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Describes the aircraft's fuel storage, selector valve, boost pump, and fuel types.
Details manual and optional electrical landing gear systems, indicators, and manual operation.
Explains the pneumatic roll stability system, its operation, and override features.
Describes the system for adjusting stabilizer pitch using a control wheel and linkage.
Details the hydraulic flap control, pump, and setting indications.
Covers the engine-driven vacuum pump, regulator, and powered systems like the artificial horizon.
Explains cabin heat from exhaust muff, air ducts, and individual outlet controls.
Discusses determining CG, max takeoff weight, and baggage limitations.
Provides instructions on cabin entry, door operation, and gear lever checks.
Outlines standard engine starting procedures and the "Push to Start" feature.
Details procedures for starting in cold conditions and with a low battery.
Describes checking the vacuum-operated step retraction and potential issues.
Lists essential documents to be carried with the aircraft at all times.
Lists certificated calibrated airspeeds for various flight conditions and maneuvers.
Details power and speed limitations for the engine.
Explains the color-coded markings on engine instruments for operating ranges.
General| Manufacturer | Mooney Aircraft |
|---|---|
| Model | M 20 C |
| Year | 1963 |
| Engine | Lycoming O-360-A1D |
| Horsepower | 180 hp |
| Maximum Speed | 170 knots (196 mph, 315 km/h) |
| Maximum Takeoff Weight | 2, 575 lb (1, 168 kg) |
| Seating Capacity | 4 |
| Type | Single-engine |
| Stall Speed | 55 mph |
| Fuel Capacity | 52 US gallons |
| Wingspan | 35 ft |
| Length | 23 ft 2 in |
| Height | 8 ft 4 in |
| Range | 780 nm (898 mi, 1, 445 km) |
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