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B787 MEMORY ITEMS
[] CABIN ALTITUDE
Condition: Cabin Altitude is excessive.
1 Don the oxygen masks.
2 Establish crew communications.
3 LEFT PILOT becomes PF.
4 Check the cabin altitude and rate.
5 If the cabin altitude is uncontrollable:
PASS OXYGEN switch............................................Push to ON and
Hold for 1 second
Without delay, descend to the lowest safe
altitude or 10,000 feet, whichever is higher.
To Descend:
Move the thrust levers to idle
Extend the speedbrakes
If structural integrity is in doubt, limit
airspeed and avoid high maneuvering loads
Descend at Vmo/Mmo
Verify the lowest safe altitude
ATC..............ADVISE
Obtain the area altimeter setting (QNH), if
required
Verify memory items completed. Call
any ommited items
Call out 2000feet and 1000feet above level
off altitude
If Escape Route:
Advise track/altitudes
Monitor flight path
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Aborted Engine Start L,R
Condition: On the ground, an aborted engine start is needed.
1 FUEL CONTROL switch
(affected side)...................................................................CUTOFF
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[] ENG AUTOSTART L,R
Condition: Autostart did not start the engine.
1 FUEL CONTROL switch
(affected side)..............................Confirm...........................CUTOFF
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Dual Eng Fail/Stall
Condition: Engine speed for both engines is below idle.
1 FUEL CONTROL switches
(both).................................................................CUTOFF, then RUN
2 RAM AIR TURBINE switch....................................................Push and
Hold for 1 second
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[] ENGINE LIMIT EXCEED L, R
Condition: An engine limit exceedance occurs.
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
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[] ENGINE SURGE L, R
Condition: An engine surge or stall that requires crew action is detected.
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
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Eng Svr Damage/Sep L, R
Condition: One or more of these occur:
• Airframe vibrations with abnormal engine
indications
• Engine separation
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
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[] STABILIZER
Condition: One of these occurs:
• Stabilizer movement without a signal to trim
• The stabilizer is failed
1 STAB cutout switches (both)........…………………...…………………….…CUTOUT
2 Do not exceed the current airspeed.
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[] FIRE ENG L, R
Condition: Fire is detected in the engine.
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
5 If the FIRE ENG message stays shown:
Engine fire switch
(affected side)..................................................Rotate to the stop
and hold for 1 second
If after 30 seconds, the FIRE ENG message
stays shown:
Engine fire switch
(affected side)....................................................Rotate to the
other stop and
hold for 1 second
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[] AIRSPEED UNRELIABLE
Condition: The airspeed or Mach indications disagree with AOA calculated
airspeed.
Objective: To identify a reliable airspeed indication.
1 Autopilot disengage switch……………………………………………………………….Push
2 A/T ARM switches (both)……………………………………………………………………OFF
3 F/D switches (both)…………………………………………………………………………….OFF
4 Set the following gear up pitch attitude and thrust:
Flaps extended…………………………………………………10° and 85% N1
Flaps up……………………………………………………………..4° and 70% N1
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Differences Training Boeing 787
