References ( ... REF.) in the illustrations signify assemblies that are included in the illustrations for orientation purposes only. These referenced assemblies are parts of assemblies shown elsewhere in the catalog.

HOW TG ORDER PARTS Place your order with the Mooney distributor in your area. Parts are available only through the authorized Mooney distribl,ltor organization I and all orders received at the factory that originate from other sources will be returned to the area distributor for processing. Always specify the PART NUMBER, DESCRIPTION, AND QUANTITY of parts desired. Be sure to include the part CODE NUMBER when listed in the price list I and indicate the MODEL and SERIAL NUMBER of the aircraft for which the parts are intended. Give complete address information. When the method of shipment (freight I express I parcel post I air express I air freight I or air parcel post) is not specified I or when the nature of the shipment requires special handling I parts will be shipped by the means most suitable to the shipper. LIABILITIES Orders are double checked before leaving the shipping departinent I and a packing slip is enclosed in ::he shipment. Claims for errors or shorta<Jes must be made within three days after receipt of orders I and no material should be returned without first obtaining written permission from the factory. Goods returned without notice will be held at the owner's risk for thirty days and will then be disposed of at the Company's discretion. Transportation charges £ or returned goods must be prepaid or the shipment will be refused. Mooney Aircraft I Inc. I cannot be held liable for damage to parts incurred in transit. If a shipment is received in a damaged condition I have the delivery man or shipping company make a notation of the damage and file the claim with the carrier. CAUTION This parts catalog is intended only to aid in the ordering of replacement parts. Thc illustrations omit many details for the sake of clarity. Dimensions I systems routing I and irrelevallt details have been intentionally distorted for maximum econ- omy of space utilization. Therefore·, it is essential that the illustrations not be used as guides for mechanical reassembly and installation of parts.

GROUP ASSEMBLY INDEX Section L WING GROUP 1 FIG. 1. WING, CENTER SECTION DETAIL FIG. 2. WING, TIP SECTION DETAIL FIG. 3. WING, SKIN DETAIL FIG. 4. WING, SCUPPER BOX & TANK VENT DETAIL FIG. 5. WING, AILERON ASSEMBLY & FLAP ASSEMBLY FIG. 6. WING, FUSELAGE TO WING MATING Section II. FUSELAGE AND TAIL CONE GROUP 20 FIG. 7. FUSELAGE, TUBULAR STRUCTURE FIG. 8. FUSELAGE, TUBULAR SUB-ASSEMBLIES FIG. 9. FUSELAGE, FORWARD SKINS & FIREWALL DETAIL FIG. 10. FUSELAGE, BOTTOM SKINS & BULKHEADS FIG. 11. FUSELAGE, INSTRUMENT PANEL DETAIL FIG. 12. FUSELAGE, CABIN DOOR DETAIL FIG. 13. FUSELAGE, BAGGAGE DOOR DETAIL FIG. 14. FUSELAGE, WINDOW & WINDSmELD INSTALLATION FIG. 15. FUSELAGE, FLOORBOARD ASSEMBLY & INSTAL_ , M-20B FIG. 16. FUSELAGE, FLOORBOARD ASSEMBLY & INSTAL. , M-20C, D & E FIG. 17. TAIL CONE, DETAIL FIG. 18. TAIL CONE, SKIN DETAIL FIG. 19. ACCESS DOORS & PANELS Section III. CHASSIS GROUP FIG. 20 FIG. 21. FIG. 22. FIG. 23. FIG. 24. FIG. 25. FIG. 26. FIG. 27. MAIN LANDING GEAR ASSEMBLY & INS'mLLATION NOSE LANDING GEAR ASSEMBLY & INSTALLATION LANDING GEAR FAIRING ASSEMBLIES LANDING GEAR DOOR INSTALLATION WHEEL & BRAKE DETAIL, M-20B WHEEL & BRAKE DETAIL, M-20C, D & E GEAR RETRACTION SYSTEM HYDRAULIC BRAKE SYSTEM Section IV. CONTROL SYSTEM GROUP FIG. 28. TRIM CONTROL SYSTEM, M-20B FIG. 29. TRIM CONTROL SYSTEM, M-20C, D & E FIG. 30. FLAP CONTROL SYSTEM, M-20B FIG. 31. HYDRAULIC FLAP CONTROL SYSTEM, M-20C, D &: E FIG. 32. ELEVATOR & AILERON CONTROL SYSTEM FIG. 33. RUDDER, BRAKE & NOSE WHEEL CONTROL SYSTEM 77

Section V. TAIL SECTION GROUP 94 FIG. 34. STABILIZER & STINGER ASSEMBLY FIG. 35. FIN ASSEMBLY FIG. 36. ELEVATOR ASSEMBLY & RUDDER ASSEMBLY FIG. 37. EMPENNAGE INSTALLATION Section VI. POWER PLANT GROUP 104 FIG. 38 ENGINE & PROPELLER INSTALLATION, M-20B, C & D FIG. 39. ENGINE & PROPELLER INSTALLATION, M-20E FIG. 40. ENGINE COWLING DETAIL, M-20B, C & D FIG. 41. ENGINE COWLING DETAIL, M -20E FIG. 42. ENGINE BAFFLE DETAIL, M-20B, C & D FIG. 43. ENGINE BAFFLE DETAIL, M-20E FIG. 44. ENGINE CONTROLS INSTALLATION, M-20B FIG. 45. ENGINE CONTROLS INSTALLATION, M-20C, D & E FIG. 46. ENGINE INDUCTION & EXHAUST SYSTEM, M-20B FIG. 47. ENGINE INDUCTION & EXHAUST SYSTEM, M-20C & D FIG. 48. ENGINE INDUCTION SYSTEM, M-20E FIG. 49. ENGINE EXHAUST SYSTEM, M-20E Section VII. FUEL AND OIL SYSTEM 132 FIG. 50. FUEL SYSTEM SCHEMATIC, M-20B, C & D FIG. 51. FUEL SYSTEM SCHEMATIC I M -20C & D FIG. 52. FUEL SYSTEM SCHEMATIC, M-20E FIG. 53. OIL SYSTEM INSTALLATION Section VIII. CABIN INTERIOR GROUP 142 FIG. 54. CABIN INTERIOR, M-20B & C FIG. 55. CABIN INTERIOR, M -20C, D & E FIG~ 56. SEAT ASSEMBLY & INSTALLATION FIG. 57. INTERIOR PLACARDS & DECALS Section IX. ELECTRICAL GROUP 156 FIG. 58. ELECTRICAL SYSTEM SCHEMATIC, M-20B FIG. 58A. ELECTRICAL SYSTEM SCHEMATIC, M-20B FIG. 59. ELECTRICAL SYSTEM SCHEMATIC, M-20C FIG. 59A. ELECTRICAL SYSTEM SCHEMATIC, M-20C FIG. 60. ELECTRICAL SYSTEM SCHEMATIC, M-20D 'FIG. 60A. ELECTRICAL SYSTEM SCHEMATIC, M -20D FIG. 61. ELECTRICAL SYSTEM SCHEMATIC, M-20C FIG. 6lA. ELECTRICAL SYSTEM SCHEMATIC, M-20C FIG. 62. ELECTRICAL SYSTEM SCHEMATIC, M-20E FIG. 62A. ELECTRICAL SYSTEM SCHEMATIC, M-20E

Section X. SYSTEMS GROUP FIG. 63. FIG. 64. FIG. 65. FIG. 66. FIG. 67. FIG. 68. CABIN VENTILATION' SYSTEM, M-20B & C CABIN VENTILATION SYSTEM, M-20C, D & E CABIN COOLING SYSTEM VACUUM SYSTEM INSTALLATION COWL FLAP CONTROL SYSTEM RETRACTABLE STEP SYSTEM Section XI. MISCELLANEOUS FIG. 69. PAINT SCHEME FIG. 70. EXTERIOR DECALS FIG. 71. EXTERIOR PLACARDS FIG. 72. EXTERIOR DECORATING TAPE, M-20C & E FIG. 73. WING, FIN & STABILIZER STATIONS FIG. 74. FUSELAGE & TAIL CONE STATIONS 170 183

1- WI'NG GROUP 11- FUSELAGE & TAIL CON E GROUP III-CHASSIS GROUP IV - CONTROL SYSTEMS GROUP V- TAIL GROUP VI-POWER PLANT GROUP VII- FUEL & OIL SYSTEM GROUP VIII-INTERIOR DETAIL GROUP IX - ELECTRICAL GROUP X-SYSTEMS GROUP, MISC. XI-MISC. GROUP

FIG. 1 - WING, CENTER SECTION DETAIL 2182 REF. 88 83 /84 85 86 I 1 ~ I FT=l i---~ 87 JIO ,11, ----..,'--.. 90 80------· ,.... 1940 & ON ~2 / 58 57 16 54 '.31 cr-:=r? 47 48 69 :2 67

Mooney M20 B C D E IPC parts manual 1961 - 1964

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