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Fly Exclusive > Memory items - emergency > Flashcards

Memory items - emergency Flashcards

1
Q

Engine failure/fire - V1 take off rejected

A

Takeoff: Abort

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2
Q

Engine failure/fire - V1 take off continued

A
  1. Climb to safe altitude.
  2. WING XFLOW ICE PROTECTION Switch: ON
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3
Q

Engine failure during final approach

A
  1. Thrust (operating eng) - Increase
  2. Airspeed - Vapp
  3. Flaps - Takeoff and approach
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3
Q

EMERGENCY RESTART – TWO ENGINES

A
  1. Throttles (both): OFF
  2. BATTERY SWITCH (if descent to FL200 will take longer than 5 mins): EMBER
    · Altitude: At or Below FL200
  3. BATTERY SWITCH: ON
  4. WING/ENG ICE PROTECTION: Switches (both): OFF
  5. Airspeed: 230 KIAS Minimum (Altitude permitting)
  6. Throttles (both): IDLE
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4
Q

ELECTRICAL FIRE OR SMOKE

A
  1. Oxygen Masks: DON and EMER
  2. Microphone Select Switches: MIC OXY MASK
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5
Q

ENVIRONMENTAL SYSTEM SMOKE OR ODOR

A
  1. Oxygen Masks: DON and EMER
  2. Microphone Select Switches: MIC OXY MASK
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6
Q

SMOKE REMOVAL

A
  1. Oxygen Masks: DON and EMER
  2. Microphone Select Switches: MIC OXY MASK
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7
Q

CABIN ALT (CABIN ALTITUDE)

A
  1. Oxygen Masks: DON and 100%
  2. Microphone Select Switches: MIC OXY MASK
  3. Emergency Descent: AS REQUIRED
  4. OXYGEN CONTROL VALVE Selector: MANUAL DROP, As Required
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8
Q

EMERGENCY DESCENT

A
  1. AP TRIM DISC Button: PRESS and RELEASE
  2. Throttles: IDLE
  3. Speed Brakes: EXTEND
  4. Airplane Pitch Attitude: INITIALLY TARGET 7.5 DEGREES NOSE DOWN
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9
Q

BATT FAULT/BATT FAIL (BATTERY OVERTEMPERATURE)

A
  1. Battery Volt/Amp: NOTE
  2. Battery Switch: EMER
  3. Volt/Amp: NOTE DECREASE
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10
Q

BATT O’TEMP (BATTERY OVERTEMPERATURE)

A
  1. Volt/Amp: NOTE
  2. Battery Switch: EMER
  3. Volt/Amp: NOTE DECREASE
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11
Q

AUTOPILOT MALFUNCTION

A
  1. AP TRIM DISC Button: PRESS AND RELEASE
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12
Q

ELECTRIC ELEVATOR TRIM RUNAWAY

A
  1. AP TRIM DISC Button: PRESS and RELEASE
  2. Throttles: AS REQUIRED
  3. Speed Brakes: AS REQUIRED
  4. Manual Elevator Trim: AS REQUIRED
  5. PITCH TRIM Circuit Breaker (LP-C13R4): Pull
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13
Q

EMERGENCY EVACUATION

A
  1. Parking Brake: SET
  2. Throttles: BOTH OFF
  3. LH/RH ENG FIRE Buttons: BOTH PRESS
  4. Illuminated BOTTLE ARMED Buttons: BOTH PRESS (if fire suspected)
  5. Battery Switch: OFF
  6. Emergency Locator Transmitter (ELT): MAKE SURE SYSTEM IS ACTIVATED (if required for search and rescue services)
  7. Airplane and Immediate Area: CHECK FOR BEST ESCAPE ROUTE
  • IF THRU CABIN DOOR
    8. Cabin Door: OPEN
    9. Move away from airplane
    Procedure completed
  • IF THRU EMERGENCY EXIT
    8. Emergency Exit Door: REMOVE and THROW EXIT DOOR OUT OF AIRPLANE
    9. Move away from airplane
    Procedure completed
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14
Q

INADVERTENT STALL (STICK SHAKER, BUFFET, AND/OR ROLL-OFF)

A
  1. AP/TRIM DISC Button: PUSH
  2. Pitch Attitude: Reduce Approximately 5°
  3. Roll Attitude: Level
  4. Throttles: TO
  5. Airspeed: Increase 5 KIAS, Minimum
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15
Q

WHEEL BRAKE FAILURE

A
  1. Brake Pedals: Remove Feet
  2. EMER BRAKE Handle: Pull as Required
  3. Directional Control: Maintain with Nosewheel Steering
16
Q

TCAS RESOLUTION ADVISORY (RA) ALERTS (TCAS II ONLY)

A
  1. Autopilot: Disengage
  2. Initiate corrective action per PFD guidance.
17
Q

ENGINE FIRE L or R

A
  1. Throttle (affected side): IDLE IF Light Remains On After 15 Seconds
  2. Illuminated ENG FIRE Button: PUSH If Light Remains ON After Additional 15 Seconds
  3. Illuminated BOTTLE ARMED Button: PUSH
18
Q

What does the RED SMOKE AFT or FWD

A

Smoke has been detected in the baggage compartment. This will stay on for the remainder of the flight, even if the smoke dissipates.
1. Land as soon as possible

19
Q

What does the RED GENERATOR OFF L and R

A

Both generators are inoperative. The air conditioner and cabin items will turn off automatically.

20
Q

What does the RED NO TAKEOFF

A

Aircraft is not configured for safe takeoff

21
Q

What does the RED OIL PRESSURE LOW L or R

A

Oil pressure is below limits

22
Q

During the Ice Protection Test, the temperature of the ITT split is 50° or more.

A

Do not depart, maintenance is required.

23
Q

Ice protection system test

A
  1. Throttle - N2 - 75% or above
  2. WING/ENG A/I PROTECTION switches - WING/ENG
  3. White WING/ENG A/I ON, WING A/I COLD L-R, and ENGINE A/I COLD L-R messages - displayed
  4. TAIL ICE PROTECTION switch - AUTO
  5. White TAIL DE-ICE On message - displayed
  6. WINDSHIELD ANTI-ICE BLEED AIR Knobs - MAX
  7. WINDSHIELD ANTI-ICE BLEED Switch - Low - check for bleed air noise
  8. White WING/ENG A/I COLD and ENGINE A/I COLD messages - clear within 2 minutes
  9. Amber WING A/I COLD, ENGINE A/I COLD, and TAIL DE-ICE FAIL messages - NOT DISPLAYED
  10. Ice protection switches - OFF
  11. Throttles - as required

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