Mooney M20K 1978–1984 Pilot's Operating Handbook (P/N 1224)
238 Pages • Printable PDF • 8.03 MB • Download
Mooney Models Covered & Key Technical Specifications
Model: M20K
Model Years: 1978–1984 (1978, 1979, 1980, 1981, 1982, 1983, 1984)
Serial Numbers: 25-0001 thru 25-0446
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Engine: Continental TSIO-360-GB1, 6-cylinder, horizontally opposed, turbo-charged, aircooled, fuel-injected
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Horsepower: 210 BHP at 2700 RPM
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Propeller: McCauley 2A34C216/90DHB-16E, constant speed, 74.0 in. diameter
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Fuel: 100 or 100LL grade, 80 U.S. Gal. total capacity (72 U.S. Gal. usable)
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Gross Weight: 2900 lbs.
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Maximum Operating Altitude: 24,000 feet MSL
Mooney Manual Features & Selected Content Preview
The 1978–1984 Mooney M20K (231) Pilot's Operating Handbook and Airplane Flight Manual, P/N 1224, Revision F dated March 7, 1984, covers S/N 25-0001 thru 25-0446. It provides operating limitations, flight procedures and owner-level servicing information for aircraft equipped with the Continental TSIO-360-GB1.
PDF Search, Bookmarks and Diagram Detail
Search and navigation: Text search works through much of the handbook, with OCR errors and gaps in charts and equipment lists. Embedded bookmarks cover most main sections but omit Weight & Balance; small electrical-schematic labels need zooming, and some chart and table pages need rotation.
Delivered as one printable 238-page PDF. This includes 14 preliminary pages, the two-page Supplemental Data introduction, the 20-page Safety Information section and blank pages within the file.
Flight Procedures, Performance and Owner Servicing
These selected contents outline the main areas covered; further topics include cabin heating and ventilation and Emergency Locator Transmitter operation.
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Normal flight procedures: Preflight inspection, engine starting, magneto and propeller checks, takeoff, climb, cruise, descent, landing, go-around and shutdown checklists.
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Emergency procedures: Engine power loss, air starts, engine and electrical fires, turbocharger and fuel-pump failures, alternator faults and manual landing-gear extension.
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Performance and loading: Takeoff and landing charts, climb data, cruise power schedules, range and endurance curves, airplane weighing and loading calculations.
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Aircraft systems: Operation of continuous-flow fuel injection, the turbocharger, constant-speed propeller, vacuum and pitot-static systems, with supporting system illustrations.
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Controls and warnings: Annunciator-panel indications, electrical circuit protection, landing-gear interlocks, wing flaps and the empennage pitch-trim mechanism.
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Owner servicing: Step-by-step instructions for Donaldson induction-air-filter cleaning and gascolator flushing, plus battery, tire, lubrication and hydraulic-brake-reservoir care.
This handbook is suited to M20K pilots and owners reviewing aircraft operation and routine care; engine servicing calls for qualified personnel.
Flight Planning and Loading Records
The Airspeed Calibration and Takeoff Ground Roll Distance charts support preflight performance planning. Cruise power schedules and nautical-miles-per-gallon curves let pilots compare speed, fuel use and range under the stated conditions.
Chart assumptions: Some range and endurance charts use a fuel assumption that differs from the usable capacity stated in the fuel limitations.
Weight & Balance includes the Center of Gravity Moment Envelope, a Pilot's Loading Guide and equipment lists with weights and arms. These references help account for installed equipment and loading changes. Aircraft-identification and owner weight-and-balance record fields are blank in this copy.
System Operation and Optional Equipment
The systems section explains the oil system, fuel metering unit, manifold valve and injector nozzles. The electrical schematic and circuit-breaker-panel view identify the alternator, voltage regulator, battery, starter and protected circuits.
Visual references include the Three View drawing and Priming Time Requirement curve. The ice-protection discussion addresses alternate induction air, pitot heat and the alternate static source; the handbook prohibits operation in known icing conditions.
Supplement coverage: Section 9 contains only its introductory material. Equipment-specific oxygen and autopilot supplements are not included.
Servicing Depth and Engine Performance Checks
Section 8 limits servicing coverage to work the operator would normally perform or supervise. For repair work beyond these procedures, the handbook refers to separate Service & Maintenance and Parts Manuals.
Engine performance checks include idle-mixture, full-power and critical-altitude ground and flight checks, with results recorded for verification by service personnel. Those records give owners and technicians a defined basis for discussing suspected performance changes.
The handbook warns that excessive turbocharger overboost can damage the engine and require inspection or replacement.
Ensure all hands-on work aligns with current FAA regulations and OEM guidelines. This manual is for technical reference and operational planning.
Examples of Engine Limits and Propeller Data
The powerplant tables specify a 1650°F maximum continuous TIT and a 1725°F transient maximum for the TSIO-360-GB1, with operation above the continuous limit restricted to 30 seconds. Normal-procedure notes also specify a 100°F minimum engine oil temperature for takeoff and high-power operation.
For the McCauley propeller, blade-angle specifications at the 30-inch station are 14.7° ± 0.2° at low pitch and 33.0° ± 0.5° at high pitch.
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