CRJ Memory Items Flashcards

1
Q

L (R) Rev Deployed

A

Affected Thrust Lever…………………..Confirm and IDLE

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2
Q

Engine Overspeed or Uncommanded Acceleration

A

Affected Thrust Lever……………………Confirm and IDLE

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3
Q

NO STRTR CUTOUT (in flight)

APU or Cross Bleed Start Scenario

A

Affected ENG STOP………………………STOP

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4
Q

NO STRTR CUTOUT

L (R) SRT VLV OPEN (In flight) Scenario

A

Affected ENG STOP………………………STOP

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5
Q

NO STRTR CUTOUT (On Ground)

APU or Cross Bleed Start

A

Affected ENG STOP………………………STOP

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6
Q

NO STRTR CUTOUT

L (R) SRT VLV OPEN (On Ground)

A

Affected ENG STOP………………………STOP

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7
Q

Loss of All AC Power (ADG Inop)

A

ADG Manual Deploy Handle…………………………….Pull

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8
Q

Aileron System Jammed

A
  • Autopilot……………………….Disengage
  • Aileron Controls (both)……………………Release Pressure
  • ROLL DISC……………………Confirm then PULL & TURN to lock
  • Airplane Control………………..Transfer to pilot with operative aileron
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9
Q

Elevator System Jammed

A
  • Autopilot………………Disengage
  • Elevator Controls (both)……..Release differential Pressure
  • PITCH DISC. handle….Confirm then PULL & TURN to lock
  • Airplane Control………………..Transfer to pilot with operative elevator
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10
Q

Rudder System Jammed

A

YAW DAMPER DISC…………….Select

Rudder Pedals……….Overpower

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11
Q

Stabilizer Trim Runaway

A
  • Control Wheel…..Assume manual control and override runaway
  • STAB TRIM DISC………. Select
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12
Q

Cabin Alt (RED)

A

Oxygen Masks……………Don, set to 100%

Crew Communication…………Establish

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13
Q

Excessive Asymmetry or Loss of Braking

During Landing

A

Wheel Brakes……………Release Momentarily
ANTI SKID…………………OFF
Wheel Brakes…………..Re-Apply as required

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14
Q

Configuration Warning

A

Takeoff……………………Discontinue Immediately

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15
Q

Rejected Takeoff

A

Simultaneously…..

  • Thrust Levers………..IDLE
  • Wheel Brakes……….Maximum until safe stop
  • Thrust Reverser(s) Operating Engine(s)………..Maximum consistent with directional control
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16
Q

Double Engine Failure

A

CONT IGNITION switch…………………….ON

17
Q

Unreliable Airspeed In Flight

A

Autopilot……………………Disconnect
Flight Directors…………..Deselect
Use ISI for pitch reference
Initial Takeoff climb or go-around is required
Pitch/N1…………………..10 degrees/TOGA from SL to 15000ft
…………………..5 degrees/CLB above 15000ft

18
Q

Engine Failure in Climb During ALTS CAP

A

Autopilot (if engaged)……………………………..Disengage
Pitch Attitude…………………….Adjust to maintain the required single engine operating speed

19
Q

Engine Failure in Climb During (V) ALTS CAP or (V) ALTV CAP

A

Autopilot (if engaged)……………………………..Disengage
Pitch Attitude…………………….Adjust to maintain the required single engine operating speed