Generic Single-Engine Piston — Normal Procedures (FAA Airplane Flying Handbook) NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: partial Source: Airplane Flying Handbook (FAA-H-8083-3C) Rights: public_domain CC0-1.0 Checklist hash: 666eaeba85ccb8ad25f18dbebbaab29a38468002420201ed19ca5a45e812a948 Verify against the aircraft's own approved documentation before use. ======================================================================== PREFLIGHT INSPECTION -------------------- ** NOTE: Accomplish preflight inspection using the AFM/POH checklist for the specific aircraft. The sequence below is a generic reminder of the categories to cover; the specific items and their order depend on the aircraft. COCKPIT [ ] Required documents (AROW): Airworthiness certificate, Registration, Operating limitations, Weight and balance ... ON BOARD [ ] Fuel quantity: visually check tanks match gauges ... QUANTITY NOTED AND CONFIRMED [ ] Fuel selector ............................. ON FULLEST TANK OR BOTH [ ] Mixture ...................................................... RICH [ ] Master switch .................... ON — CHECK FUEL GAUGES, THEN OFF [ ] Ignition ...................................................... OFF [ ] Flight controls .............. FREE AND CORRECT SENSE — FULL TRAVEL [ ] Trim: elevator (and rudder/aileron if equipped) ... SET TO NEUTRAL FOR INSPECTION [ ] Pitot heat (if equipped) .................................. CHECKED EXTERIOR WALK-AROUND ** NOTE: Complete the exterior inspection in a consistent sequence — typically left (pilot) door, left wing, nose, right wing, right door, empennage — per the AFM/POH. [ ] Fuel: drain sample from each sump — check for water and correct grade ... CLEAR, CORRECT COLOR, NO WATER [ ] Oil: check quantity and condition .... WITHIN LIMITS, CORRECT GRADE [ ] Engine compartment: no fluid leaks, no loose items, hoses and wiring secure ... NO DISCREPANCIES [ ] Propeller: no nicks, cracks, or cord showing; hub secure ... NO DEFECTS [ ] Landing gear and tires: inflation, wear, brake line condition, no hydraulic leaks ... SERVICEABLE [ ] Wing leading edge, skin, control surfaces: no damage, hinges secure ... NO DAMAGE [ ] Flap condition and hinge pins ......................... SERVICEABLE [ ] Pitot tube: unobstructed, cover removed ..................... CLEAR [ ] Static ports: unobstructed .................................. CLEAR [ ] Empennage: control surfaces, hinges, trim tab, no damage ... SECURE, NO DAMAGE [ ] Tie-downs, chocks, and control locks ...................... REMOVED ENGINE START ------------ [ ] Passenger briefing ........... SEAT BELTS, DOOR, NO TOUCHING CONTROLS [ ] Seats and seat belts .......................... ADJUSTED AND FASTENED [ ] Brakes .......................................................... SET [ ] Fuel selector .................................. FULLEST TANK OR BOTH [ ] Circuit breakers ............................................. ALL IN [ ] Electrical equipment ............................................ OFF [ ] Avionics master ................................................. OFF [ ] Master switch (battery and alternator) ........................... ON [ ] Anti-collision light (strobe or beacon) .......................... ON [ ] Mixture .......................... RICH (or as required for altitude) [ ] Prime: per AFM/POH for engine temperature .................... PRIMED [ ] Throttle .................................. SLIGHTLY OPEN (~1/4 INCH) [ ] Look around, call "CLEAR PROP" and wait [ ] Ignition ...................................................... START [ ] Oil pressure ............ RISING WITHIN 30 SECONDS — SHUT DOWN IF NOT [ ] Avionics master .................................................. ON [ ] Engine: warm up at 1,000 RPM until oil temperature rises .... WARMING TAXI ---- ** NOTE: 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 [ ] Brakes: test at slow taxi speed ........................... EFFECTIVE BEFORE-TAKEOFF CHECK -------------------- ** GO TO: Use the before-takeoff checklist in this aircraft's AFM/POH to perform the run-up. ** CAUTION: Choose a run-up location that is firm and free of debris. The propeller may pick up pebbles and hurl them rearward. ** CAUTION: 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. [ ] Oil temperature ...................... WITHIN RANGE BEFORE HIGH POWER SYSTEMS CHECKED AND SET [ ] Fuel system .............................. ON, PROPER TANK SELECTED [ ] Trim .............................................. SET FOR TAKEOFF [ ] Flaps ............................... SET PER AFM/POH FOR DEPARTURE [ ] Flight controls ..................... FREE AND CORRECT, FULL TRAVEL [ ] Mixture .................... RICH (or set per AFM/POH for altitude) [ ] Engine operation: magneto check, carburetor heat check, RPM and temperatures ... WITHIN AFM/POH LIMITS [ ] Engine gauges: oil pressure and temperature, fuel pressure (if applicable) ... IN GREEN RANGE [ ] Electrical system: voltage, ammeter .... CHARGING, VOLTAGE IN RANGE [ ] Vacuum system (if mechanical gyros) ...................... IN RANGE [ ] Flight instruments ................ RECHECKED AND SET FOR DEPARTURE [ ] Avionics: frequencies, navigation sources, transponder code ... SET [ ] Seats and seat belts ........................ ADJUSTED AND FASTENED [ ] Doors and windows ......................................... LATCHED [ ] Takeoff briefing: runway, wind, Vr, initial turn, engine failure actions ... COMPLETE, STATED ALOUD TAKEOFF CHECKS -------------- [ ] Runway numbers vs. magnetic compass and heading indicator ..... AGREE [ ] Doors and windows .................... LATCHED AND CLOSED AS REQUIRED [ ] Controls: positioned for crosswind ....................... POSITIONED [ ] Power: advancing smoothly to full ........................... CORRECT [ ] Engine RPM at full power ......................... NORMAL PER AFM/POH [ ] Engine ....................................................... SMOOTH [ ] Engine instruments: all in green ............................. NORMAL AFTER LANDING ------------- ** WARNING: Perform the after-landing checklist only after the airplane is stopped clear of the runway. Pilots have retracted the landing gear instead of the flaps by manipulating the wrong handle while the aircraft was still moving. [ ] Slow gradually to normal taxi speed before turning off the landing runway ** GO TO: Use the after-landing checklist in this aircraft's AFM/POH. [ ] Flaps .................... RETRACTED (unless POH specifies otherwise) [ ] Carburetor heat ................................................. OFF [ ] Trim ............................................... RESET TO NEUTRAL [ ] Transponder ........................... STANDBY OR AS DIRECTED BY ATC SHUTDOWN -------- [ ] Parking brake ................................................... SET [ ] Avionics master ................................................. OFF [ ] Throttle: idle for engine cool-down per AFM/POH .............. IDLING [ ] Mixture .................. CUTOFF (to stop engine by fuel starvation) [ ] Ignition ........................................................ OFF [ ] Master switch ................................................... OFF [ ] Fuel selector ......... OFF (if aircraft has a fuel shutoff position) [ ] Control lock .............................................. INSTALLED [ ] Tie-down: chock, tie down or hangar as required ............. SECURED [ ] Pitot cover ............................................... INSTALLED