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Manual contains FAA approved limitations that must be carried onboard.
Details Mooney's warranty coverage for the aircraft and its components.
Overview of the aircraft's main design aspects including airframe, power plant, controls, and gear.
Key technical specifications for power plant, propeller, landing gear, fuel, oil, weight, and baggage.
Details on engine controls, ignition, fuel, oil, cooling, and vacuum systems.
Information on primary controls, positive control, trim, and flap controls.
Operation of electric gear retraction, emergency extension, and brakes.
Operation of alternator, battery, circuit breakers, and lighting systems.
Details on heating, ventilation, and defrosting systems.
Covers preflight checks, engine starting, warmup, and taxiing procedures.
Details takeoff, climb, cruise, stall, spin, landing, and shutdown procedures.
Specifies critical airspeed, power plant, weight, load factor, and maneuver limits.
Lists instruments and equipment necessary for VFR and IFR operations.
Step-by-step procedure for manual landing gear extension.
Data for takeoff distance over a 50-foot obstacle.
Data for landing distance over a 50-foot obstacle.
Tables detailing climb performance at various altitudes and conditions.
Data on cruise speed, fuel consumption, and range.
Procedures for towing and tying down the aircraft.
Covers refueling, engine lubrication, gear, tire, and battery service.
Information on propeller, exterior, and interior care.
General| Model | M20 F |
|---|---|
| Engine | Lycoming IO-360-A1A |
| Crew | 1 |
| Capacity | 3 passengers |
| Seating Capacity | 4 |
| Manufacturer | Mooney Aircraft |
| Type | Single-engine propeller aircraft |
| Horsepower | 200 hp |
| Height | 8.3 ft (2.5 m) |
| Empty weight | 1, 700 lb |
| Fuel capacity | 64 US gallons (242 L) |
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