1978 Mooney M20J Precision Pilot's Operating Handbook & Flight Manual (P/N 1221)
153 Pages • 6.29 MB • Instant, Printable PDF
Mooney Models Covered & Key Technical Specifications
Models: Mooney M20J
Sub-models / Variants: Mooney 201
Trade Names: Mooney 201
Model Years: 1978
Serial Numbers: 24-0084, 24-0378 and on
Technical Data:
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Engine: Lycoming IO-360-A3B6D
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Engine displacement: 361.0 cubic inches (5916 cc)
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Horsepower: 200 BHP @ 2700 RPM
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Fuel capacity: 66.5 U.S. gallons (64 U.S. gallons usable)
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Propeller: McCauley B2D34C214/90DHB-16E constant-speed
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Maximum takeoff weight: 2740 lbs
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Standard empty weight: 1640 lbs
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Cylinder head temperature limit: 475°F (246°C)
Mooney Manual Features & Content Preview
- Official OEM Publication: Manual Number 1221 (Issued November 15, 1977) for the 1978 Mooney M20J, certificated under FAA Type Certificate No. 2A3.
- Complete Documentation: 153 pages spanning 9 distinct sections. Covers limitations, standard and emergency procedures, performance charts, weight and balance, and detailed system descriptions.
- Model Specifics: First edition serving as the foundational operating reference for the Mooney 201 series. Thoroughly details the Lycoming IO-360-A3B6D engine integration.
Flight Operations and System Overview
Navigating FAA CAR Part 3 compliance requires exact manufacturer protocols. This manual delivers exactly that. It gives maintenance technicians and flight crews a clear, technical look at the Mooney 201 airframe and its integrated systems. You will find comprehensive preflight walk-around diagrams. Precise instrument markings are mapped out alongside detailed weight limit tables. Understanding these factory limitations is critical for safe operation and maintenance; always verify procedures against current directives before initiating flight or shop work. The handbook also breaks down complex emergency procedures. It outlines the exact steps needed to handle alternator power loss, engine fires, or landing gear malfunctions efficiently.
Technical Specifications
Need exact factory-baseline operating limits? This documentation is the definitive source. It locks down the maximum structural takeoff weight at 2,740 lbs. You get standard capacities, like the 8-quart engine oil sump. It also details the maximum continuous cylinder head temperature for the IO-360-A3B6D engine, rated precisely at 475°F. Verifying cockpit placards or calculating weight and balance requires highly accurate data. Reviewing system tolerances is just as demanding. This manual hands you the exact factory numbers necessary to keep the aircraft compliant with OEM standards, whether you are on the ramp or in the hangar.
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