Memory Items Flashcards
Airspeed Unreliable
Condition: Airspeed or Mach indications are suspected to be unreliable. (Items which can indicate unreliable airspeed are listed in the Additional Information section.)
Objective: To identify a reliable airspeed indication, if possible, or to continue the flight using the Flight With Unreliable Airspeed table in the Performance Inflight chapter.
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 degrees and 85% N1
Flaps up . . . . . . . . . . .4 degrees and 70% N1
Automatic Unlock
Condition: The correct emergency access code is entered.
1 FLT DECK DOOR lock selector. . . . . . . . . . . . . . . . . . . Rotate to DENY and hold for 1 second
CABIN ALTITUDE
Condition: Cabin altitude is excessive.
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 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
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 AUTOSTART L, R
Condition: During a ground start, one of these 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
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 or the response is abnormal •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 stay within limits or the thrust lever is at idle
Eng Svr Damage/Sep L, R
Condition: One or more of these occur: •Airframe vibration 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
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
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.
Aborted Engine Start L, R
1 FUEL CONTROL switch (affected side) . . . . . . . . . . . . . . . . . . . CUTOFF
