737 Memory / Quick Actions

Question 1

ENGINE FIRE

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, press the override and pull).
5 If the engine fire switch or Overheat light is illuminated:
- Eng fire switch: rotate to stop and hold for one second
(If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated):
- Eng fire switch: rotate to other stop and hold for one second

Question 2

Airspeed Unreliable

Answer 2

1 Autopilot (if engaged): Disengage
2 Autothrottle (if engaged): Disengage
3 F/D Switches (both): OFF
4 Set following gear up pitch attitude and thrust:
Flaps extended: 10 deg and 80% N1
Flaps up: 4 degrees and 75% N1

Question 3

APU FIRE

Answer 3

1 APU Fire Switch: Confirm: Pull, rotate to the stop and hold for 1 second.
2 APU Switch: Off

Question 4

CABIN ALTITUDE WARNING or Rapid Depressurisation (Airline specific)

Answer 4

• Don oxygen Masks and set regulators to 100%
• Establish crew communications
• Captain “I HAVE CONTROL”
• FO “YOU HAVE CONTROL”
• Pressurisation selector; Man (Man AC Classic)
• Outflow valve switch: hold in close until outflow VALVE indication shows fully closed
• If cabin altitude is uncontrollable:
• “PRESSURISATION NOT CONTROLLABLE”
  
  • Pass. Signs On
  • PASS OXYGEN switch: On
  • Go to emergency descent checklist on page 0.1

Question 5

Emergency Descent (company specific, FO inital actions)

Answer 5

• Engine Start Switches……CONT
• Declare Mayday, obtain regional QNH
• Transponder…….7700
• Confirm MSA
• Call “2000 feet to go” then “1000 feet to go”
• Engine Start Switches……As Needed

Question 6

ENGINE OVERHEAT

Answer 6

1 Autothrottle (if engaged): Disengage
2 Thrust Lever (affected engine): Confirm, close
3 If ENGINE OVERHEAT light stays illuminated: go to ENGINE FIRE or Engine severe damage or separation checklist 8.8

Question 7

LANDING CONFIGURATION

Answer 7

Assure correct airplane landing configuration

Question 8

TAKEOFF CONFIGURATION

Answer 8

Assure correct airplane takeoff configuration

Question 9

Runaway Stabiliser

Answer 9

1 Control Column: Hold firmly
2 Autopilot: Disengage (do not re-engage)
3 Autothrottle: Disengage
4 Control Column and Thrust levers: Control airplane pitch attitude and airspeed
5 Main Electric Stabiliser trim: Reduce control column forces
6 If runaway stops after autopilot is disengaged: Do not re-engage the autopilot or autothrottle
—————
7 If runaway continues after autopilot is disengaged: STAB TRIM CUTOUT switches (both): CUTOUT
If runaway continues: stabilizer trim wheel: grasp and hold

Question 10

SMOKE/FIRE in cargo compartment (main deck) G-JMCU

Answer 10

1 O2 Masks: On, 100%
2 Smoke goggles (if required): ON
3 Crew Communication: Establish
4 Cockpit Door: Close
5 CARGO DEPRESS switch: push (light on)

Question 11

Uncommanded Roll

Answer 11

1 Autopilot: Disengage
2 Maintain control of A/C with all available flight controls. If roll is uncontrollable, immediately reduce pitch angle / AoA and increase airspeed. Do not attempt to maintain altitude until control is recovered
3 Autothrottle: Disengage
4 Verify thrust is symmetrical

Question 12

Loss Of Thrust On Both Engines

Answer 12

1 ENGINE START switches (both): FLIGHT
2 Engine Start Levers (both): CUTOFF
3 WHEN EGT DECREASES: Engine Start Levers (both): IDLE
4 IF EGT reaches 930C or there is no increase of EGT within 30 seconds:
Engine Start Lever (affected engine): Confirm: CUTOFF then Idle detent

IF EGT again reaches 930C or there is no increase in EGT in 30 seconds; repeat as needed

Question 13

Aborted Engine Start

Answer 13

1 Engine Start Lever…..(Affected Engine)…….CUTOFF

Question 14

Engine Limit or Surge or Stall

Answer 14

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

Question 15

Rejected Take-off (captain)

Answer 15

• Simultaneously: Close thrust levers, disengage autothrottle and apply max manual wheel brakes or verify operation of RTO autobrake.
• Raise SPEED BRAKE lever
• Apply reverse thrust to maximum amount consistent with conditions.
• Continue max braking until certain the aircraft can stop on the runway.

Question 16

Windshear escape manoeuvre in manual flight (PF)

Answer 16

• Disengage autopilot
• Push either TO/GA switch
• Aggressively apply maximum thrust (EECs normal - full forward, EECs alt only apply full forward if terrain contact is imminent)
• Disengage Autothrottle
• Simultaneously roll wings level and rotate toward an initial pitch attitude of 15 degrees
• Retract speedbrakes
• Follow flight director TO/GA guidance (if available) (do not exceed pitch limit indication)
• Do not change flap or gear configuration until windshear is no longer a factor
• Monitor vertical speed and altitude
• Do not attempt to regain lost airspeed until windshear is no longer a factor.

Question 17

Windshear escape manoeuvre in automatic flight (PF)

Answer 17

• Push either TO/GA switch (if not available disconnect autopilot and autothrottle and fly manually)
• Verify TO/GA mode annunciation
• Verify GA thrust
• Retract speedbrakes
• Monitor system performance (severe windshear can exceed performance of AFDS - be prepared to disconnect and fly manually)
• Do not change flap or gear configuration until windshear is no longer a factor
• Monitor vertical speed and altitude
• Do not attempt to regain lost airspeed until windshear is no longer a factor.

Question 18

When should you carry out the GPWS Warning (Terrain Escape) Manoeuvre?

Answer 18

• Activation of “PULL UP” or “TERRAIN TERRAIN PULL UP” warning.
• Activation of the “PULL UP” or “OBSTACLE OBSTACLE PULL UP” warning.
• Other situations resulting in unacceptable flight toward terrain.

Question 19

Response to a GPWS caution?

Answer 19

Correct the flight path, airplane configuration, or airspeed.

Question 20

Response to GPWS “TOO LOW TERRAIN”?

Answer 20

Correct the flight path, airplane configuration, or airspeed.
(It’s a GPWS caution)

Question 21

Response to GPWS “DON’T SINK”?

Answer 21

Correct the flight path, airplane configuration, or airspeed.
(It’s a GPWS caution)

Question 22

Correct response to “PULL UP” or “TERRAIN TERRAIN PULL UP” or “OBSTACLE OBSTACLE PULL UP”

Answer 22

• Disengage autopilot
• Disengage autothrottle
• Aggressively apply maximum thrust
• Simultaneously roll wings level and rotate to an initial pitch attitude of 20 degrees
• Retract Speedbrakes
• If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet
• Do not change flap or gear configuration until terrain separation assured
• Monitor radio altimeter for sustained or increasing terrain separation
• When clear of terrain, slowly decrease pitch attitude and accelerate

Question 23

FO’s actions during Emergency Descent (Airline specific)

Answer 23

After captain calls “EMERGENCY DESCENT”, commence QRH memory items:
- Passenger Signs: ON
- Engine Start Switches: CONT
- Declare a Mayday
- Obtain regional QNH
- Transponder: 7700
- Confirm MSA
- At 2000’ to level off: “2000 feet to go”
- At 1000’ to level off: “1000 feet to go”
- When cabin altitude is at or below 10,000’: Engine Start Switches: As needed

Question 24

Captain’s actions during Emergency Descent (airline specific)

Answer 24

• Call “EMERGENCY DESCENT”
• Call “CABIN CREW DESCENT, CABIN CREW DESCENT”
• Initiate turn if required, using HDG SEL
• Without delay, descend to lowest safe altitude or 10,000: set lower alt. on MCP, select LVL CHG
• Close thrust levers, extend speedbrakes
• Set target speed Mmo/Vmo (unless structural damage)
• Set 10,000’ or MSA in MCP altitude window
• At 2000’ to level off, commence level off, set speed to 300kts or LRC.
• At 1000’ to level off, smoothly lower the SPEED BRAKE lever to the DOWN detent and level off, add thrust and stabilise on altitude and airspeed.

New course of action based on weather, oxygen, fuel remaining and available airports. LRC may be needed.