Memory Items Flashcards

1
Q

Engine Fire/Failure in Flight

A

Affected engine:

  1. Condition lever - FUEL CUTOFF
  2. Prop lever - FEATHER
  3. Firewall valve - CLOSE (EXTINGUISHER PUSH) and (CLOSED) - ILLUMINATED
  4. Fire extinguisher (if fire warning persists) - ACTUATE (DISCHARGED) - ILLUMINATED
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2
Q

EMERGENCY ENGINE SHUTDOWN ON THE GROUND

A
  1. Condition levers - FUEL CUTOFF
  2. Prop levers - FEATHER
  3. Firewall valves - CLOSE (EXTINGUISHER PUSH) and (CLOSED) - ILLUMINATED
  4. Master switch (gang bar) - OFF
  5. Battery bus switch - EMER OFF
  6. ESIS power - OFF
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3
Q

ENGINE FAILURE DURING TAKEOFF AT/BELOW V1 - TAKEOFF ABORTED

A
  1. Power Levers - GROUND FINE

2. Brakes - MAXIMUM (or as required to achieve desired stopping distance)

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4
Q

ENGINE FAILURE DURING TAKEOFF AT/ABOVE V1 - TAKEOFF CONTINUED

A
  1. VR speed - ROTATE TO APPROXIMATELY 10° PITCH ATTITUDE
  2. Gear - UP (When positive climb established)
  3. Airspeed - MAINTAIN V2 TO 400 ft AGL AND CLEAR OF OBSTACLES
  4. Prop (inoperative engine) - VERIFY FEATHERED
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5
Q

ENGINE FAILURE IN FLIGHT BELOW Vmca

A
  1. Power - REDUCE AS REQUIRED TO MAINTAIN CONTROL

2. Nose - LOWER TO ACCELERATE ABOVE Vmca

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6
Q

GLIDE (BOTH ENGINES INOPERATIVE)

A
  1. Landing Gear - UP
  2. Flaps - UP
    WARNING: Do not feather second engine propeller if a No Starter Assist air start is to be conducted. Air starts with a windmilling propeller will result in lower starting temperatures. Refer to Abnormal Procedures for Air Start Procedures.
  3. Prop Levers - FEATHERED
  4. Airspeed - 135 KTS
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7
Q

DUAL GENERATOR FAILURE [L DC GEN] and [R DC GEN]

A
  1. Instrument emergency lights (if required) - ON
  2. Generator - RESET, THEN ON
    If either generator will reset:
  3. Operating generator loadmeter - MONITOR
    If neither generator resets:
  4. ECS mode - OFF
  5. Cockpit/Cabin blower - AUTO
  6. Non-essential equipment - OFF
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8
Q

UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION

A
  1. Aircraft attitude - MAINTAIN WITH ELEVATOR CONTROL

2. AP/Trim disconnect - DEPRESS FULLY (Pitch Trim OFF) - ILLUMINATED

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9
Q

UNSCHEDULED RUDDER BOOST ACTIVATION

A
  1. AP/Trim disconnect - DEPRESS/HOLD (FIRST LEVEL)
  2. Rudder boost - OFF
    If condition persists:
  3. YD/AP DISC (on Flight Guidance Panel) - PULL DOWN
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10
Q

SPINS

A

If a spin is entered inadvertently:

  1. Control column - FULL FORWARD - AILERONS NEUTRAL
  2. Rudder - APPLY FULL OPPOSITE SPIN DIRECTION
  3. Power levers - REDUCE TO IDLE ON BOTH ENGINES

These action should be accomplished as nearly simultaneously as possible

  1. RUDDER - NEUTRALIZE - HOLD UNTILE ROTATION STOPS
  2. Execute smooth pullout
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11
Q

ELECTRICAL SMOKE OR FIRE

A

WARNING: Dissipation of smoke is not sufficient evidence that a fire has been extinguished. If it cannot be visually confirmed that no fire exists, land at the nearest suitable airport.

  1. Oxygen mask(s) - DON
  2. Mask selector switch - EMERG
  3. Mic switch(es) - OXY
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12
Q

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A

Oxygen:

  1. Crew mask - DON
  2. Mask selector switch - EMERG
  3. Mic selector - OXY
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13
Q

AIRSTAIR/CARGO DOOR UNLOCKED

A

WARNING: Do not attempt to check the security of the airstair door or cargo door in flight. Remain as far from the door as possible with seat belts securely fastened.
If the [DOOR UNLOCKED] Illuminates, of If An Unlatched Airstair Door/Cargo Door is Suspected:

  1. All occupants - SEATED WITH SEAT BELTS SECURELY FASTENED
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14
Q

EMERGENCY DESCENT

A
  1. Power levers - IDLE
  2. Prop levers - FULL FORWARD
  3. Flaps - APPROACH/202 KTS MAX
  4. Landing gear - DOWN/184 KTS MAX
  5. Airspeed - 184 KTS MAX
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15
Q

OXYGEN USE

A

Crew System:

  1. Crew mask - DON
  2. Mic Switches - OXYGEN MASK
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16
Q

PRESSURIZATION LOSS [CABIN ALT HI]

A
  1. Oxygen mask(s) - DON
  2. Mic switch(es) - OXYGEN MASK
  3. Passenger manual drop out - PULL ON [PASS OXYGEN ON] - ILLUMINATED
  4. Descent - AS REQURED

WARNING: The highest recommended cabin altitude for sustained flight is 25,000 ft.

17
Q

HIGH DIFFERENTIAL PRESSURE

A
  1. Bleed air valve switches - ENVIR OFF
  2. Oxygen
    (crew and passengers) - AS REQUIRED
  3. Descend as required
18
Q

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE

A
  1. Passenger manual dropout - PULL ON
19
Q

BLEED AIR FAILURE

A

If illuminated during flight:

  1. Bleed air valve switch
    (affected engine) - PNEU/ENVIR OFF
20
Q

AUTOPILOT MISTRIM [E] or [A]

A

WARNING: Intentional or automatic disengagement of the autopilot without restraining the control wheel during mistrim condition will produce a significant airplane response in the direction of the mistrim force.

If a Mistrim Indication continues for more than a few seconds:

  1. Flight controls - HOLD FIRMLY
    (Control forces may exceed 25 lbs)
  2. AP - DISENGAGE
21
Q

AUTOPILOT TRIM FAIL [TRIM]

A
  1. Flight controls - HOLD FIRMLY

2. AP - DISENGAGE

22
Q

AUTOPILOT AUTOMATIC DISENGAGEMENT

A

If an Automatic Disengagement occurs:

  1. Maintain airplane control
  2. AP/TRIM disconnect - DEPRESS TO 1st LEVEL TO CANCEL HORN
23
Q

EGPWS in IMC or NIGHT

A
  1. Wings - LEVEL
  2. Power - MAX ALLOWABLE
  3. Pitch - INCREASE
    - Promptly and smoothly increase pitch toward an initial pitch attitude of 20° to 25°
    - Adjust as required to avoid continuous buffeting and/or stall warning
    - Adjust to maintain 125 KIAS
  4. Gear and Flaps - UP
24
Q

TAWS+ in IMC or NIGHT

A
  1. Autopilot - DISENGAGE
  2. Wings - LEVEL
  3. Power - MAX ALLOWABLE
  4. Pitch - INCREASE
    - Promptly and smoothly increase pitch toward an initial pitch attitude of 20° to 25°
    - Adjust as required to avoid continuous buffeting and/or stall warning
    - Adjust to maintain 125 KIAS
  5. Gear and Flaps - UP
25
Q

ENG FIRE ON GROUND

A
  1. Condition Lever - FUEL CUTOFF
  2. Firewall Fuel Valve - CLOSE (EXTINGUISHER PUSH AND CLOSED) - ILLUMINATED
  3. Starter Switch - STARTER ONLY
  4. Fire Extinguisher [if fire warning persists] - ACTUATE [DISCHARGED] - ILLUMINATED