Memory Items Flashcards
(15 cards)
Aborted Engine Start
Condition: On the ground an aborted engine start is
needed.
Objective: To shut down the engine and motor it.
1 Engine start lever (affected engine) . . . . CUTOFF
Airspeed Unreliable
OR
Airspeed Unreliable
(Stick Shaker Deactivation by
Pulling Circuit Breaker)
Condition: Airspeed or Mach indications are suspected
to be unreliable. (Items which might indicate
unreliable airspeed are listed in the
Additional Information section.)
Objective:
To identify a reliable airspeed indication, if
possible, or to use the Flight With Unreliable
Airspeed table in the Performance Inflight
chapter for the remainder of the flight.
1 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
2 Autothrottle (if engaged). . . . . . . . . . .Disengage
3 F/D switches (both) . . . . . . . . . . . . . . . . . . OFF
4 Set the following gear up pitch attitude and thrust:
Flaps extended . . . . . . . . . . 10° and 80% N1
Flaps up . . . . . . . . . . . . . . . . 4° and 75% N1
APU Fire
Condition: Fire is detected in the APU.
1 APU fire switch. . . Confirm . . . .Pull, rotate to the
stop, and hold
for 1 second
2 APU switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
Cabin Altitude Warning or Rapid Depressurization
Condition: One or more of these occur:
*A cabin altitude exceedance
*In flight, the intermittent cabin
altitude/configuration warning horn
sounds or a CABIN ALTITUDE light (if
installed and operative) illuminates.
1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications.
3 Pressurization mode selector . . . . . . . . . . . .MAN
4 Outflow VALVE switch . . . . . . . . . . Hold in CLOSE
until the outflow VALVE
indication shows fully closed
5 If cabin altitude is uncontrollable:
Passenger signs . . . . . . . . . . . . . . . . . . . . ON
PASS OXYGEN switch . . . . . . . . . . . . . . . . ON
►►Go to the Emergency Descent checklist
on page 0.1
Cargo Fire (Main)
Condition: Fire is detected in the main deck cargo
compartment.
Objective: To suppress the fire. To land at the nearest
suitable airport.
1 Don oxygen masks and set regulators to 100%, as
needed.
2 Don smoke goggles, as needed.
3 Close the flight deck door. This step prevents
smoke or fumes contamination from other
compartments.
4 Establish crew and cabin communications.
Emergency Descent
Condition: One or more of these occur:
*Cabin altitude cannot be controlled
*A rapid descent is needed.
1 Announce the emergency descent. The pilot flying
will advise the cabin crew, on the PA system, of
impending rapid descent. The pilot monitoring will
advise ATC and obtain the area altimeter setting.
2 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
3 Without delay, descend to the lowest safe
altitude or 10,000 feet, whichever is higher.
4 ENGINE START switches (both) . . . . . . . . . CONT
5 Thrust levers (both) . . . . . . . . . Reduce thrust to
minimum or as
needed for anti-ice
6 Speedbrake . . . . . . . . . . . . . . . .FLIGHT DETENT
If structural integrity is in doubt, limit speed as
much as possible and avoid high maneuvering
loads.
7 Set target speed to Mmo/Vmo.
- - - - - - - - - - - - - - - -
ENGINE FIRE
Condition: One or more of these occur:
*Engine fire warning
*Airframe vibrations with abnormal engine
indications
*Engine separation.
1 Autothrottle (if engaged). . . . . . . . . . .Disengage
2 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . . Close
3 Engine start lever
(affected engine) . . . . . . Confirm . . . . . CUTOFF
4 Engine fire switch
(affected engine) . . . . . . Confirm . . . . . . . . Pull
To manually unlock the engine fire switch, press
the override and pull.
5 If the engine fire switch or ENG OVERHEAT light is
illuminated:
Engine fire switch
(affected engine) . . . . . . . . Rotate to the stop
and hold for 1 second
- - - - - - - - - - - - - - - - - - - - - - -
Engine Limit or Surge or Stall
Condition: One or more of these occur:
*Engine indications are abnormal
*Engine indications are rapidly approaching
or exceeding limits
*Abnormal engine noises are heard,
possibly with airframe vibration
*There is no response to thrust lever
movement or the response is abnormal
*Flames in the engine inlet or exhaust are
reported.
Objective: To attempt to recover normal engine opera-
tion or shut down the engine if recovery is
not possible.
1 Autothrottle (if engaged). . . . . . . . . . .Disengage
2 Thrust lever
(affected engine) . . . . Confirm. . . . .Retard until
engine indications
stay within limits or
the thrust lever is close
Engine Overheat
1 Autothrottle (if engaged). . . . . . . . . . .Disengage
2 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . . Close
3 If the ENG OVERHEAT light stays illuminated:
►►Go to the ENGINE FIRE or Engine
Severe Damage or Separation checklist
on page 8.8
■ ■ ■ ■
Landing Configuration
Condition: In flight, the steady warning horn sounds.
1 Assure correct airplane landing configuration.
Takeoff Configuration
Condition: On the ground, the intermittent cabin
altitude/configuration warning horn sounds
or a TAKEOFF CONFIG light (if installed and
operative) illuminates when advancing the
thrust levers to takeoff thrust.
1 Assure correct airplane takeoff configuration.
Loss Of Thrust On Both Engines
Condition: Both of these occur:
*Both engines have a loss of thrust
*Both ENG FAIL alerts show.
Objective: To restart at least one engine.
1 ENGINE START switches (both) . . . . . . . . . . FLT
2 Engine start levers (both) . . . . . . . . . . . CUTOFF
3 When EGT decreases:
Engine start levers (both) . . . . . . IDLE detent
4 If EGT reaches a 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.
Runaway Stabilizer
Condition: Uncommanded stabilizer trim movement
occurs continuously or in a manner not
appropriate for flight conditions.
1 Control column. . . . . . . . . . . . . . . . . Hold firmly
2 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
3 Autothrottle (if engaged). . . . . . . . . . .Disengage
4 Control column and
thrust levers . . . . . . . . . . . Control airplane pitch
attitude and airspeed
5 Main Electric
Stabilizer trim . . . . . . . . . . . . . . .Reduce control
column forces
6 If the runaway stops after the autopilot is
disengaged:
Do not re-engage the autopilot or autothrottle.
■ ■ ■ ■
7 If the runaway continues after the autopilot is
disengaged:
STAB TRIM cutout
switches (both) . . . . . . . . . . . . . . . . CUTOUT
If the runaway continues:
Stabilizer
trim wheel . . . . . . . . . . Grasp and hold
WARNING HORN (INTERMITTENT)
Condition: One of these occurs:
*In flight, at an airplane flight altitude
above 10,000 feet MSL, the intermittent
warning horn sounds or a CABIN
ALTITUDE light (if installed and operative)
illuminates
*On the ground, the intermittent warning
horn sounds or a TAKEOFF CONFIG light
(if installed and operative) illuminates
when advancing the thrust levers to
takeoff thrust.
1 If the intermittent warning horn sounds or a CABIN
ALTITUDE light (if installed and operative)
illuminates in flight at an airplane flight altitude
above 10,000 feet MSL:
Don the oxygen masks and set the regulators to
100%.
Establish crew communications.
►►Go to the CABIN ALTITUDE WARNING
or Rapid Depressurization checklist on
page 2.1
2 If the intermittent warning horn sounds or a
TAKEOFF CONFIG light (if installed and operative)
illuminates on the ground when advancing the
thrust levers to takeoff thrust:
Assure correct airplane takeoff configuration.
