1978 Mooney M20J Precision Pilot's Operating Handbook & Flight Manual
Aircraft systems, engine limits, and emergency procedures for Mooney M20J models with full performance charts, weight and balance data, and detailed maintenance instructions.
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Mooney Models Covered & Key Technical Specifications
Models: Mooney M20J
Sub-models / Variants: Mooney 201
Trade Names: Mooney 201
Build Years: 1978
Serial Numbers: 24-0084, 24-0378 and on
Technical Data:
- Engine: Lycoming IO-360-A3B6D
- Engine displacement: 361.0 cubic inches (5916 cc)
- Horsepower: 200 BHP @ 2700 RPM
- Fuel capacity: 66.5 U.S. gallons (64 U.S. gallons usable)
- Propeller: McCauley B2D34C214/90DHB-16E constant-speed
- Maximum takeoff weight: 2740 lbs
- Standard empty weight: 1640 lbs
- Cylinder head temperature limit: 475°F (246°C)
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Mooney M20J 1978 Pilot's Operating Handbook Coverage
- Covers 1978 Mooney M20J, also designated as the Mooney 201, certificated under FAA Type Certificate No. 2A3
- Official Mooney Aircraft Corporation publication, Manual Number 1221, issued November 15, 1977
- Documents performance, weight and balance, emergency procedures, and normal operating limitations across 153 pages
- Includes 9 distinct sections covering general data, limitations, emergency, normal, performance, weight and balance, system descriptions, and maintenance
- Delivers a direct download the moment payment clears
- Stored against your account so you can retrieve it after a hard-drive loss
- Full-text search finds any part number in seconds
- Laid out for standard letter and A4 printing
- This 1978 first edition serves as the foundational operating manual for the Mooney 201 series, documenting the specific IO-360-A3B6D engine integration and airframe limitations
Flight Operational and System Data
This manual provides flight crews and owners with the manufacturer-specified operational protocols for the Mooney 201. The document is structured to facilitate compliance with FAA-required CAR Part 3 standards, detailing everything from preflight inspection walk-around diagrams to complex emergency procedures for engine fires, alternator power loss, and landing gear extension malfunctions. Each system is described with technical depth, supported by placards, instrument markings, and weight limit tables essential for safe flight operation.
Specification Highlights
Engine oil capacity is standardized to 8 quarts representing the maximum engine sump volume. The IO-360-A3B6D engine maximum cylinder head temperature is rated at 475°F for maximum continuous operation. Gross maximum takeoff weight achieves 2740 pounds structural limit requirement. This official 153-page Mooney OEM pilot's operating handbook covers the 1978 Mooney M20J, documenting engine, performance, weight and balance, and emergency procedures for the 201 model-series aircraft.
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