c6974bda7066a99bd563c9345b560d91a0b467ee0dacde544f6981a552751a90 Section "Landing Without Positive Indication of Gear Locking" item count differs between passes (9 vs 3); verify nothing was dropped.

Throttle IDLE Brakes APPLY Wing Flaps Retract Mixture Idle Cut Off Ignition Switch OFF Master Switch OFF

Airspeed 85 KIAS Mixture Idle Cut Off Fuel Selector Valve OFF Ignition Switch OFF Wing Flaps AS REQUIRED (30° recommended) Master Switch OFF

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

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

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)

Master Switch OFF Avionics Power Switch OFF All Other Switches (except ignition) OFF Vents/Cabin Air/Heat CLOSED Fire Extinguisher ACTIVATE 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.

Master Switch OFF Vents/Cabin Air/Heat CLOSED Fire Extinguisher ACTIVATE 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.

Landing/Taxi Light Switches OFF Navigation Light Switch OFF Strobe Light Switch OFF Pitot Heat Switch OFF 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.

Pitot Heat Switch ON Turn back or change altitude Pull cabin heat control full out and open defroster outlets.

Static Pressure Alternate Source Valve PULL ON

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

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 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

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

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) 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 Refer to expanded checklist E-12