Memory Items Flashcards

(33 cards)

1
Q

What is the procedure for descending if cabin altitude is uncontrollable?

A

Thrust levers to idle, extend speedbrakes, descend at Vmo/Mmo.

These steps help to safely reduce altitude.

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2
Q

What should be done with the RAM AIR TURBINE switch during a dual engine failure?

A

Push and hold 1 for sec.

Activating the RAM AIR TURBINE provides emergency power.

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3
Q

In case of engine limit exceedance, what should be done with the thrust lever (affected side)?

A

Retard until ENG LIMIT EXCEED message blanks or thrust lever is at idle.

This action helps to mitigate engine stress.

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4
Q

What is the procedure for addressing engine surge?

A

A/T ARM switch (affected side) OFF, Thrust lever (affected side) Retard until ENG SURGE message blanks.

Managing engine surge is critical for engine safety.

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5
Q

What should be done with the A/T ARM switch during an engine fire in flight?

A

A/T ARM switch (affected side) OFF.

This step helps to control engine power during an emergency.

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6
Q

What is the final action if the FIRE ENG message stays shown after pulling the engine fire switch?

A

Confirm pulling the engine fire switch (affected side).

This ensures that the engine is shut down in an emergency.

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7
Q

What should be done with the STAB cutout switch (both)?

A

CUTOUT.

This action is necessary to manage the stabilizer control in critical conditions.

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8
Q

True or False: The thrust lever (affected side) should be set to idle during an engine fire.

A

True

This is part of the standard emergency procedure.

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9
Q

What should be advised to the cabin in case of evacuation?

A

Advise the cabin to evacuate

Important for ensuring passenger safety during emergencies

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10
Q

What is the first action to take if an engine or APU fire is observed?

A

Related fire switch CUTOFF

Critical step in fire management procedures

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11
Q

What should be done with the OUTFLOW VALVE switches during evacuation?

A

Set both OUTFLOW VALVE MANUAL switches to MAN

Ensures proper cabin pressure management

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12
Q

What should be established when below FL 290 in oceanic airspace?

A

Maintain 150m (500ft) vertical offset when able

Ensures safe separation from other aircraft

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13
Q

What is the recommended action for transponder settings in emergencies?

A

Set transponder to 7700

Indicates emergency situation to ATC

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14
Q

Fill in the blank: When in oceanic airspace, you must establish a _______ track offset by 5NM.

A

parallel

Important for maintaining safe distance from other aircraft

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15
Q

What should be done if ATC clearance is not received?

A

Proceed as required until clearance is received

Ensures compliance with safety regulations

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16
Q

What should be done with the MCP altitude in case of engine failure?

A

Set at or below CRZ ALT shown on CDU

Ensures altitude compliance during engine failure

17
Q

What action is required for electronic checklists during emergencies?

A

Use electronic Checklist(s)

Ensures systematic approach to emergency procedures

18
Q

True or False: In oceanic airspace, you should leave track by at least 30° to the left or right.

A

True

Helps maintain safe separation from other aircraft

19
Q

What is the procedure for descent below FL290?

A

Establish & maintain 500ft vertical offset when able

Ensures safety during altitude adjustments

20
Q

What should be done with exterior lights during emergencies?

A

Turn on exterior lights

Enhances visibility for other aircraft

21
Q

What key action is required when executing an emergency broadcast?

A

Transmit via CPDLC, HF, or VHF

Ensures communication with air traffic control

22
Q

Aborted Engine Start L,R

A

Fuel control switch ( affected side)………………….cutoff

23
Q

Airspeed Unreliable

A
  1. Autopilot disconnect switch ………………push
  2. A/T Arm switch both…………………………..off
    3.F/D switch both……………………………………off
  3. Set the following gear-up pitch attitude and thrust
    Flaps extended…………..10 degree. 85%N1
    Flaps up”……………………..4 degree. 70% N1
24
Q

CABIN ALTITUDE [QRH 2.1]

A
  1. Don the oxygen masks.
  2. Establish crew communications.
  3. Check cabin altitude and rate.
  4. IF cabin altitude uncontrollable:
    PASS OXYGEN switch…………………………………………………………..Push to ON and hold for 1 sec
    Without delay, descend to lowest safe altitude or 10,000’ (whichever is higher).
    To descend:
    x Thrust levers to idle.
    x Extend speedbrakes.
    x If structural integrity in doubt, limit airspeed and avoid high maneuvering loads.
    x Descend at Vmo/Mmo.
25
Dual Eng Fail/Stall [QRH 7.2]
1. FUEL CONTROL switches (both) .......................................................................... CUTOFF, then RUN 2. RAM AIR TURBINE switch .............................................................................Push and hold 1 for sec
26
ENG AUTOSTART L, R [QRH 7.3]
1. FUEL CONTROL switch (affected side) ......................................................... Confirm…..……..…CUTOFF
27
ENG LIMIT EXCEED L, R [QRH 7.4]
1. A/T ARM switch (affected side) .................................................................. Confirm…………...………OFF 2. Thrust lever (affected side) ....................................................................... Confirm….……Retard until ENG LIMIT EXCEED message blanks, or the thrust lever is at idle
28
ENG SURGE L, R [QRH 7.7]
1. A/T ARM switch (affected side) .................................................................. Confirm…….………..……OFF 2. Thrust lever (affected side) ....................................................................... Confirm….……Retard until the ENG SURGE, Message blanks or the thrust lever is at idle
29
Eng Svr Damage/Sep L, R [QRH 7.10]
1. A/T ARM switch (affected side) ................................................................... Confirm……..….….……OFF 2. Thrust lever (affected side) .........................................................................Confirm……..…….…….Idle 3. FUEL CONTROL switch (affected side) .......................................................... Confirm…..…….…CUTOFF 4. Engine fire switch (affected side)..................................................................Confirm…….…..….……Pull
30
FIRE ENG L, R [QRH 8.2]
1. In Flight: 2. A/T ARM switch (affected side) .....................................................................Confirm……..………...OFF 3. Thrust lever (affected side) ..........................................................................Confirm…..….…………Idle 4. FUEL CONTROL switch (affected side) ............................................................Confirm…..……..CUTOFF 5. Engine fire switch (affected side)................................................................... Confirm…….….……...Pull 6. If the FIRE ENG message stays shown: Engine fire switch (affected side).......................................... Rotate to the stop and hold for 1 sec
31
STABILIZER [QRH 9.1]
1. STAB cutout switch (both)................................................................................................. CUTOUT 2. Do not exceed current airspeed
32
Evacuation [QRH Back Cover.4]
1. PARKING BRAKE ................................................................................................Set……………….……C 2. OUTFLOW VALVE switches (both) ........................................................................MAN……………....F/O 3. OUTFLOW VALVE MANUAL switches (both) ..................................Move to OPEN until the outflow valve indications show at the12 o’clock position to depressurize the airplane…..F/O 4. FUEL CONTROL switches (both) ......................................................................CUTOFF……………..…..C 5. Advise the cabin to evacuate. ...................................................................................................... C 6. Advise ATC. ........................................................................................................................... F/O 7. Engine fire switches (both) ................................................................................. Pull…..…………...F/O 8. APU fire switch........................................................................................Override and pull……...F/O 9. If an engine or APU fire is observed or indicated: Related fire switch................................................Rotate to the stop and hold for 1 second..…F/O
33
Engine Failure in Oceanic Airspace
1. If Eng Svr Damage/Sep: Memory Items ........................................................................................................... Perform 2. VNAV CRZ page .................................................................................................................. Select 3. ENG OUT prompt................................................................................................................. Select 4. MCP altitude ........................................................................Set at or below CRZ ALT shown on CDU 5. EXEC key ............................................................................................................................. Push 6. MCP heading........................................................................... Leave track by at least 30º to the L/R establish a parallel track in the same direction offset by 5NM 7. Emergency broadcast ......................................................................Transmit via CPDLC, HF, or VHF 8. Transponder ........................................................................................................................ 7700 9. Exterior Lights .........................................................................................................................On 10. ATC .................................................................................................. Advise via CPDLC, HF, or VHF 11. Electronic Checklist(s)....................................................................................................... Perform