EMERGENCY PROCEDURES Flashcards
ALTERNATOR FAILURE
ALTERNATOR FAILURE
- ELECTRICAL LOAD - REDUCE
- If C.B. tripped -
a. ) Turn off ALT switch
b. ) Reset ALT C.B.
c. ) Turn on ALT (If C.B. pops, turn off ALT.) - If no C.B. pop - monitor output on voltammeter
ELECTRICAL SMOKE OR FIRE
ELECTRICAL SMOKE OR FIRE
- Battery and Alternator Switches - OFF
- Electrical Switches - OFF
- Battery and Alternator Switches – ON
- Essential Electrical Equipment - ON (Isolate defective equipment)
EMERGENCY PROCEDURES ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT
After positive control of the airplane is established: EMERGENCY PROCEDURES
ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT
- Gear and Flaps· UP
- Throttle (inoperative engine} - CLOSED
- Propeller (inoperative engine) - FEATHER
- Power (operative engine) - AS REQUIRED
- Airspeed - MAINTAIN SPEED (100 kts. MAX) UNTIL OBSTACLES ARE CLEARED After positive control of the airplane is established:
- Secure inoperative engine: a) Mixture Control - IDLE CUT-OFF b) Fuel Selector – OFF c) Auxiliary Fuel Pump – OFF d) Magneto - Start Switch – OFF e) Alternator Switch – OFF f) Cowl Flap – CLOSED
- Electrical Load - MONITOR (Maximum load of 1.0 on remaining engine)
ENGINE DRIVER FUEL PUMP FAILURE
ENGINE DRIVER FUEL PUMP FAILURE
- FUEL SELECTOR - MAIN TANK.
- AUX FUEL PUMP - ON
- COWL FLAP - OPEN
- MIXTURE - FULL RICH
- LAND - AS SOON AS PRACTICAL
NOTE: Fuel in Aux tank is unusable.
NOTE: If botn engine-driven fuel pump and aux fuel pump fail on the same side, the failing engine cannot be supplied with fuel from opposite MAIN tank since the AUX fuel pump will operate on low presure setting as long as corresponding engine-driven fuel pump is operating.
ENGINE FAILURE - TAKEOFF
ENGINE FAILURE - TAKEOFF
- Throttles - Close Immediately
- Brakes - As Required
ENGINE FAILURE AFTER TAKEOFF
ENGINE FAILURE AFTER TAKEOFF
- MIXTURES - RICH
- PROPS - FULL FORWARD
- THROTTLES - FULL FORWARD
- GEAR UP
- IDENTIFY
- VERIFY
- FEATHER
- SECURE
a. ) Fuel Selector - OFF
b. ) Aux Pump - OFF
c. ) Magneto Switch - OFF
d. ) Alternator - OFF - VXSE - 105 mph
- VYSE - 118 mph
- COWL FLAPS - CLOSED
LANDING GEAR FAILURE
LANDING GEAR FAILURE
- C.B. - Check to make sure have not tripped.
- C.B. - Pull
- Landing Gear - NEUTRAL
- Pilot’s Seat - TILT full aft
- Hand Crank - EXTEND AND LOCK
- Rotate Crank - CLOCKWISE 4 turns past point where gear lights illuminate (approx 54 turns)
- Gear Lights - Green
- Hand Crank - PUSH BUTTON and STOW
ONE ENGINE INOPERATIVE GO-AROUND
ONE ENGINE INOPERATIVE GO-AROUND
- Power - MAXIMUM
- POSITIVE RATE - GEAR UP
- STABILIZED - FLAPS - UP
- Airspeed - MAINTAIN 100 kts. MINIMUM
ONE ENGINE INOPERATIVE LANDING
On final approach and when it is certain that the field can be reached’
ONE ENGINE INOPERATIVE LANDING
On final approach and when it is certain that the field can be reached
- Landing Gear - DOWN
- Flaps - APPROACH (15°)
- Airspeed • 110 mph
- Power - maintain 800’ / min rate of descent
- Execute normal landing
SIMULATED ONE ENGINE INOP. ZERO THRUST (Simulated Feather)
SIMULATED ONE ENGINE INOP. ZERO THRUST (Simulated Feather)
The following procedure should be accomplished by alternating small reductions of propeller and then throttle, until the desired setting has been reached.
- Propeller Lever - RETARD TO FEATHER DETENT
- Throttle Lever - SET 12 in. Hg MANIFOLD PRESSURE
EMERGENCY PROC
ENGINE FAILURE DURING TAKE-OFF
If insufficient runway remains for stopping:
EMERGENCY PROC
ENGINE FAILURE DURING TAKE-OFF
- Throttles - CLOSED
- Braking - MAXIMUM If insufficient runway remains for stopping:
- Fuel Selector Valves – OFF
- Battery, Alternator, and Magneto / Start Switches – OFF
EMERGENCY PROCEDURES ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT
After positive control of the airplane is established: EMERGENCY PROCEDURES
ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT
- Gear and Flaps· UP
- Throttle (inoperative engine} - CLOSED
- Propeller (inoperative engine) - FEATHER
- Power (operative engine) - AS REQUIRED
- Airspeed - MAINTAIN SPEED (100 kts. MAX) UNTIL OBSTACLES ARE CLEARED After positive control of the airplane is established:
- Secure inoperative engine: a) Mixture Control - IDLE CUT-OFF b) Fuel Selector – OFF c) Auxiliary Fuel Pump – OFF d) Magneto - Start Switch – OFF e) Alternator Switch – OFF f) Cowl Flap – CLOSED
- Electrical Load - MONITOR (Maximum load of 1.0 on remaining engine)
EMERGENCY PROCEDURES
ENGINE FIRE ON THE GROUND
EMERGENCY PROCEDURES
- Mixture Controls - IDLE CUT-OFF
- Continue to crank affected engine
- Fuel Selector Valves - OFF
- Battery and Alternator Switches - OFF
- Extinguish with Fire Extinguisher
EMERGENCY PROCEDURES
ENGINE FIRE IN FLIGHT
EMERGENCY PROCEDURES
Shut down the affected engine according to the following procedure and land immediately.
Follow the applicable single-engine procedures in this section.
- Fuel Selector Valve - OFF
- Mixture Control - IDLE CUT-OFF
- Propeller - FEATHERED
- Aux Fuel Pump - OFF
- Maqneto / Start Switch - OFF
- Alternator Switch - OFF