b9185db02f250a23fc68da70577262de0d6d318ef3cb5fc6f8ef149088d76614 Covers taxi, before-takeoff, takeoff and after-landing checks only. Contains no preflight inspection, no engine start, no in-flight and no emergency procedures. Type-generic by construction. Every aircraft-specific value (RPM for the magneto check, vacuum range, flap settings, speeds) is either absent or a Handbook illustration, not a limitation for any real aircraft. The Handbook's numbered takeoff checks are phrased as questions. They are rendered here as action/response pairs, which is an interpretation rather than a transcription.

Taxi checks are sometimes specified by the AFM/POH; accomplish any items that are required. Where none are specified, use the taxi to verify and cross-check the flight instruments. Airspeed indicator AT OR NEAR ZERO Attitude indicator PITCH AND ROLL LEVEL, NO FLAGS Altimeter FIELD ELEVATION WITHIN LIMITS Turn indicator CORRECT DIRECTION, BALL OUTSIDE TURN, NO FLAGS Directional gyro SET AND CROSS-CHECKED TO MAGNETIC COMPASS Vertical speed indicator ZERO

Use the before-takeoff checklist in this aircraft's AFM/POH to perform the run-up. Choose a run-up location that is firm and free of debris. The propeller may pick up pebbles, dirt, sand or other loose objects and hurl them rearward, damaging the propeller and possibly the tail. Prolonged ground operation may overheat the cylinders long before oil temperature indicates a rise. Head as nearly as possible into the wind, and monitor cylinder head temperature if equipped. Allow the airplane to roll forward slightly to align the nosewheel or tailwheel with the longitudinal axis Oil temperature WITHIN RANGE BEFORE HIGH POWER Many engines require oil temperature to reach a minimum value stated in the AFM/POH before takeoff power is applied. Systems checked and set Fuel system ON, PROPER TANK SELECTED Trim SET FOR TAKEOFF Includes elevator, and may also include rudder and aileron trim. Flight controls FREE AND CORRECT, FULL TRAVEL Full aileron, elevator and rudder deflection in all directions. A partial range of movement is not acceptable. Engine operation TEMPERATURES AND PRESSURES NORMAL, IGNITION AND CARBURETOR HEAT CHECKED Magneto or FADEC operation within limits. Where a constant-speed or feathering propeller is fitted, check that the engine continues to run normally as the propeller is exercised. Electrical system VOLTAGE IN RANGE, BATTERY CHARGING Vacuum system IN RANGE If equipped Typically between 4.8 and 5.2 inches of mercury at 2,000 RPM; refer to the AFM/POH for the manufacturer's values. Mechanical gyroscopic instruments need adequate time to spool up before departure. Flight instruments RECHECKED AND SET FOR DEPARTURE Verify the directional gyro and magnetic compass agree. A heading bug may be set to the runway heading in use or as assigned by ATC. Avionics SET Frequencies, initial navigation sources and courses, autopilot preselects and transponder code. Takeoff briefing COMPLETE, OUT LOUD Made out loud by the pilot even when no other person is there to listen. Includes visual verification of the correct surface and direction, to preclude a wrong-surface departure; the type of takeoff, runway, wind, rotation speed, initial turn and altitude; and the actions planned for engine failure below rotation speed, after rotation with runway remaining, and after rotation with no runway remaining.

Runway numbers vs. magnetic compass and heading indicator AGREE Doors and windows LATCHED AND CLOSED AS REQUIRED Controls POSITIONED FOR CROSSWIND Power CORRECT Engine RPM NORMAL Engine SMOOTH Engine instruments NORMAL, IN GREEN RANGES

Perform the after-landing checklist only after the airplane is stopped clear of the runway holding position markings. Pilots have retracted the landing gear instead of the flaps by manipulating the wrong handle while the airplane was still moving. Slow gradually to normal taxi speed with normal brake pressure before turning off the landing runway Any significant degree of turn at faster speeds could damage the landing gear, tires, brakes or airframe. This sequence may be modified where the manufacturer recommends that specific after-landing items be accomplished during the landing rollout, for example retracting flaps to improve braking after a short-field landing. Positively identify the flap control before moving it. Use the after-landing checklist in this aircraft's AFM/POH.