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Overview of the aircraft's key design elements and construction.
Key technical data and specifications of the aircraft.
Description of the engine, its controls, and related systems.
Details about flight and engine instruments and their functions.
Explanation of primary flight controls, trim, and flaps.
Operation of the electric gear retraction and extension systems.
Components and functions of the aircraft's electrical system.
Heating, ventilation, and defrosting systems for cabin comfort.
Information on seats, safety belts, and cargo areas.
Procedures for preflight checks, starting, and taxiing.
Detailed steps for takeoff, climb, cruise, and landing.
Speed limits, instrument markings, and operational restrictions.
Maximum weights and center of gravity range for safe flight.
Approved maneuvers and flight load factor limits.
List of instruments and equipment required for VFR/IFR.
Normal and emergency procedures for aircraft operation.
Guidelines for proper aircraft loading and weight distribution.
Steps to manually extend the landing gear in an emergency.
Handling malfunctions of the Positive Control system.
Procedures for dealing with a loss of electrical power.
Data for takeoff distance over a 50-foot obstacle.
Data for landing distance over a 50-foot obstacle.
Information on climb rates and speeds at various altitudes.
Calibrated airspeed corrections and power-off stall speeds.
Chart for converting altitude and temperature to TAS.
Data tables for cruise speed, endurance, and range.
Procedures for towing and tying down the aircraft.
Refueling, engine lubrication, gear/tire, and battery service.
Care for propeller, exterior, interior, and required data.
General| Model | M20C |
|---|---|
| Type | Light aircraft |
| Crew | 1 |
| Passengers | 3 |
| Length | 23 ft 2 in (7.06 m) |
| Wingspan | 35 ft 0 in (10.67 m) |
| Horsepower | 180 hp (134 kW) |
| Seating | 4 |
| Manufacturer | Mooney Aircraft |
| Propeller | Two-bladed, constant speed |
| Rate of Climb | 1, 000 ft/min |
| Fuel Capacity | 52 US gallons |
| Engine | Lycoming O-360-A1A |
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