Memory Itens Flashcards

1
Q

EMERGENCY ENGINE SHUTDOWN

•Engine torque increase - unschedule in flight (not responsive to power lever movement)
• Engine fire in flight
• Engine failure in flight
• Low oil pressure

A

AFFECTED ENGINE

  1. Condition Lever - - - - - FUEL CUTOFF
  2. Propeller Lever - - - - - FEATHER
  3. Fuel FW Shutoff Valve - - - - - CLOSE
  4. Fire Extinguisher (if installed) (if fire warning persists) - - - - - ACTUATE
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2
Q

ENGINE FIRE ON GROUND

A

AFFECTED ENGINE

  1. Condition Lever - - - - - FUEL CUTOFF
  2. Fuel FW Shutoff Valve - - - - - CLOSE
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3
Q

ENGINE FAILURE DURING GROUND ROLL

A
  1. Power Lever - - - - - GROUND FINE
  2. Brakes - - - - - MAXIMUM (or as required to achieve stopping performance)

If Insufficient Runway Remains for Stopping

  1. Condition Lever - - - - - FUEL CUTOFF
  2. Fuel FW Shutoff Valve - - - - - CLOSE
  3. Master Switch - - - - - OFF (Gang Bar down)
  4. Boost Pumps - - - - - OFF
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4
Q

ENGINE FAILURE AFTER LIFT-OFF
(IF CONDITIONS PRECLUDE AN IMMEDIATE LANDING)

A
  1. Maximum Continuous Power - - - - SET
  2. Airspeed - - - - - MAINTAIN (Takeoff Speed or above)
  3. Landing Gear - - - - - UP
  4. Propeller (inoperative engine) - - - - - FEATHER (or verify FEATHER if Autofeather is installed)
  5. Airspeed (after obstacle clearance altitude is reached) - - - - - 108 KNOTS
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5
Q

ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (VMcA)

A
  1. Power - - - - - REDUCE
  2. Nose - - - - - LOWER TO ACCELERATE ABOVE VMcA
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6
Q

2ND ENGINE FLAMEOUT

A
  1. Power Lever - - - - - IDLE
  2. Propeller - - - - - DO NOT FEATHER
  3. Condition Lever - - - - - FUEL CUTOFF
  4. Conduct Air Start Procedures in Abnormal Procedures
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7
Q

ELECTRICAL SMOKE OR FIRE OR ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A
  1. Oxygena. Oxygen System Control - - - - - CONFIRM ON
    b. Crew - - - - - DON MASKS
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8
Q

CABIN DOOR UNLOCKED

A

If the [CABIN DOOR] Illuminates, or If an Unlocked Cabin Door Is Suspected:

1 . All Occupants - - - - - SEATED WITH SEAT BELTS SECURELY FASTENED

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9
Q

EMERGENCY DESCENT

A
  1. Power Levers - - - - - IDLE
  2. Propeller Levers - - - - - HIGH RPM
  3. Flaps (184 knots maximum) - - - - - APPROACH
  4. Landing Gear (182 knots maximum) - - - - - DOWN
  5. Airspeed - - - - - 182 KNOTS MAXIMUM
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10
Q

GLIDE

A
  1. Landing Gear - - - - - UP
  2. Flaps - - - - - UP
  3. Propellers - - - - - FEATHERED
  4. Airspeed - - - - - 125 KNOTS
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11
Q

UNSCHEDULED ELECTRIC ELEVATOR TRIM

A
  1. Maintain pitch control with elevator
  2. Control Wheel Trim Switch - - - - - ATTEMPT TO TRIM IN OPPOSITE DIRECTION OF RUNAWAY
  3. Elevator Trim Switch (Pedestal) - - - - - OFF
  4. Manual Trim - - - - - RETRIM AS REQUIRED
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12
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. Rudder Boost - - - - - OFF
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13
Q

USE OF OXYGEN

A
  1. Oxygen System Control - - - - - CONFIRM ON
  2. Crew - - - - - DON MASKS
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14
Q

PRESSURIZATION LOSS [CABIN ALT HI]

A
  1. Oxygen System Control - - - - - CONFIRM ON
  2. Crew - - - - - DON MASKS
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15
Q

HIGH DIFFERENTIAL PRESSURE

A

Anytime the Differential Pressure Goes Into the Red Arc:
1. Cabin Altitude Controller - - - - SELECT HIGHERCABIN ALTITUDE SETTING

If Condition Persists:
2. Bleed Air Valves - - - - - CLOSE
3. Cabin Pressure (after cabin is depressurized) - - - - - DUMP
4. Bleed Air Valves - - - - - OPEN

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16
Q

EMERGENCY EXIT

A
  1. Emergency Release Hatch Cover - - - - - OPEN
  2. Release Button - - - - - PUSH
  3. If release button will not push, PULL hooks to override pressure lock and then PUSH the release button
  4. PULL handle and PUSH out hatch
17
Q

SPINS

A
  1. Control Column - - - - - FULL FORWARD, AILERONS NEUTRAL
  2. Full Rudder - - - - - OPPOSITE THE DIRECTION OF SPIN
  3. Power Levers - - - - - IDLE
  4. Rudder - - - - - NEUTRALIZE WHEN ROTATION STOPS
  5. Execute a smooth pullout