Memory Items

Question 1

ABORTED ENGINE START

Answer 1

FUEL CONTROL SWITCH (affected side)…. CUTOFF

Question 2

AIRSPEED UNRELIABLE

Answer 2

1 Autopilot disconnect switch…. Push
2 A/T Arm switches (both)…. OFF
3 FD switches (both)…. OFF
4 Set the following gear up pitch and thrust:

Flaps extended…. 10 degrees and 85% N1
Flaps up…. 4 degrees and 70% N1

Question 3

CABIN ALTITUDE

Answer 3

1 Don the oxygen mask
2 Establish crew communication
3 Check the cabin altitude and rate
4 IF the cabin altitude is uncontrollable:

PASS OXYGEN switch…. Push to ON and hold for one second

Without delay descend to lowest safe altitude or 10,000 feet, whichever is higher.

To descend:

Move the thrust levers to idle
Extend the speed-brakes

IF structural integrity is in doubt, limit airspeed and avoid high maneuvering loads.

Descend at VMO/MMO

Question 4

DUAL ENGINE FAIL/STALL

Answer 4

Fuel control switches (both)…. Cutoff, then RUN
RAM AIR TURBINE…. Push and hold for 1 second

Question 5

ENG AUTOSTART L,R

Answer 5

Condition: During a ground start, one of these occur:
AUTOSTART did not start the engine
Fuel control switch is in RUN with low engine RPM with the AUTOSTART witch OFF
————————————————————-

Fuel control switch (affected side)…. Cutoff

Question 6

ENG LIMIT/SURGE/STALL L,R

Answer 6

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

Question 7

Eng Svr Damage/Sep L, R

Answer 7

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

Question 8

[] FIRE ENG L, R

Condition: Fire is detected in the affected engine.

Answer 8

1 Choose one:

> ON THE GROUND = Follow checklist
INFLIGHT 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 shows:

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.