Memory Items Flashcards
Automatic Unlock
Condition: The correct emergency access code is entered.
- FLT DECK DOOR lock selector………………. Rotate to DENY and hold for 1 second
Aborted Engine Start L, R
Condition: During a ground start, an abort engine start condition
occurs.
- FUEL CONTROL switch (affected side)………………. CUTOFF
Airspeed Unreliable
Condition: The airspeed or Mach displays are suspected to be unreliable. (Items which may indicate unreliable airspeed are listed in the Additional Information section.)
- A/P disengage switch…push
- A/T ARM switches (both)….off
- F/D switches (both)…..off
- Set the following gear up pitch attitude and thrust: Flaps extended (10deg/85% N1). Flaps up (4deg/ 70%N1)
[] CABIN ALTITUDE
Condition: A cabin altitude exceedance occurs.
1 Don the oxygen masks.
2 Establish crew communications.
3 Check the cabin altitude and rate.
4 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 14,000 feet, whichever is higher. If fuel is not critical, descend to 10,000ft.
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
[] ENG AUTOSTART L, R
Condition: During a ground start, any of the following conditions
occurs:
•Autostart did not start the engine
•Fuel control switch is in RUN at low engine RPM with the
autostart switch off
1 FUEL CONTROL switch (affected side)………………. CUTOFF
[] 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. . . . . . . Rotate to the stop and hold for 1 second
If after 30 seconds, the FIRE ENG message stays shown:
Engine fire switch. . . . . Rotate to the other stop and hold for 1 sec
[] 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.
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
Eng Lim/Surge/Stall L, R
Condition: One or more of these occur:
•Engine indications are abnormal
•Engine indications are quickly nearing or show an exceedance
•Abnormal engine noises are heard, possibly with airframe
vibration
•There is no response to thrust lever movement
•Flames in the engine inlet or exhaust are reported
1 A/T ARM switch (affected side) . . . Confirm . . . . . . OFF
2 Thrust lever (affected side) . . . Confirm . . . . . . . .Retard until engine indications remain within appropriate limits or the thrust lever is at idle
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