Memory Itens Flashcards

1
Q

ENGINE FAILURE DURING TAKEOFF (BELOW V1 - TAKEOFF ABORTED)

A
  1. Brakes………………………..APPLY 2.Thrust………………………….IDLE 3.ThrustReverser(s)………..DEPLOY
  2. Reverser Nights………….VERIFY
  3. Reverse Thrust…………AS REQUIRED 6.SpeedBrakes……………..EXTEND
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2
Q

ENGINE FAILURE DURING TAKEOFF (ABOVE V1 - TAKEOFF CONTINUED)

A
  1. Nose Up Pitch Attitude at Rotation (VR) …………. 13 - 15° DESIRED
  2. Landing Gear (when positive climb established)…………………..UP
  3. Airspeed……..MAINTAIN V2
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3
Q

ENGINE FIRE

A
  1. Thrust(affectedengine)……..IDLE If ENG FIRE PUSH Switch Remains Illuminated:
  2. Thrust Lever (affected engine)………. CUTOFF
  3. Illuminated Engine Fire Switch……….PUSH
  4. Either Fire Bottle Switch………..PUSH
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4
Q

ENGINE FIRE DETECTOR FAILURE

A
  1. Engine Fire Procedures………….COMPLETE
  2. Remaining Illuminated Fire Bottle Switch………………..PUSH
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5
Q

DUAL ENGINE FLAMEOUT

A
  1. N2………….. VERIFY ABOVE 52%
  2. Ignitions…………………….ON If N2 Is Not Above 52% Or Neither Engine Relights:
  3. Battery…………. EMER
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6
Q

ENGINE FAILURE IN LANDING CONFIGURATION

A
  1. Thrust (operating engine) ………..AS REQUIRED
  2. Airspeed……….VREF
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7
Q

INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKEOFF (BELOW V1 - TAKEOFF ABORTED)

A
  1. Brakes……..APPLY
  2. Thrust……….IDLE
  3. Thrust Reversers………. BOTH DEPLOY
  4. Reverser Lights…………..VERIFY
  5. Reverse Thrust…………..AS REQUIRED
  6. SpeedBrakes……EXTEND
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8
Q

INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKEOFF (ABOVE V1 - TAKEOFF CONTINUED)

A
  1. Emergency Stow Push-Switch (affected engine)………………PUSH
  2. Nose Up Pitch Attitude at Rotation (VR) …………. 13 - 15° DESIRED
  3. Landing Gear (when positive climb established)…………………..UP
  4. Airspeed……………. V2 (MIN)
    If Reverser Will Not Stow And Lock:
  5. Thrust Lever (affected engine)……… CUTOFF
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9
Q

INADVERTENT THRUST REVERSER DEPLOYMENT IN FLIGHT (UNLOCK/DEPLOY ANNUNCIATOR ILLUMINATED)

A
  1. Emergency Stow Push-Switch (affected engine)………………PUSH
  2. Altitude……………………….. BELOW 30,000 FT
  3. Airspeed (until reverser stows/locks) ……………. BELOW 135 KIAS
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10
Q

INADVERTENT OVERSPEED

A
  1. Thrust…………………..IDLE
  2. SpeedBrakes………..EXTEND
  3. If airplane is in a nose-down attitude, initiate a wings-level pull-up without exceeding structural limits (3.2 g’s).
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11
Q

LOSS OF AIRSPEED INDICATION

A
  1. Autopilot……………DISCONNECT
  2. Airspeed…………….SLOW TO AND MAINTAIN 0.2 AOA
  3. Thrust……………….AS REQUIRED
  4. SpeedBrakes…….AS REQUIRED (SLOW TO 0.25 AOA WITH SPEED BRAKES EXTENDED)
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12
Q

ELECTRICAL FIRE OR SMOKE

A
  1. Oxygen Masks………….DON
  2. Smoke Goggles………..DON
  3. Mic Selectors…………..OXY MASK
  4. SPKR Switches ……….. ON OR DON HEADSET
  5. INTPH Switch……………ON
  6. Smoke Removal Procedures…………….. IF NECESSARY
    If Known Source:
  7. FaultedCircuits………….ISOLATE
    If Unknown Source:
  8. Battery…………………EMER
  9. Master Generator Switches…………………..EMER
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13
Q

ENVIRONMENTAL SYSTEM SMOKE OR ODOR

A
  1. Oxygen Masks………..DON
  2. Smoke Goggles……….DON
  3. Mic Selectors……..OXY MASK
  4. SPKR Switches ……… ON OR DON HEADSET
  5. INTPH Switch…………. ON
  6. Cabin Pressure Source……. ISOLATE SOURCE BY SELECTING L ENG OR R ENG
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14
Q

SMOKE REMOVAL

A
  1. Oxygen Masks………..DON
  2. Smoke Goggles……….DON
  3. Mic Selectors………….OXY MASK
  4. SPKR Switches ………. ON OR DON HEADSET
  5. INTPH Switch………… ON
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15
Q

CABIN DECOMPRESSION

A
  1. Oxygen Masks…………DON
  2. Mic Selectors…………..OXY MASK
  3. SPKR Switches ………..ON OR DON HEADSET
  4. INTPH Switch…………..ON
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16
Q

EMERGENCY DESCENT

A
  1. Thrust………….IDLE
  2. SpeedBrakes………..EXTEND
  3. Autopilot………………..OFF
  4. Initiate Moderate Bank……………….45° MAX
17
Q

OVERPRESSURIZATION

A
  1. Cabin Pressure Source……………………OFF
  2. Oxygen Masks……..DON
  3. Mic Selectors……….OXY MASK
  4. SPKR Switches …….. ON OR DON HEADSET
  5. INTPH Switch…………ON
18
Q

LOSS OF BOTH GENERATORS

A
  1. GEN FLD and START/GEN Circuit
    Breakers (AFT MAIN PANEL) ……. CHECK
  2. Generator Reset (L and R) ………….RESET/NORM
19
Q

PITCH TRIM RUNAWAY OR FAILURE

A
  1. TRIM INT/AP Disengage Switch……PUSH AND HOLD
20
Q

ROLL TRIM RUNAWAY OR FAILURE

A
  1. TRIM INT/AP Disengage Switch……….PUSH AND HOLD
21
Q

RUDDER TRIM RUNAWAY OR FAILURE

A
  1. TRIM INT/AP Disengage Switch………..PUSH AND HOLD
22
Q

POWER BRAKE FAILURE

A
  1. Break Safety Wire and Remove Guard Clip on Emergency Brake Handle.
  2. Emergency Brakes…….. APPLY GRADUALLY
23
Q

AUTOPILOT TRIM FAIL

A
  1. Trim Indicators ….. CHECK FOR PROPER POSITION FOR FLIGHT CONDITION
  2. TRIM INT/AP Disengage Switch…………..PUSH
24
Q

AUTOPILOT OVERSPEED RECOVERY

A
  1. Thrust…………IDLE
25
Q

FLIGHT DIRECTOR MALFUNCTIONS

A
  1. TRIM INT/AP Disengage Switch……..PUSH