NNC - Memory Items

Question 1

AUTOMATIC UNLOCK

Answer 1

Condition: The correct emergency access code is entered.
Objective: To deny unauthorised access to the flight deck before the door automatically unlocks.

1 FLT DK DOOR lock selector . . . . . Rotate to DENY and hold for 1 second

Question 2

Emergency Descent

Answer 2

Condition: One of more of these occur

• Cabin altitude cannot be controlled
• A rapid descent is needed

1 Announce the emergency descent.
2 Passenger signs . . . . . . . . . . . . . . . . . . ON
3 Without delay, descend to the lowest safe altitude or 10,000ft, 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 manoeuvring loads.
7 Set target speed to Mmo/Vmo.

Question 3

Aborted Engine Start

Answer 3

Condition: On the ground, an aborted engine start is needed.
Objective: To shut down the engine and motor it.

1 Engine start lever (affected engine) . . . . . CUTOFF

Question 4

Engine Limit or Surge or Stall

Answer 4

Condition: One or more of these occur
- Engine indications are abnormal
- Engine indications are rapidly approaching or exceeding limits
- Abnormal engine noises are heard, possibly with airframe vibration
- There is not 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 operation or shut down the engine if recovery is not possible.

1 Autothrottle (if engaged) . . . . . . . Disengage
2 Thrust lever (affected engine) . . . Confirm . . Retard until engine indications stay within limits or thrust lever is closed

Question 5

CABIN ALTITUDE WARNING
or
Rapid Depressurisation

Answer 5

Condition: One or more of these occur

• A cabin altitude exceedance
• In flight, the intermittent cabin altitude/configuration warning horn sounds or the CABIN ALTITUDE light illuminates

1 Don oxygen masks and set regulators to 100%
2 Establish crew communications
3 Pressurisation mode sector . . . . . . . . . MAN
4 Outflow VALVE switch . . . Hold in CLOSE until outflow VALVE indications 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 6

Loss Of Thrust On Both Engines

Answer 6

Condition: Both of these occur
- Both engines have a loss of thrust
- Both ENG FAIL alerts show.
Objective: To restart at least one engine

1 ENGINE START switches (both) . . . . FLT
2 Engine start levers (both) . . . . . . . . . . CUTOFF
3 When EGT decreases:
Engine start levers (both) . . . . . . . . . IDLE detent
3 If EGT reaches a redline or there is no increase in EGT within 30 seconds:
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 seconds, repeat as needed.

Target speeds

• above FL270 - 275kt
• below FL270 - 300kt

Question 7

APU FIRE

Answer 7

Condition: Fire is detected in the APU.

1 APU fire switch . . . Confirm . . . Pull, rotate to the stop, and hold for 1 second
2 APU switch . . . . . . . . . . . . . . . . . . . . . OFF

Question 8

ENGINE FIRE
or
Engine Severe Damage or Separation

Answer 8

Condition: One or more of these occur

• Engine fire warning
• Airframe vibrations with abnormal engine indications
• Engine separation.

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 . . . Rotate to the stop and hold for 1 second
If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated:
Engine fire switch . . . Rotate to the other stop and hold for 1 second

Question 9

ENGINE OVERHEAT

Answer 9

Condition: An overheat is detected in the engine.

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 10

Runaway Stabilizer

Answer 10

Condition: Uncommanded stabilizer trim movement occurs continuously.

1 Control column . . . . . . . . . . . . . . . . . . . Hold firmly
2 Autopilot (if engaged) . . . . . . . . . . . . . . Disengage
Do not re-engage the autopilot.
Control the airplane pitch attitude manually with the control column and main electric trim as needed.
3 Autothrottle (if engaged) . . . . . . . . . . . . Disengage
Do not re-engage the autothrottle
4 If the runaway stops after the autopilot is disengaged: (checklist compete)
5 If the runaway continues after the autopilot is disengaged:
STAB TRIM CUTOUT switches (both) . . . . CUTOUT
If the runway continues:
Stabilizer trim wheel . . . . . . . . . . . . Grasp and hold

Question 11

Airspeed Unreliable

Answer 11

Condition: Airspeed or Mach indications are suspected to be unreliable. (Items which might indicated unreliable airspeed are listed in the Additional Information section.)
Objective: To identify a reliable airspeed indication, if possible, or to continue flight using the Flight With Unreliable Airspeed table in the Performance Inflight chapter.

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 12

LANDING CONFIGURATION

Answer 12

Condition: In flight, the steady warning horn sounds.

1 Assure correct aircraft landing configuration.

Question 13

TAKEOFF CONFIGURATION

Answer 13

Condition: On the ground, the intermittent cabin altitude/configuration warning horn sounds or a TAKEOFF CONFIG light illuminates when advancing the thrust levers to takeoff thrust.

1 Assure correct aircraft takeoff configuration.

Question 14

WARNING HORN (INTERMITTENT)
or
WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION

Answer 14

Condition: One of these occurs

• In flight, at an airplane flight altitude above 10,000 feet MSL, the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates
• On the ground, the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates when advancing the thrust levers to takeoff thrust.

1 If the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates in flight at an airplane altitude above 10,000 feet MSL:
Don the oxygen masks and set the regulators to 100%
Establish crew communications
Go to the CABIN ALTITUDE WARNING or Rapid Depressurisation checklist on page 2.1

2 If the intermittent warning horn sounds or TAKEOFF CONFIG light (if installed and operative) illuminates on the ground when advancing the thrust levers to takeoff thrust:
Assure correct airplane takeoff configuration.