MC-12 Emergency Procedures Flashcards

1
Q

FLIGHT CONTROLS MALFUNCTIONS

Unscheduled Rudder Boost Activation

A
  1. Autopilot/trim disconnect switch – Press to first
    detent and hold
  2. RUDDER BOOST switch – OFF
  3. Autopilot/trim disconnect switch – Release
    If condition persists:
  4. YD/AP DISC switch (on flight guidance panel) –
    Pull down
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2
Q

Autopilot Mistrim [TRIM]

A
  1. Flight Controls – Hold firmly. (control forces may exceed 25 lb)
  2. Autopilot – Disengage
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3
Q

Engine Failure After V1

A
  1. POWER – Maximum allowable
  2. LANDING GEAR CONTROL handle (positive rate of climb confirmed) – UP
  3. Airspeed – Maintain V2 until 400’ AGL and clear of obstacles
  4. Propeller (affected engine) – Verify feathered. If propeller does not autofeather, perform manual feather
  5. FLAPS (after Vyse) – UP
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4
Q

FIRE

Engine Fire in Flight (Identified)

A
  1. POWER lever (affected engine) – IDLE
  2. PROP lever (affected engine) – FEATHER
  3. CONDITION lever (affected engine) – FUEL CUTOFF
  4. F/W VALVE PUSH switch - Push Ensure CLOSED and EXTINGUISHER PUSH illuminated
  5. EXTINGUISHER PUSH switch – PUSH Ensure DISCHARGE illuminates
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5
Q

Single Engine Go Around

A
  1. POWER – Maximum allowable/controllable
  2. LDG GEAR CONTROL handle – UP
  3. FLAPS – UP
  4. Airspeed – VYSE
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6
Q

Cracked Cabin Window

A
  1. Crew oxygen masks - ON
  2. MIC switches - OXY
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7
Q

Spins

A
  1. Autopilot and yaw damper - Disengage
  2. Control Wheel – Full forward, ailerons neutral
  3. Full Rudder – Opposite the direction of the spin
  4. POWER levers - IDLE
  5. Rudder – Neutralize when rotation stops
  6. Execute a smooth recovery
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8
Q

PROPELLER MALFUNCTIONS

Primary & Overspeed Governors Failed (Above 1768 RPM)

A
  1. POWER lever (affected engine) - IDLE.
  2. PROP lever (affected engine) -
    FEATHER.
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9
Q

Engine Failure During Flight

A
  1. Autopilot/yaw damper – Disengage
  2. POWER – As required
  3. Failed Engine – Identify
  4. Propeller (affected engine) – Verify feathered. If propeller does not autofeather, perform manual
    feather
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10
Q

Engine Failure During Final Approach (After Flaps Full Down)

A
  1. POWER - As required.
  2. Landing Gear - Confirm down
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11
Q

FIRE

Wing Fire

A
  1. ENGINE SHUTDOWN IN FLIGHT (affected side) –Perform
  2. Land as soon as possible.
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12
Q

FIRE

Fuselage Fire

A
  1. Fight the fire.
  2. Land as soon as possible.
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13
Q

FIRE

Environmental System Smoke or Fumes

A
  1. Crew oxygen masks - EMER and don.
  2. MIC switches - OXY.
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14
Q

Door Unlock Warning Annunciator Illuminated

A

1 . All occupants - Seated with seatbelts securely fastened.

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15
Q

ENVIRONMENTAL SYSTEMS

L or R Bleed Air Fail Annunciator Illuminated

A
  1. BLEED AIR VALVES switch (affected engine) - PNEU & ENVIR OFF.
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16
Q

ENVIRONMENTAL SYSTEMS

Excessive Differential Pressure (Cabin Diff HI Annunciator Illuminated)

A
  1. BLEED AIR VALVES switches – ENVIR OFF
  2. Crew oxygen masks – EMER and don (as
    required)
  3. MIC switches – OXY (as required)
  4. PASSENGER MANUAL DROPOUT handle – Pull
    on
  5. Descend – As required
17
Q

ENVIRONMENTAL SYSTEMS

Loss of Pressurization

(CABIN ALT and/or
Cabin ALT Hi Annunciator Illuminated)

A
  1. Crew oxygen masks - EMER and don.
  2. MIC switches - OXY
  3. PASSENGER MANUAL DROP OUT handle - Pull on.
  4. Descend - As Required
18
Q

ELECTRICAL SYSTEM

Both DC Gen Lights Illuminated

A
  1. INSTRUMENT EMERG LTS – (as required)
  2. MISSION PWR switch – Off
  3. GEN switches – GEN RESET, then ON
    If either generator resets:
  4. Operating generator DC % lLOAD meter –
    Monitor (100% maximum)
    If neither generator will reset:
  5. ENVIRONMENTAL MODE switch – OFF
  6. COCKPIT/CABIN BLOWER knobs – AUTO
  7. Non-essential equipment – Off
19
Q

EMERGENCY DESCENT

A
  1. POWER levers – IDLE
  2. PROP levers – HIGH RPM
  3. FLAPS (202 KIAS maximum) – APPROACH
  4. LDG GEAR CONTROL handle (182 KIAS
    maximum) – DN/confirm
  5. Airspeed – 182 KIAS maximum
20
Q

Stalls (Departure from Controlled Flight)

A
  1. Autopilot and yaw damper - Disengage
  2. Aircraft pitch – Apply pitch control input to
    reduce angle of attack
  3. Aircraft bank – Wings level
  4. POWER – As required
  5. Execute a smooth recovery
21
Q

FLIGHT CONTROLS MALFUNCTIONS

Unscheduled Electric Elevator Trim

A
  1. Aircraft attitude – Maintain using elevator control
  2. Autopilot/trim disconnect switch – Press fully and hold. Verify TRIM illuminated
22
Q

FIRE

Engine/Nacelle Fire during Start or Ground Operations

A
  1. PROP levers – FEATHER
  2. CONDITION levers – FUEL CUTOFF
  3. F/W VALVE PUSH switch – Push Ensure CLOSED
    and EXTINGUISHER PUSH illuminated
  4. EXTINGUISHER PUSH switch – PUSH
  5. MASTER SWITCH – OFF
  6. BAT BUS switch – EMER OFF
23
Q

Engine Failure (Second Engine)

A
  1. Airspeed - As required.
  2. POWER lever - IDLE.
  3. PROP lever - As required.
24
Q

Engine Failure Before V1 (Abort)

A
  1. POWER levers – GND FINE
  2. Braking – As required
25
Q

Autopilot Mistrim [E] OR [A)

A
  1. Flight controls - Hold firmly. Control forces may exceed 25 pounds.
  2. Autopilot - Disengage.
26
Q

Unexpected AP disengagement

A
  1. Aircraft Control - Maintain
  2. Autopilot/trim disconnect switch – Press to first level to cancel horn.
27
Q

Maximum Glide

A
  1. LDG GEAR CONTROL handle – UP
  2. FLAPS – UP
  3. PROP levers – FEATHER
  4. Airspeed – 135 KIAS
28
Q

FIRE

Electrical Smoke or Fire

A
  1. Crew oxygen masks - EMER and don.
  2. MIC switches - OXY.
29
Q

Engine Failure during Flight Below VMCA

A
  1. POWER - Reduce as required to maintain control
  2. Pitch attitude - Lower to accelerate above VMCA.
30
Q

Passenger Oxygen Auth-Deployment System Failure (Cabin ALT HI Annunciator Illuminated and Pass Oxygen on Annunciator Extinguished)

A
  1. PASSENGER MANUAL DROP OUT handle – Pull on