Memory items

Question 1

Engine Fire
or
Engine Severe Damage
or
Separation

Condition: one or more of these occur
- Engine Fire warning
- Airframe vibrations with abnormal engine indications
- Engine separation

Answer 1

1) Autothrottle (if engaged)…………… Disengage
2) Thrust Lever
(affected engine) ……..Confirm… Close
3) Engine Start Lever
(affected engine) ……..Confirm… CUTOFF
4) Engine Fire Switch
(affected engine) ……..Confirm… Pull
To Manually unlock the engine fire switch, press the override and pull

5) IF the engine fire switch or ENG OVERHEAT light is illuminated:

Engine Fire Switch (affected engine) ……….. Rotate to the stop and hold for 1 sec.

Question 2

ENGINE OVERHEAT

Condition: an overheat is detected in the engine

Answer 2

1) Autothrottle (if engaged) ……………… Disengage

2) Thrust lever
(affected engine) ……..Confirm… Close

3) IF the ENG OVERHEAT light stays illuminated:

• Go to the ENGINE FIRE or Engine Severe Damage or Separation Checklist on page 8.2

Question 3

Loss of Thrust on Both Engines

Condition: both of these occur:
* Both engines have a loss of thrust
* Both ENG FAIL aerts show

Objective: To restart at least one engine

Answer 3

1) ENGINE START Switches (both)……………. FLT
2) Engine Start Levers (both)……………………. CUTOFF
3) WHEN EGT decreases:

Engine Start Levers (both)………………… IDLE detent

4) IF EGT reaches a redline or there is no increase in EGT within 30 sec.

Engine Start Lever
(affected engine)……Confirm……………. CUTOFF, then IDLE Detent

IF EGT again reaches a redline or there is no increase in EGT within 30 sec., repeat as needed.

Question 4

Engine Limit or Surge or Stall

Condition: One or more of these occur:
- Engine indications are abnormal
- Engine indications are rapidly approaching or exceeding limits
- Unusual 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

Objective:
- To attempt to recover normal engine operations or shut down
the engine if recovery is not possible

Answer 4

1) Autothrottle (if enganged) …………………….. Disengage

2) Thrust lever
(affected engine)………Confirm………………. Retard until indications stay within limits or the thrust lever is closed

Question 5

APU Fire

Condition: Fire is detected in the APU

Answer 5

1) APU Fire Switch ……………Confirm………. Pull, Rotate to the stop and hold for 1 sec.

2) APU Switch ……………………………………… OFF

Question 6

Aborted Engine Start

Condition: On the ground, an aborted engine start is needed

Objective: To shut down the engine and motor it.

Answer 6

1) Engine Start Lever (affected engine) ………………. CUTOFF

Question 7

TAKEOFF CONFIGURATION

Condition:
On the ground, the intermittent cabin altitude/configuration warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates, when advancing the thrust levers to takeoff thrust

Answer 7

1) Assure correct airplane takeoff configuration

Question 8

LANDING CONFIGURATION

Condition:
In flight, the steady warning horn sounds

Answer 8

1) Assure correct airplane landing configuration

Question 9

CABIN ALTITUDE WARNING
or
RAPID DEPRESSURIZATION

Condition: One or more of these occur:
- A cabin altitude exceedance
- In flight, the intermittent cabin altitude/configuration warning horn sounds
or a CABIN ALTITUDE light (if installed and operative) illuminates

Answer 9

1) Don oxygen masks and set regulators to 100%
2) Establish crew communications
3) Pressurization mode selector ………………………….MAN
4) Outflow VALVE switch …………………………………….. Hold in CLOSE until outflow valve indication shows fully closed
5) If cabin altitude is uncontrollable:
* Passenger signs …………………………………………….. ON
* PASS OXYGEN switch ……………………………………. ON

-Go to the Emergency Descent checklist on page 0.1-

Question 10

Airspeed Unreliable

Condition:
Airspeed or Mach indications are suspected to be unreliable. (Items which might indicate unerliable airspeed are listed in the Additional Information section.)

Objective:
To identify a reliable airspeed indication, if possible, or to use the Flgith With Unreliable Airspeed table in the Performance Inflight chapter for the remainder of the flight.

Answer 10

1) Autopilot (if engaged) … Disengage
2) Autothrottle (if engaged) … Disengage
3) F/D switches (both) … OFF
4) Set the following gear up pitch attitude and thrust
* Flaps extended … 10° and 80% N1
* Flaps up … 4° and 75% N1

Question 11

Emergency Descent

Condtion: One or more of these occur:
- Cabin altitude cannot be controlled
- A rapid descent is needed

Answer 11

1) Announce the emergency descent. The Pilot Flying will advise the cabin crew, on the PA system, of the impending rapid descent. The Pilot Monitoring will advise ATC and obtain the area altimeter setting.
2) Passenger signs …………………………………………… ON
3) WITHOUT DELAY, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
4) ENGINE START switches (both) ………………….. CONT
5) Thrust levers (both) ………………………………………. Reduce Thrust to minimum or as needed for anti-ice
6) Speedbrake …………………………………………………… FLIGHT DETENT

If structural integrity is in doubt, limit speed as much as possible
and avoid high maneuvering loads.

7) Set target speed to Mmo/Vmo.

Question 12

Runaway Stabilizer

Condition: Uncommanded stabilizer trim movement occurs continuously or in a manner not appropriate for flight conditions

Answer 12

1) Control Column ……………………………… Hold Firmly
2) Autopilot (if engaged) …………………… Disengage
3) Autothrottle (if ingaged ………………… Disengage
4) Control column and thrust levels … Control airpline pitch attitude and airspeed
5) Main electric stabilizer trim ………….. Reduce control column forces

6) IF the runaway stops after the autopilot is disengaged
* Do NOT re-engage the autopilot or autothrottle
END OF CHECKLIST

7) IF the runaway CONTINUES after the autopilot is disengaged:
STAB TRIM CUTOUT switches (both) …………………………. CUTOUT

IF the runaway CONTINUES:
Stabilizer Trim Wheel ……………….. Grasp and hold