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
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
1978 Mooney M20J (201) Pilot's Operating Handbook
- 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, including limitations, normal and emergency procedures, performance, weight and balance, and system descriptions.
- Instant Digital Access: Fully searchable PDF format delivered immediately at checkout.
- Secure & Print-Ready: Permanently backed up in your account for future retrieval. Optimized for standard letter and A4 printing.
- Model Specific: First edition serving as the foundational operating manual for the Mooney 201 series, detailing the IO-360-A3B6D engine integration.
Flight Operations and System Overview
As the foundational reference for the Mooney 201 series, this manual outlines the manufacturer-specified protocols required for safe flight and FAA CAR Part 3 compliance. It provides flight crews and maintenance technicians with deep technical insight into the airframe and systems. The handbook includes comprehensive preflight walk-around diagrams, precise instrument markings, and detailed weight limit tables. It also thoroughly breaks down complex emergency procedures, equipping operators with the correct steps for scenarios like alternator power loss, engine fires, and landing gear malfunctions.
Technical Specifications
This documentation serves as the definitive source for factory-baseline operating limits. It details the maximum structural takeoff weight of 2,740 lbs, standard engine oil sump capacity of 8 quarts, and the maximum continuous cylinder head temperature for the IO-360-A3B6D engine (rated at 475°F). Whether you are verifying cockpit placards, calculating weight and balance, or reviewing system tolerances, this manual delivers the exact factory data required to operate the aircraft safely and maintain strict compliance with OEM standards.
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