Mooney M20K Pilot's Operating Handbook (POH) 1978-1984 Service Manual
238 Pages • 8.03 MB • Instant, Printable PDF
Mooney Models Covered & Key Technical Specifications
Models: Mooney M20K
Model Years: 1978–1984
Serial Numbers: 25-0001 thru 25-0446
Technical Data:
- Engine: Continental TSIO-360-GB1, 6-cylinder, horizontally opposed, turbo-charged, aircooled, fuel-injected
- Horsepower: 210 BHP at 2700 RPM
- Propeller: McCauley 2A34C216/90DHB-16E, constant speed, 74.0 in. diameter
- Fuel: 100 or 100LL grade, 80 U.S. Gal. total capacity (72 U.S. Gal. usable)
- Gross Weight: 2900 lbs.
- Maximum Operating Altitude: 24,000 feet MSL
Mooney Manual Features & Content Preview
The 1978–1984 Mooney M20K Pilot's Operating Handbook is an official 238-page manual detailing flight limitations, performance specifications, and emergency handling protocols. It specifically covers the serial range 25-0001 through 25-0446. Designed for mechanics, technicians, and aviation DIYers, this guide provides accurate reference material for maintenance planning, troubleshooting, and pre-flight verification.
Please note: Ensure all hands-on work aligns with current FAA regulations and OEM guidelines. This manual serves strictly for technical reference and operational planning.
Inside the Mooney M20K Handbook
- Covers aircraft equipped with the Continental TSIO-360-GB1 engine, outlining normal, emergency, and performance procedures.
- Official Mooney publication: Manual Number 1224, Revision F (dated 3-7-84).
- Features 47 performance and configuration charts, 12 emergency checklist tables, and 19 detailed placard specifications.
Flight Procedures and Operational Data
This handbook delivers deep insights into managing high-altitude operations and standard flight cycles. Initial chapters outline aircraft dimensions and base weights. Subsequent sections dive into technical data for the electrical system, landing gear, and engine cooling parameters. It also acts as the primary reference for emergency procedures. You will find step-by-step protocols for engine power loss, electrical fires in-flight, and manual gear extension methods.
Performance and Technical Specifications
Section 5 contains extensive performance data, including precise airspeeds for gear and flap extension. The maximum continuous manifold pressure for the TSIO-360-GB1 is documented at 40.0 inches Hg. The propeller governor controls blade angles between 14.7° and 33.0°, while operating fuel limits are capped at 72 U.S. gallons of usable capacity. Service data shown is highly detailed, allowing professionals to verify system parameters quickly and efficiently.
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