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B737-8 MAX > Memory items > Flashcards

Memory items Flashcards

1
Q

Aborted Engine Start

A

Engine Start Lever (affected engine)……………………..CUTOFF

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2
Q

Engine Limit or Surge or Stall

A

Autothrottle (if engaged)……………………………………Disengage

Thrust Lever (affected engine)…….……..Confirm………Retard until engine indications stay within limits or the thrust lever is closed.

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3
Q

Loss of Thrust on Both Engines

A

ENGINE START switches (both)……………………..……..FLT

Engine start levers (both)……………………………..…….CUTOFF

WHEN EGT decreases

Engine start levers (both)……………….IDLE Detent

IF EGT reaches redline or there is no increase in EGT within 30 seconds

Engine Start Lever (affected engine)……CONFIRM……CUTOFF then IDLE detent

IF EGT again reaches a redline or there is no increase in EGT within 30 seconds, repeat as needed.

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4
Q

APU Fire

A

APU fire switch………….confirm………..Pull, rotate to the stop and hold 1 second

APU switch…………………………………OFF

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5
Q

Engine Overheat

A

Autothrottle (if engaged)………………………………………..Disengage

Thrust lever (affected engine)………..confirm………….…….Close

IF ENG OVERHEAT light stays illuminated:

GO TO ENGINE FIRE OR ENGINE SEVER DAMAGE CHECKLIST

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6
Q

Smoke or Fire from Lithium Battery

A

If necessary transfer control to the flight crew member seated on opposite side of fire.

PA…………..”BACKUP TO THE FLIGHTDECK, BACKUP TO THE FLIGHTDECK”

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7
Q

Smoke, Fire or Fumes

A

Oxygen Masks and smoke goggles…………..ON, 100%

Crew and cabin communications…………….Establish

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8
Q

Runaway Stabilizer

A

Control Column……………………..Hold Firmly

Autopilot (if engaged)……………….Disengage

  1. Autothrottle (if engaged)………..……Disengage
  2. Control column and thrust levers……..Control airplane pitch attitude and airspeed
  3. Main electric stab trim…………………….Reduce control column control forces
  4. IF the runaway stops after the autopilot is disengaged:
    Do not re-engage the autopilot or autothrottle
               ■■■■
  5. IF the runaway continues after the autopilot is disengaged:

STAB TRIM CUTOUT switches (both)…………….CUTOUT

IF the runaway still continues:

Stab Trim wheel………………..Grasp and hold

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9
Q

Airspeed Unreliable

A

Autopilot (if engaged)………………………..Disengage

Autothrottle (if engaged)…………………….Disengage

F/D Switches (both)…………………………Off

Set the following gear up pitch attitudes and thrust:

Flaps extended…………10* and 80% N1

Flaps UP………………….4* and 75% N1

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10
Q

Landing Configuration (in flight, steady warning horn sounds)

A

Assure correct airplane configuration

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11
Q

Takeoff Configuration (Takeoff Config light)

A

Assure correct airplane takeoff configuration

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12
Q

Warning Horn (intermittent) OR Warning Light - Cabin altitude or takeoff config

A
  1. IF the intermittent warning horn sounds or a CABIN ALTITUDE light illuminates in FLIGHT, at an airplane altitude above 10,000’ MSL:

Don oxygen masks and set regulators to 100%
Establish Crew communications
GO to Cabin Altitude Warning or Rapid Depressurization checklist

  1. IF the intermittent warning horn sounds or a TAKEOFF CONFIG light illimunates on the GROUND when advancing the thrust levers for takeoff thrust:
    - Assure correct airplane takeoff configuration
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13
Q

Oceanic Diversion (All Engine)

A
  1. Initiate Applicable drills and time critical checklists
  2. Declare Emergency and request clearance
  3. Choose one: - If clearance obtained -> proceed as per clearance
    - if clearance unavailable - turn at least 30 degrees right or left and offset 5nm. When established on offset +/- 500’
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14
Q

Oceanic Diversion (engine out)

A
  1. Initiate Applicable drills and time critical checklists
  2. Declare Emergency and request clearance
  3. Choose one: - If clearance obtained -> proceed as per clearance
    - if clearance unavailable - turn at least 30 degrees right or left and offset 5nm. Minimize descent until established on offset. When established on offset descend below FL290 and maintain +/- 500’
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15
Q

Emergency Descent

A
  1. Call “Emergency Descent”
  2. PA (if conditions permit) “Attention Flight attendants secure the cabin, passengers take your seats”
  3. FASTEN BELTS On
  4. Without delay descend to lowest safe or 10,000’ whichever is higher.
    5 Landing Lights ON
    6 ATC advise, obtain alt setting
    7 TRANSPONDER 7700
    8 If Cabin altitude cannot be controlled: PA
    » “ATTENTION PUT ON YOUR OXYGEN MASKS IMMEDIATELY”
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16
Q

CABIN ALTITUDE WARNING or Rapid Depressurization

A
  1. O2 Masks Don, 100%
    2 Establish Crew communications
    3 FASTEN BELTS On
  2. PA (if conditions permit) ATTENTION FLIGHT ATTENDANTS, SECURE THE CABIN,
    PASSENGERS TAKE YOUR SEAT”
    5 Presurization mode Selector MAN
    6 Outflow VALVE switch Hold in Close until the outflow indication shows fully closed
    7 If cabin altitude is uncontrollable:
    PASS OXYGEN switch ON
    » go to the Emergency Descent checklist on
    Page 0.1
17
Q

Nose High Recovery

A

Recognize and confirm the situation

Disengage autopilot and autothrottle
• Apply as much as full nose-down elevator
• * Apply appropriate nose down stabilizer trim
• Reduce thrust
• * Roll (adjust bank angle) to obtain a nose down
pitch rate
• Complete the recovery:
- When approaching the horizon, roll to wings
level
- Check airspeed and adjust thrust
-Establish Pitch attitude

PM - Call out attitude, airspeed and
altitude throughout the
recovery
• Verify all required actions
have been completed and call
out any omissions.
18
Q

Nose Low

A

Recognize and confirm the situation

• Disengage autopilot and autothrottle
• Recover from stall, if required
• * Roll in shortest direction to wings level (unload
and roll if bank angle is more than 90 degrees)
• Recover to level flight:
- Apply nose up elevator
- *Apply nose up trim, if required
- Adjust thrust and drag as required.
PM - • Call out attitude, airspeed
and altitude throughout the
recovery
• Verify all required actions
have been completed and call
out any omissions.
19
Q

GPWS

A

Call “FIREWALL”.
Disengage autopilot.
Disengage autothrottle.
Aggressively apply maximum* thrust.
Simultaneously roll wings level and rotate to an
initial pitch attitude of 20°.
Retract speedbrakes.
If terrain remains a threat, continue rotation up
to the pitch limit indicator (if available) or stick
shaker or initial buffet.

Do not change gear or flap configuration until
terrain separation is assured.
Monitor radio altimeter for sustained or
increasing terrain separation.
When clear of terrain, slowly decrease pitch
attitude and accelerate.

PM - Assure maximum* thrust.
Verify all required actions have been completed
and call out any omissions.
Monitor vertical speed and altitude (radio
altitude for terrain clearance and barometric
altitude for a minimum safe altitude.)
Call out any trend toward terrain contact.

20
Q

Approach to Stall

A 
• Simultaneously call “STALL” and :
• Initiate the recovery:
• Hold the control column firmly.
• Disengage autopilot and autothrottle.
• Smoothly apply nose down elevator to
reduce the angle of attack until buffet
or stick shaker stops. Nose down
stabilizer trim may be needed.*
• Continue the recovery:
• Roll in the shortest direction to wings
level if needed.**
• Advance thrust levers as needed.
• Retract the speedbrakes.
• Do not change gear or flap
configuration, except
• During liftoff, if flaps are up, call for
flaps 1.

WHEN CONTROL OF FLIGHT PATH IS REGAINED AND GROUND CONTACT IS NOT A
FACTOR:

• Complete the recovery:
• Check airspeed and adjust thrust as
needed.
• Establish pitch attitude.
• Return to the desired flight path.
• Re-engage the autopilot and autothrottle if
desired.
PM - • Monitor altitude and airspeed.
• Verify all required actions have
been done and call out any
omissions.
• Call out any trend toward terrain
contact.
21
Q

Windshear

A

MANUAL FLIGHT
• Call “WINDSHEAR TOGA”
• Disengage autopilot.
• Push either TO/GA switch.
• Aggressively apply maximum thrust*
• Disengage autothrottle.
• Simultaneously roll wings level and rotate
toward an initial pitch attitude of 15 °.
• Retract speedbrakes.
• Follow flight director TO/GA guidance (if
available)**

AUTOMATIC FLIGHT
• Call “WINDSHEAR TOGA”
• Push either TO/GA switch***
• Verify TO/GA mode annunciation.
• Verify thrust advances to GA power
• Retract speedbrakes.
• Monitor system performance****

MANUAL OR AUTOMATIC FLIGHT
• Do not change flap or gear configuration until
windshear is no longer a factor.
• Monitor vertical speed and altitude.
• Do not attempt to regain lost airspeed until
windshear is no longer a factor.

PM - • Assure maximum* thrust. (GA thrust for auto flight)
• Verify all required actions have
been completed and call out any
omissions.
Monitor vertical speed and
altitude.
• Call out any trend toward terrain
contact, descending flight path, or
significant airspeed changes.
22
Q

Low energy Go around

A

The low energy landing regime is defined as:
• Aircraft is in descent.
• Thrust is at or near idle.
• Airspeed is decreasing.
• Aircraft height is 50 ft or less above the runway elevation.

A speed of VREF should be achieved prior to commencing climb.
In the event of a low energy go-around continue with normal go-around procedures.

23
Q

TCAS RA

A

Disengage AP and AT.
Smoothly adjust pitch and thrust to satisfy RA command

RA in climb configuration:
Disengage AP and AT.
advance thrust levers forward to ensure max thrust and call flaps 15. Smoothly adjust pitch to satisfy RA command.

Verify positive rate (PM Call “positive rate”) and call “Gear UP”

PM CALLS to ATC: “AC____, TCAS RA”
“AC___ clear of conflight, returning to ____ft”

24
Q

Ground Incident

A

If an immediate evacuation is not required I will
PA,
“REMAIN SEATED, REMAIN SEATED”.
If urgent contact with the In-Charge is required, I
will PA,
“IN-CHARGE FLIGHT ATTENDANT CALL (OR
REPORT TO) THE FLIGHT DECK”.
If an evacuation is required I will call,
“CHECKLIST, PASSENGER EVACUATION”.

25
Q

Engine Inoperative Cruise/Driftdown

A

PF - “DISENGAGE AUTOTHROTTLE”, “SET MAX
CONTINUOUS THRUST”.

PM - • Disengage autothrottle
• Select CON thrust in FMC
• Manually set Maximum Continuous
Thrust (MCT)

PF - Confirm that the thrust mode changes to CON
and the thrust is set to MCT.
Request ENG OUT to be selected on the ECON
CRZ page.

PM - Select failed engine and 
Set the Maximum Engine Out Altitude in
the MCP Altitude Window.
• Set the Engine Out Target Airspeed in
the MCP IAS Window.

PF - At engine out target speed, LVL CHG

PM - All lights on, ATC advise

PF - Call “checklist engine failure”

26
Q

Overrun Warning (ORW)

A

In air - Go around

On ground:

PF : Without delay:
Simultaneously close the thrust levers and
apply maximum manual wheel brakes.
Verify speed brakes are deployed or raise
the SPEED BRAKE lever.
Apply reverse thrust up to the maximum
amount consistent with conditions.
Continue maximum braking until certain the
airplane can stop on the runway.

PM: Verify actions as follows:
Thrust levers closed.
Maximum brakes applied.
Verify SPEED BRAKE lever UP and call
“SPEEDBRAKES UP.” If SPEED BRAKE
lever is not UP, call “NO SPEEDBRAKES”.
Reverse thrust applied. When both REV
indications are green, call "REVERSE
GREEN".
If there is no REV indication(s) or the
indication(s) stays amber, call
"NO REVERSE NUMBER 1” (or 2), as
appropriate".
Call out omitted action items.

When stopping is assured:
Start movement of the reverse thrust levers
to reach the reverse idle detent before taxi
speed.
After the engines are at reverse idle, move
the reverse thrust levers to full down.

B737-8 MAX (2 decks)

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