EMERGENCY PROCEDURES Flashcards

1
Q

ALTERNATOR FAILURE

A

ALTERNATOR FAILURE

  1. ELECTRICAL LOAD - REDUCE
  2. 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.)
  3. If no C.B. pop - monitor output on voltammeter
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2
Q

ELECTRICAL SMOKE OR FIRE

A

ELECTRICAL SMOKE OR FIRE

  1. Battery and Alternator Switches - OFF
  2. Electrical Switches - OFF
  3. Battery and Alternator Switches – ON
  4. Essential Electrical Equipment - ON (Isolate defective equipment)
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3
Q

EMERGENCY PROCEDURES ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT

After positive control of the airplane is established: EMERGENCY PROCEDURES

A

ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT

  1. Gear and Flaps· UP
  2. Throttle (inoperative engine} - CLOSED
  3. Propeller (inoperative engine) - FEATHER
  4. Power (operative engine) - AS REQUIRED
  5. Airspeed - MAINTAIN SPEED (100 kts. MAX) UNTIL OBSTACLES ARE CLEARED After positive control of the airplane is established:
  6. 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
  7. Electrical Load - MONITOR (Maximum load of 1.0 on remaining engine)
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4
Q

ENGINE DRIVER FUEL PUMP FAILURE

A

ENGINE DRIVER FUEL PUMP FAILURE

  1. FUEL SELECTOR - MAIN TANK.
  2. AUX FUEL PUMP - ON
  3. COWL FLAP - OPEN
  4. MIXTURE - FULL RICH
  5. 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.

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5
Q

ENGINE FAILURE - TAKEOFF

A

ENGINE FAILURE - TAKEOFF

  1. Throttles - Close Immediately
  2. Brakes - As Required
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6
Q

ENGINE FAILURE AFTER TAKEOFF

A

ENGINE FAILURE AFTER TAKEOFF

  1. MIXTURES - RICH
  2. PROPS - FULL FORWARD
  3. THROTTLES - FULL FORWARD
  4. GEAR UP
  5. IDENTIFY
  6. VERIFY
  7. FEATHER
  8. SECURE
    a. ) Fuel Selector - OFF
    b. ) Aux Pump - OFF
    c. ) Magneto Switch - OFF
    d. ) Alternator - OFF
  9. VXSE - 105 mph
  10. VYSE - 118 mph
  11. COWL FLAPS - CLOSED
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7
Q
A
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8
Q

LANDING GEAR FAILURE

A

LANDING GEAR FAILURE

  1. C.B. - Check to make sure have not tripped.
  2. C.B. - Pull
  3. Landing Gear - NEUTRAL
  4. Pilot’s Seat - TILT full aft
  5. Hand Crank - EXTEND AND LOCK
  6. Rotate Crank - CLOCKWISE 4 turns past point where gear lights illuminate (approx 54 turns)
  7. Gear Lights - Green
  8. Hand Crank - PUSH BUTTON and STOW
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9
Q

ONE ENGINE INOPERATIVE GO-AROUND

A

ONE ENGINE INOPERATIVE GO-AROUND

  1. Power - MAXIMUM
  2. POSITIVE RATE - GEAR UP
  3. STABILIZED - FLAPS - UP
  4. Airspeed - MAINTAIN 100 kts. MINIMUM
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10
Q

ONE ENGINE INOPERATIVE LANDING

On final approach and when it is certain that the field can be reached’

A

ONE ENGINE INOPERATIVE LANDING

On final approach and when it is certain that the field can be reached

  1. Landing Gear - DOWN
  2. Flaps - APPROACH (15°)
  3. Airspeed • 110 mph
  4. Power - maintain 800’ / min rate of descent
  5. Execute normal landing
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11
Q

SIMULATED ONE ENGINE INOP. ZERO THRUST (Simulated Feather)

A

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.

  1. Propeller Lever - RETARD TO FEATHER DETENT
  2. Throttle Lever - SET 12 in. Hg MANIFOLD PRESSURE
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12
Q

EMERGENCY PROC

ENGINE FAILURE DURING TAKE-OFF

If insufficient runway remains for stopping:

A

EMERGENCY PROC

ENGINE FAILURE DURING TAKE-OFF

  1. Throttles - CLOSED
  2. Braking - MAXIMUM If insufficient runway remains for stopping:
  3. Fuel Selector Valves – OFF
  4. Battery, Alternator, and Magneto / Start Switches – OFF
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13
Q

EMERGENCY PROCEDURES ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT

After positive control of the airplane is established: EMERGENCY PROCEDURES

A

ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT

  1. Gear and Flaps· UP
  2. Throttle (inoperative engine} - CLOSED
  3. Propeller (inoperative engine) - FEATHER
  4. Power (operative engine) - AS REQUIRED
  5. Airspeed - MAINTAIN SPEED (100 kts. MAX) UNTIL OBSTACLES ARE CLEARED After positive control of the airplane is established:
  6. 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
  7. Electrical Load - MONITOR (Maximum load of 1.0 on remaining engine)
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14
Q

EMERGENCY PROCEDURES

ENGINE FIRE ON THE GROUND

A

EMERGENCY PROCEDURES

  1. Mixture Controls - IDLE CUT-OFF
  2. Continue to crank affected engine
  3. Fuel Selector Valves - OFF
  4. Battery and Alternator Switches - OFF
  5. Extinguish with Fire Extinguisher
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15
Q

EMERGENCY PROCEDURES

ENGINE FIRE IN FLIGHT

A

EMERGENCY PROCEDURES

Shut down the affected engine according to the following procedure and land immediately.

Follow the applicable single-engine procedures in this section.

  1. Fuel Selector Valve - OFF
  2. Mixture Control - IDLE CUT-OFF
  3. Propeller - FEATHERED
  4. Aux Fuel Pump - OFF
  5. Maqneto / Start Switch - OFF
  6. Alternator Switch - OFF
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