Mooney M20K Pilot's Operating Handbook (POH) 1978–1984 Service Manual

238 Pages • 8.03 MB • Instant, Printable PDF

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Mooney Models Covered & Key Technical Specifications

Models: M20K

Model Years: 1978–1984 (1978, 1979, 1980, 1981, 1982, 1983, 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

Technical Specifications
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Document Number / Seller:
28389 / Elizabeth Morgan
File Size:
8.03 MB
File Type:
PDF
Language:
English
Pages:
238
Printable:
Yes
Category:
Aircraft
Last updated / verified
Aug 18, 2026

Mooney Manual Features & Content Preview

The 1978–1984 Mooney M20K Pilot's Operating Handbook is an official 238-page PDF manual (P/N 1224) 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, diagnostic evaluations, and pre-flight verification. For a working professional, having these exact factory baselines directly at the workstation drastically reduces downtime during system run-ups and functional tests, eliminating guesswork on the hangar floor.

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.
  • Explores critical sub-assemblies including the turbocharger, continuous flow fuel injection, vacuum system, pitot-static system, and the empennage.
  • Highlights operational parameters for the annunciator panel, oxygen equipment, ice protection hardware, and the hydraulic brake reservoir.

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. To save owners from an expensive trip to the repair shop, the manual also includes precise step-by-step instructions for routine upkeep, such as executing engine performance checks, cleaning the Donaldson dry-type induction air filter, and properly flushing the gascolator fuel lines.

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. To assist with accurate evaluations, the document incorporates specific visual aids, naming the Three View drawing, Airspeed Calibration chart, Takeoff Ground Roll Distance graph, Center of Gravity Moment Envelope, and the Priming Time Requirement curve.

When executing a repair or evaluating the Continental TSIO-360-GB1, technicians must be aware of a notorious operational pitfall: inadvertently overboosting the turbocharger. Advancing the throttle too aggressively during cold weather operations—before the engine oil reaches the 100°F minimum—can easily induce a severe manifold overboost that mandates a major engine repair. Additionally, failing to strictly observe the 1650°F Turbine Inlet Temperature (TIT) limits during mixture leaning frequently masks underlying issues and leads to premature exhaust valve degradation.

Technical Safety Notice
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This official OEM document is intended for professional technicians and skilled operators. Performing service on mechanical equipment involves inherent risks. By purchasing, you acknowledge that RepairLoader provides original manufacturer data for informational purposes. Always prioritize safety: use correct tools, wear protective gear, and consult a certified professional if you are uncertain of any procedure.

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