Recall Memory Items

Question 1

Cabin Altitude

Answer 1

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

Question 2

Aborted Engine Start L, R
Condition: On the ground, an aborted engine start is
needed.

Answer 2

1 FUEL CONTROL switch
(affected side) . . . . . . . . . . . . . . . . . . . CUTOFF

Question 3

Dual Eng Fail/Stall
Condition: Engine speed for both engines is below idle.

Answer 3

1 FUEL CONTROL switches
(both) . . . . . . . . . . . . . . . . . . CUTOFF, then RUN
2 RAM AIR TURBINE switch . . . . . . . Push and hold
for 1 second

Question 4

ENG AUTOSTART L, R
Condition: Autostart did not start the engine.

Answer 4

1 FUEL CONTROL switch
(affected side) . . . . . Confirm . . . . . . . . CUTOFF

Question 5

ENG LIMIT EXCEED L, R
Condition: An engine limit exceedance occurs.

Answer 5

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

Question 6

ENG SURGE L, R
Condition: An engine surge or stall that requires crew
action is detected.

Answer 6

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

Question 7

Eng Svr Damage/Sep L, R
Condition: One or more of these occur:
* Airframe vibrations with abnormal engine
indications
* Engine separation

Answer 7

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

Question 8

FIRE ENG L, R
Condition: Fire is detected in the affected engine.

Answer 8

1 Choose one:
On the ground:
►►Go to step 13
In flight:
►►Go to step 2

2 A/T ARM switch
(affected side) . . . . . . . . . .Confirm . . . . . . OFF
3 Thrust lever
(affected side) . . . . . . . . . .Confirm . . . . . . Idle
4 FUEL CONTROL
switch (affected side) . . . . .Confirm . . . CUTOFF
5 Engine fire switch
(affected side) . . . . . . . . . .Confirm . . . . . . Pull
6 If the FIRE ENG message stays shown:
Engine fire switch
(affected side) . . . . . . . . . . Rotate to the stop
and hold for 1 second

Question 9

STABILIZER
Condition: One of these occurs:
* Stabilizer movement without a signal to trim
* The stabilizer is failed

Answer 9

1 STAB cutout switches (both) . . . . . . . . . CUTOUT
2 Do not exceed the current airspeed.

Question 10

AIRSPEED UNRELIABLE
Condition: The airspeed or Mach indications disagree
with AOA calculated airspeed.
Objective: To identify a reliable airspeed indication.

Answer 10

1 Autopilot disconnect 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