1962-1978 Mooney MC20 & 22 Series Service Manual
Comprehensive repair and service manual for the Mooney M20C, M20D, M20E, M20F, M20G, M20J, M20K, M22 aircraft models. Includes detailed maintenance procedures and specifications for engines and airframes. Part number 150010-111.
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Sample pages from the 1962-1978 Mooney MC20 & 22 Series Service Manual manual
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Mooney Models Covered & Key Technical Specifications
Models: M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, M22
Sub-models / Variants: Mark 21, Super 21, Executive 21
Build Years: 1962–1978
Serial Numbers: 101–680001, 2321–670135, 20-101 thru 20-1258, 22-1362 thru 22-1407, 24-0001 thru 24-3154, 25-0001 thru 25-0855, 660001 thru 670539, 680001 thru 700006
Technical Data:
- Engine: Lycoming O-360-A1D
- Engine power: 180 HP at 2700 RPM
- Propeller diameter: 74 inches
- Fuel type: 91/98 octane
- Electrical system: 12 volt, 50 amp generator
- Battery capacity: 35 amp-hour
- Tire pressure: 30 PSI
- Oil capacity: 8 quarts (6 quarts minimum)
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Technical Scope and Coverage for 1962–1978 Mooney Aircraft
- Built for owners and workshops servicing the 1962–1978 Mooney M20 and M22 series aircraft, specifically including the M20C, M20E, M20F, M20J, and M20K models
- Contains 61 figures documenting the structural, mechanical, and electrical components with detailed exploded-view references
- Official manufacturer parts documentation, Revision July 1976
- Downloads to your account within seconds of checkout
- Re-download the file any time, no expiration
- Full-text search finds any part number in seconds
- Laid out for standard letter and A4 printing
- This 1976 revised parts catalog provides the only verified manufacturer part numbers and assembly data required for airframe, wing, and engine component procurement during routine maintenance cycles
Component and System Documentation
The 1962–1978 Mooney M20 series parts catalog presents an extensive assembly breakdown organized by airframe, wing, empennage, and power plant groups. This manual provides detailed illustrations of structural rib stations, fuel tank sealant applications, and landing gear retraction systems. Detailed exploded-view diagrams illustrate every component, from flight control surfaces and cabin interior furnishings to the electrical system configurations for each model variant. Each listing provides the required units per assembly, enabling accurate inventory management during shop floor maintenance or structural restoration.
Specification Highlights
Technical data sections provide critical reference values for engine oil capacity and battery specifications. The Lycoming O-360-A1D engine produces 180 HP at 2700 RPM in the Mark 21. Tire pressure for the main and nose gear is documented at 30 PSI in the servicing data. The electrical system utilizes a 12-volt generator architecture supporting a 35 amp-hour battery. Note: This page is a contents overview for the manual. It does not provide repair or diagnostic instructions. This professional 100-page OEM publication details all standard replacement parts for the 1962–1978 Mooney M20 and M22 series aircraft, covering primary airframe, electrical, and propulsion system components for various build serials.
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