Memory Items (QRH Quick Reference)

Question 1

ABORTED ENGINE START L, R

1.

Answer 1

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

Question 2

AIRSPEED UNRELIABLE

Condition: The airspeed or Mach indications disagree with AOA calculated airspeed.

Objective: To identify a reliable airspeed indication.

1.
2.
3.
4.

Answer 2

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

Question 3

CABIN ALTITUDE

Condition: Cabin altitude is excessive.

1.
2.
3.
4.

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 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
manoeuvring loads
* Descend at Vmo/Mmo

Question 4

DUAL ENG FAIL/STALL

Condition: Engine speed for both engines is below idle.

1.
2.

Answer 4

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

Question 5

ENG AUTOSTART L, R

Condition: Autostart did not start the engine.

1.

Answer 5

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

Question 6

ENG LIMIT EXCEED L, R

Condition: An engine limit exceedance occurs.

1.
2.

Answer 6

1. A/T ARM switch
   (affected side) . . . . . . . . . . . . . . . . . . .
   Confirm . . . . . . . . . . . OFF
   2 Thrust lever (affected side) . . . . . . . Confirm . . . . . .Retard until the ENG LIMIT EXCEED message blanks or
   the thrust lever is at idle

Question 7

ENG SURGE L, R

Condition: An engine surge or stall that requires crew action is detected.

1.
2.

Answer 7

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 8

Eng Svr Damage/Sep L, R

Condition:
One or more of these occur:
* Airframe vibrations with abnormal engine indications
* Engine separation

1.
2.
3.
4.

Answer 8

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 9

Evacuation (Captain)

Condition: An evacuation is needed.

1.
2.
3.
4.

Answer 9

1. PARKING BRAKE. . . . . . . . . . . . . . . Set
2. FUEL CONTROL switches (both) . . CUTOFF
3. Advise the cabin to evacuate.
4. EVAC COMMAND switch. . . . . . . . . ON

Question 10

Evacuation (First Officer)

Condition: An evacuation is needed.

1.
2.
3.
4.
5.
6.

Answer 10

1. OUTFLOW VALVE switches (both) . MAN
2. OUTFLOW VALVE MANUAL switches (both) . . . . . . . . . . . . . . Move to OPEN until the outflow valve indications show at the 12 o’clock position to depressurize the airplane.
3. Advise ATC.
4. Engine fire switches (both) . . . . . . Pull
5. APU fire switch . . . . . . . . . . . . . . . . Override and pull
6. If an engine or APU fire is observed or indicated:
   Related fire switch . . . . . . . . . . . . . . . . Rotate to the stop and hold for 1 second

Question 11

FD DOOR AUTO UNLOCK

Condition: The correct emergency access code is entered.

1.

Answer 11

1. FD DOOR ACCESS selector . . . . . Rotate to DENY and hold for 1 second.

Question 12

FIRE APU

Condition: Fire is detected in the APU.

1.
2.
3.

Answer 12

1. APU fire switch . . . . . . . . . . . Confirm . . . . . . Pull, rotate to the stop and hold for 1 second.
2. Choose one:
   FIRE APU message stays shown:
   Plan to land at the nearest Available
   Airport.
   ►►Go to step 3
   FIRE APU message blanks:
   ►►Go to step 3
3. Do not accomplish the following checklist:
   APU SHUTDOWN

Question 13

FIRE ENG L, R

Condition: Fire is detected in the affected engine.

1.
2.
3.
4.
5.
6.

Answer 13

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 14

Fire Eng on Ground L, R (Captain)

Condition: One or more of these occur on the ground:
* Fire is observed in the affected engine
* Fire is detected in the affected engine