Recall Actions

Question 1

FIRE ENG L, R

Answer 1

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

Question 2

STABILIZER

Answer 2

1 STAB cutout switches (both) . . . . . . . . . CUTOUT

2 Do not exceed the current airspeed.

Question 3

Cabin Altitude

Answer 3

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 15,000 feet (10,000 feet if fuel endurance is not critical), 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 4

Aborted Engine Start L, R

Answer 4

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

Question 5

Eng Lim/Surge/Stall L, R

Answer 5

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 6

Eng Svr Damage/Sep L,R

Answer 6

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 high airframe vibration occurs and continues after engine shutdown:

Without delay, reduce airspeed and descend to a safe altitude which results in an acceptable vibration level.

If high vibration returns and further airspeed reduction and descent are not practical, increasing the airspeed may reduce the vibration.

Question 7

Airspeed Unreliable

Answer 7

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

Question 8

Dual Eng Fail/Stall

Answer 8

1 FUEL CONTROL switches (both) . . . CUTOFF, then RUN

2 RAM AIR TURBINE switch . . . . . . . . .Push and hold for 1 second

Question 9

ENG AUTOSTART L, R

Answer 9

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