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Overview of the M20 series aircraft construction and airframe, including tubular steel cabin frame and laminar-flow wing.
Details the manual and electric landing gear systems, including shock absorption, brakes, steerable nose wheel, and gear position indication.
Explains the operation of dual flight controls, including aileron, rudder, and elevator trim systems.
Describes the elevator trim system which rotates the entire empennage to set the stabilizer angle of attack.
Details the electric flap system, its switch location, and extension times for various flap settings.
Details the cabin air and heating system controls, airflow routing, and defrost capabilities.
Describes the location and operation of flight and engine instruments, pitot static system, and vacuum-driven instruments.
Explains the S-TEC System 30 autopilot, its modes, yoke controls, and limitations.
Covers the aircraft's electrical system components: generator, battery, voltage regulator, and circuit breakers.
Details the integral wing tanks, fuel bladders, vents, sump drains, and selector valve operation.
Explains the ram-air feature for increased manifold pressure and its operational limitations regarding air quality and temperature.
Describes the vacuum pump system for gyroscopic instruments and the function of the standby vacuum system.
Defines the reference datum plane and its relation to fuselage stations for the M20 series aircraft.
Explains the importance of W&B records, aircraft empty weight, and payload calculations for safe loading.
Lists key airspeed limitations including Va, Vfe, Vne, and Vno for the M20 series aircraft.
Provides a chart of critical airspeeds for various phases of flight, maneuvers, and aircraft configurations.
Overview of using performance charts for optimizing performance and preventing aircraft damage.
Emphasizes the importance of thoroughly reading and frequently reviewing the POH for performance data.
Details calculations for takeoff performance based on POH charts and pilot evaluation of conditions.
Explains how to obtain and interpret cruise performance data from POH tables, considering true airspeed.
Discusses descent techniques to avoid engine shock cooling and maintain efficiency, referencing RPM and MP.
Covers landing distance determination from POH charts and factors affecting performance, like density altitude.
Highlights specific pre-flight inspection items unique to the Mooney aircraft, focusing on fuel-related items and caps.
Details proper procedures for towing the aircraft to prevent damage to the nose gear strut.
Provides step-by-step instructions for safely loading/unloading passengers and closing the aircraft door.
Instructions for adjusting the front and rear seats for pilot and passenger comfort.
Outlines the procedure for starting the fuel-injected engine, including priming and ignition.
Guidance on safe taxiing practices, emphasizing caution with prop clearance and turns.
Details the steps for engine run-up, including cowl flap operation, magnetos, and prop cycle.
Covers takeoff configuration, rotation speeds, initial climb, and post-takeoff procedures.
Guidance on transitioning to cruise, setting power, and understanding engine operation limits.
Procedures for leaning the mixture using the engine monitor for climb and cruise.
Discusses considerations for high altitude flight, including oxygen requirements and icing risks.
Techniques for efficient enroute descent to conserve fuel and protect the engine.
Covers landing risks, approach speeds, go-arounds, and landing techniques for Mooneys.
Steps for shutting down the engine and securing the aircraft, including vent and plug installation.
Instructions for cleaning the aircraft, including windshield and leading edge care.
Guidance for operating the aircraft in cold weather, including engine pre-heating and cowl plugs.
Checks and considerations for operating the aircraft at night, focusing on lighting controls.
Guidelines for using iPad/Stratus 2 as situational awareness tools, not primary instruments.
Procedure for transitioning to approach level or holding, setting power and trim.
Steps for performing an IFR/ILS descent, including gear extension and speed adjustments.
Guidance for non-precision approaches, controlling airspeed and descent rate.
Procedure for circling approaches, setting power, pitch, and flap extension.
Procedure for executing a missed approach, including climb, gear, and flap retraction.
Summary of accident study data, primary causes, and percentage distributions for Mooney aircraft.
Analysis of serious accidents attributed to pilot causes, with statistical breakdown.
Detailed breakdown of accidents by primary cause, including fatalities and aircraft damage.
Analysis of pilot characteristics and experience related to accident involvement.
Correlation between pilot experience, Mooney hours, and accident history.
Analysis of accidents caused by adverse weather, including pilot profiles and contributing factors.
Analysis of accidents attributed to poor judgment, including specific scenarios and pilot profiles.
Details accidents resulting from improper maintenance of the aircraft's engine and propeller.
Examines accidents caused by loss of control, often during landing or crosswind conditions.
Analysis of accidents linked to poor airspeed management, including long landings and stalls.
Discusses accidents caused by gear mismanagement, such as failure to extend or premature retraction.
Details accidents resulting from fuel mismanagement, like tank selection errors or running dry.
Analysis of accidents caused by improper preflight checks, particularly fuel contamination.
Covers accidents attributed to miscellaneous causes like midair collisions and strikes.
Examines accidents where the primary cause could not be determined.
Concluding summary of the accident study, referencing NTSB and NASA data sources.
General| Model | M20F |
|---|---|
| Engine | Lycoming IO-360-A1A |
| Horsepower | 200 hp |
| Fuel Capacity | 64 gallons |
| Seating Capacity | 4 |
| Height | 8 ft 4 in |
| Manufacturer | Mooney |
| Type | Single-engine, piston |
| Wingspan | 36 feet 1 inch |
| Gross Weight | 2, 740 pounds |
| Range | 700 nautical miles |
| Stall Speed | 54 knots |
