Memory Items Flashcards
CABIN ALTITUDE
or
Rapid Depressurization
1 Don the oxygen masks.
2 Establish crew communications.
3 If occupants in main cargo compartment:
MAIN CARGO ALERT switch . . . . . . . . . . .Push
4 Check the cabin altitude and rate.
5 If the cabin altitude is uncontrollable:
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
- - - - - - - - - - - - - - - - - - - - - - -
Aborted Engine Start
1 FUEL CONTROL switch (affected side) . . . CUTOFF
- - - - - - - - - - - - - - - - - - - - - - -
Dual Engine Failure
1 ENG START selectors (both). . . . . . . . . . . . . FLT
2 Thrust levers (both) . . . . . . . . . . . . . . . . . . Idle
3 FUEL CONTROL
switches (both) . . . . . . . . . . . CUTOFF, then RUN
4 If engine appears stalled or EGT approaches the
Standby Engine Indicator placard limit:
FUEL CONTROL
switch (affected engine)…Confirm . . . CUTOFF,
then RUN
If engine appears stalled again or EGT
approaches the Standby Engine Indicator
placard limit, repeat as needed.
- - - - - - - - - - - - - - - - - - - - - - -
Engine Limit or Surge or Stall
1 A/T ARM switch . . . . . . . . . . . . . . . . . . . . . OFF
2 Thrust lever
(affected side) . . . Confirm . . . . . . . .Retard until
engine indications
stay within limits or
the thrust lever is at idle
- - - - - - - - - - - - - - - - - - - - - - -
ENGINE FIRE
or
Engine Severe Damage or
Separation
1 A/T ARM switch . . . . . . . . . . . . . . . . . . . . . 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 engine fire warning light is illuminated:
Engine fire switch
(affected side) . . . . . . . . . . Rotate to the stop
and hold for 1 second
- - - - - - - - - - - - - - - - - - - - - - -
Airspeed Unreliable
1 Autopilot disengage switch . . . . . . . . . . . . .Push
2 A/T ARM switch . . . . . . . . . . . . . . . . . . . . . OFF
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
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Approach to Stall or Stall Recovery
Initiate the recovery:
* Hold the control column
firmly.
* Disconnect 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.
* Monitor altitude and airspeed.
* Verify all required actions have
been done and call out any
omissions.
* Call out any trend toward terrain
contact.
* Do not change gear or flap
configuration, except
* During liftoff, if flaps are up,
call for flaps 1.
- 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
Rejected Takeoff
Captain
Without delay:
Simultaneously close the thrust levers,
disengage the autothrottles, and apply
maximum manual wheel brakes or
verify operation of RTO autobrakes.
If RTO autobrakes is selected, monitor
system performance and apply manual
wheel brakes if the AUTO BRAKES
light illuminates or deceleration is not
adequate.
Raise SPEEDBRAKE lever.
Apply reverse thrust up to the
maximum amount consistent with
conditions.
Continue maximum braking until
certain the airplane can stop on the
runway.
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.
FO
Verify actions as follows:
Thrust levers closed.
Autothrottle disengaged.
Maximum brakes applied.
Verify speedbrake lever UP and call
“SPEEDBRAKES UP.” If speedbrake
lever not UP call “SPEEDBRAKES
NOT UP.”
Reverse thrust applied. When both REV
indications are green, call
“REVERSERS NORMAL.”
If there is no REV indication(s) or the
indication(s) stays amber, call “NO
REVERSER LEFT ENGINE”, or “NO
REVERSER RIGHT ENGINE”, or
“NO REVERSERS”.
Call out any omitted action items.
When stopping is assured:
Call out 60 knots.
Communicate the reject decision to the
control tower as soon as practical
Upset Recovery
Disconnect autopilot
Disconnect autothrottle
Recover
Thrust as required
WINDSHARE PWS
- Prior to V1, reject takeoff.
- After V1, perform the Windshear Escape Maneuver
Windshear Escape Maneuver With Flight Director Guidance - Manual flight
MANUAL FLIGHT
* Disconnect autopilot.
* Push either go–around switch.
* Aggressively apply maximum* thrust.
* Disconnect autothrottle.
* Simultaneously roll wings level and
rotate toward an initial pitch attitude
of 15°.
* Retract speedbrakes.
* Follow flight director GA guidance (if
available)**
Do not change gear or flap
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.
Windshear Escape Maneuver With Flight Director Guidance - Automatic flight
AUTOMATIC FLIGHT
* Push either go-around switch.
* Verify TO/GA mode annunciation.
* Verify GA thrust.
* Retract speedbrakes.
* Monitor system performance**.
Do not change gear or flap
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.
