Cessna T210N — Sam_Dawson_T210_Immediate_Action_Checklist NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full Source: Cessna/T210N/Sam_Dawson_T210_Immediate_Action_Checklist.txt Rights: licensed Checklist hash: c6974bda7066a99bd563c9345b560d91a0b467ee0dacde544f6981a552751a90 Verify against the aircraft's own approved documentation before use. ======================================================================== ENGINE FAILURE DURING TAKEOFF ROLL [EMERGENCY] ----------------------------------------------- [ ] Throttle ....................................................... IDLE [ ] Brakes ........................................................ APPLY [ ] Wing Flaps .................................................. Retract [ ] Mixture ................................................ Idle Cut Off [ ] Ignition Switch ................................................. OFF [ ] Master Switch ................................................... OFF ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF [EMERGENCY] ----------------------------------------------------- [ ] Airspeed .................................................... 85 KIAS [ ] Mixture ................................................ Idle Cut Off [ ] Fuel Selector Valve ............................................. OFF [ ] Ignition Switch ................................................. OFF [ ] Wing Flaps ............................ AS REQUIRED (30° recommended) [ ] Master Switch ................................................... OFF ENGINE FAILURE IN FLIGHT [EMERGENCY] ------------------------------------- [ ] Airspeed .................................................... 85 KIAS [ ] Fuel Quantity ................................................. CHECK [ ] Fuel Selector Valve ..................................... FULLER TANK [ ] Mixture ........................................................ RICH [ ] Auxiliary Fuel Pump ... ON for 3-5 seconds with throttle ½ open; then OFF [ ] Ignition Switch ............. BOTH (or START if propeller is stopped) [ ] Throttle ............................................. ADVANCE slowly FIRE DURING ENGINE START ON GROUND [EMERGENCY] ----------------------------------------------- [ ] Ignition Switch ............ START (continue cranking to obtain start [ ] Auxiliary Fuel Pump ............................................. OFF IF ENGINE STARTS [ ] Power .................................... 1700 RPM for a few minutes [ ] Engine ......................................... SHUTDOWN and inspect IF ENGINE FAILS TO START [ ] Ignition Switch ........................... START (continue cranking) [ ] Throttle .................................................. FULL OPEN [ ] Mixture ................................................ IDLE CUT OFF [ ] Fire Extinguisher ............................................ OBTAIN [ ] Engine ... Secure. Master/Ignition Switches OFF; Fuel Selector Valve OFF [ ] Fire ...... Extinguish using fire extinguisher, wool blanket, or dirt [ ] Fire Damage ................................................. INSPECT ENGINE FIRE IN FLIGHT [EMERGENCY] ---------------------------------- [ ] Mixture ................................................ IDLE CUT OFF [ ] Fuel Selector Valve ............................................. OFF [ ] Master Switch ................................................... OFF [ ] Cabin Heat and Air ...................... OFF (except overhead vents) [ ] Airspeed ... 120 KIAS (if fire is not extinguished, increase glide speed to find an airspeed- within airspeed limits- which will provide and incombustible mixture) [ ] Forced Landing ... EXECUTE (as described in Emergency Landing Without Engine Power) ELECTRICAL FIRE IN FLIGHT [EMERGENCY] -------------------------------------- [ ] Master Switch ................................................... OFF [ ] Avionics Power Switch ........................................... OFF [ ] All Other Switches (except ignition) ............................ OFF [ ] Vents/Cabin Air/Heat ......................................... CLOSED [ ] Fire Extinguisher .......................................... ACTIVATE ** WARNING: If an oxygen system is available, occupants should use oxygen masks until smoke and discharge dry powder clears. After discharging an extinguisher within a closed cabin, ventilate the cabin. IF FIRE APPEARS OUT AND ELECTRICAL POWER IS NECESSARY FOR CONTINUANCE OF FLIGHT [ ] Master Switch .................................................... ON [ ] Circuit Breakers ............ CHECK for faulty circuit, do not reset. [ ] Radio Switches .................................................. OFF [ ] Avionics Master Switch ........................................... ON [ ] Radio/Electrical Switches ... ON one at a time, with delay after each until short circuit is localized. [ ] Vents/Cabin Air/Heat ... OPEN when it is ascertained that fire is completely extinguished. CABIN FIRE [EMERGENCY] ----------------------- [ ] Master Switch ................................................... OFF [ ] Vents/Cabin Air/Heat ......................................... CLOSED [ ] Fire Extinguisher .......................................... ACTIVATE ** WARNING: If an oxygen system is available, occupants should use oxygen masks until smoke and discharged dry powder clears. After discharging an extinguisher within a closed cabin, ventilate the cabin. [ ] Land the airplane as soon as possible to inspect for damage. WING FIRE [EMERGENCY] ---------------------- [ ] Landing/Taxi Light Switches ..................................... OFF [ ] Navigation Light Switch ......................................... OFF [ ] Strobe Light Switch ............................................. OFF [ ] Pitot Heat Switch ............................................... OFF ** NOTE: Perform a sideslip to keep the flames away from the fuel tank and cabin. Land as soon as possible using flaps only as required for final approach and touchdown. INADVERTENT ICING ENCOUNTER (POH PAGE 3-8) [ABNORMAL] ------------------------------------------------------ [ ] Pitot Heat Switch ................................................ ON [ ] Turn back or change altitude [ ] Pull cabin heat control full out and open defroster outlets. STATIC SOURCE BLOCKAGE (POH PAGE 3-9) — ERRONEOUS INSTRUMENT READING SUSPECTED [ABNORMAL] ------------------------------------------------------------------------ [ ] Static Pressure Alternate Source Valve ...................... PULL ON VACUUM SYSTEM FAILURE — LEFT OR RIGHT VACUUM ANNUNCIATOR [ABNORMAL] -------------------------------------------------------------------- ** CAUTION: If Vacuum Is Not Within Normal Operating Limits, A Failure Has Occurred in the Vacuum System and Partial Panel Procedures May be Required For Continued Flight. [ ] Vacuum Gauge .................................................. CHECK LANDING GEAR FAILS TO RETRACT [ABNORMAL] ----------------------------------------- [ ] Master Switch .................................................... ON [ ] Landing Gear Lever ............................ CHECK (lever Full UP) [ ] Landing Gear and Gear Pump Circuit Breaker ....................... IN [ ] Gear Up Light ................................................. CHECK [ ] Landing Gear Lever .......................................... RECYCLE [ ] Gear Motor ...................... CHECK Operation (ammeter and noise) LANDING GEAR FAILS TO EXTEND [ABNORMAL] ---------------------------------------- [ ] Landing Gear Lever ............................................. Down [ ] Emergency Hand Pump ... EXTEND HANDLE, and PUMP (perpendicular to handle until resistance becomes heavy--- about 35 cycles) [ ] Gear Down Light .................................................. ON [ ] Pump Handle .................................................... STOW GEAR UP LANDING [EMERGENCY] ---------------------------- [ ] Landing Gear Lever ............................................... UP [ ] Landing Gear and Gear Pump Circuit Breaker ....................... IN [ ] Runway — SELECT longest hard surface or smooth sod runway available [ ] Wing Flaps .................................. 30° (on final approach) [ ] Airspeed .................................................... 75 KIAS [ ] Doors .................................... UNLATCH PRIOR TO TOUCHDOWN [ ] Avionics Power and Master Switches ...... OFF when landing is assured [ ] Touchdown ......................................... SLIGHTLY TAIL LOW [ ] Mixture ................................................ IDLE CUT OFF [ ] Ignition Switch ................................................. OFF [ ] Fuel Selector Valve ............................................. OFF [ ] Airplane — EVACUATE LANDING WITHOUT POSITIVE INDICATION OF GEAR LOCKING [ABNORMAL] --------------------------------------------------------------- [ ] Pitot Heat Switch ................................................ ON [ ] Turn back or change altitude [ ] Pull cabin heat control full out and open defroster outlets. STATIC SOURCE BLOCKAGE (POH PAGE 3-9) — ERRONEOUS INSTRUMENT READING SUSPECTED [ ] Static Pressure Alternate Source Valve ...................... PULL ON VACUUM SYSTEM FAILURE — LEFT OR RIGHT VACUUM ANNUNCIATOR LIGHT (L VAC R ILLUMINATES) ** CAUTION: If Vacuum Is Not Within Normal Operating Limits, A Failure Has Occurred in the Vacuum System and Partial Panel Procedures May be Required For Continued Flight. [ ] Vacuum Guage .................................................. CHECK ** NOTE: Refer to expanded checklist E-12