Memory Items

Question 1

Aborted engine start ? (1 item)

Answer 1

1. Engine start lever (affected engine) — CUTOFF

Question 2

Airspeed unreliable (4 items)

Answer 2

1. Autopilot (if engaged) ………………….. Disengage
2. Auto throttle (if engaged) ………….. Disengage
3. F/D switches (both) …… Off
4. Gear …………………… Up (Confirm or set) Depends on phase of flight
   SET Either:
   Flap setting/pitch attitude:
   - 4° with zero flaps @ 75% N1
   - 10° extended flaps @ 80% N1

Note: If ASU occurs during take off, pitch to 15° nose attitude as per normal. Climb to 400 ft AGL then pitch to 10°. Ensure N1 is 89-90%

Question 3

APU Fire (2 items)

Answer 3

1. APU Fire switch …. CONFIRM ….. PULL, ROTATE to stop and HOLD for 1 sec.
2. APU switch ………………… OFF

Question 4

Engine LIMIT, SURGE or STALL (2 items)

Answer 4

1. Autothrottle …………….. Disengage
2. Thrust lever ……. CONFIRM …….. Retard until engine indications stay within limits or until thurst lever closed.

Question 5

AUTOMATIC UNLOCK (AUTO UNLK) - 1 Item

Answer 5

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

Question 6

Cabin Altitude Warning or Rapid depressurisation (7 items)

Answer 6

1. Don oxygen mask and set regulators to 100%.
2. Establish crew communication.
3. Pressurization mode selector ………………………….. MAN
4. Outflow VALVE switch ……………………………………. Hold in CLOSE until the outflow VALVE indication shows fully closed.
5. IF cabin altitude is uncontrollable:
   5.2 Passenger signs ……………………………………………… ON
   5.3 PASS OXYGEN switch ……………………………………… ON

Question 7

Emergency Descent (7 items)

Answer 7

1 Announce the emergency descent over PA:
- PF advises Cabin Crew)
- PM declares emergency to ATC, “PAN-PAN - Descending! - REQUEST QNH”

2 Passenger signs . . . . . . . .. . . . . …….. ON

3 MCP: …….. Set LSALT/FL100 whichever is higher
……… Select LVL CHG
(Without DELAY, descend to LSALT)

4 ENGINE START switches (both) . . . . . . . . . CONT

5 Thrust levers (both) . . . . . . . . . Reduce to minimum or as needed for anti-ice

6 Speedbrake . . . . . . …… FLIGHT DETENT

7 Set target speed to Mmo/Vmo if safe to do so.

After setting speed: Check STRUCTURAL INTEGRITY before setting maximum descent speed - If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads

If time permits: Squawk 7700 and turn on ALL LIGHTS

Question 8

ENGINE FIRE or Engine Severe Damage or Separation (5 items)

Good way to remember name of checklist- This checklist lives in CH 8 (Fire Protection) - not CH 7 (Engines)

Answer 8

1. Autothrottle …. DISENGAGE (PF)
2. Thrust lever (affected engine) ………CONFIRM (PM) .…. CLOSE (PF)
3. Engine start lever (affected engine) …. CONFIRM (PF) ….. CUTOFF (PM)
4. Engine fire switch (affected engine) … CONFIRM (PF) ………. PULL (PM)
5. IF engine fire switch OR ENG OVERHEAT light is illuminated:
   - Engine fire switch (affected engine)…………………………..ROTATE to the stop and hold for 1 sec.

Question 9

Take off CONFIGURATION (TAKEOFF CONFIG)

NOTE: Also Sounds for incorrect landing configuration.

Answer 9

1. Assure correct airplane takeoff configuration.

Question 10

Landing CONFIGURATION (TAKEOFF CONFIG horn)

NOTE: Also Sounds for incorrect take off configuration.

Answer 10

1. Assure correct airplane Landing configuration.

Question 11

Loss of thrust on both engines (4 items)

Answer 11

1. Engine START switches (BOTH) ……….. FLT
2. Engine start lever (BOTH) …………………. CUTOFF
3. When EGT decreases:
   - Engine start levers (BOTH) ………….. IDLE detent
   Check EGT:
4. IF EGT reaches RED LINE (950º) or shows NO INCREASE within 30 seconds:
   - Engine start lever (effected side): ………… CONFIRM ………………. CUTOFF,

…. then IDLE detent

Consider GEN BUSSES on APU, ENG Ignition SW to “BOTH” & Thrust lever’s closed

—> Repeat step 4 as needed to start engines.

Note: The max engine EGT for starting engines ON THE GROUND is 725 °C, in flight it is 950°C (Max take off EGT). The reason for using Take off EGT is that this is the maximum EGT the engine can take before it starts damaging components. As safety is more important during takeoff and when you’ve lost all thrust, you can push the engine to its limits to ensure the safest possible outcome.

Consider Closing thrust levers before attempting to start engines if

Question 12

Engine OVERHEAT (3 items)

Answer 12

1. Autothrottle …………………………………………………. Disengage
2. Thrust lever …………………. CONFIRM ………….. CLOSE

—> IF the ENG OVERHEAT light STAYS illuminated:
3. Go to ENGINE FIRE, SEVERE DAMAGE or seperation checklist.

Question 13

Runaway STABILISER (5 items

Answer 13

1 Control column. . . . . . . .. . . Hold firmly

2 Autopilot (if engaged) . . . . . . .. . . .Disengage

3 Autothrottle (if engaged). . . . . . . . . . .Disengage

4 Control column and thrust levers . . . . . . . . . . . . . . .Control airplane pitch attitude and airspeed

5 Main ELECTRIC Stabilizer trim . . . . . . . . . . . . . . . Reduce control column forces

6 If RUNAWAY STOPS: DO NOT RE ENGAGE AUTOPILOT

7 If the runaway continues after the autopilot is disengaged:

STAB TRIM cutout switches (both) . . . . . . .. . CUTOUT (Pilot MONITORING)

If the runaway continues:

Stabilizer trim wheel . . . . . . . . . . Grasp and hold

The control column must be held firmly before the autopilot is disconected

Question 14

SEVERE TURBULENCE

Answer 14

Yaw Damper ………………………………..…ON

Passenger signs …………………………. ON

ENGINE START …………………………… FLT

AUTOPILOT ……………………………….. CWS A/P

Auto throttle………………………………. Disengage

Set thrust & SPEED as needed for the phase of flight. Change thrust setting only if needed to modify an unacceptable speed trend.

Request different Heading or Altitude.

Note: If sustained trimming occurs, disengage the autopilot. NOTE: The airplane can withstand higher gust loads with the flaps UP

CWS is selected to maintain a pitch attitude to ensure, autopilot doesnt follow VNAV path, as this could result in overspeeding, overstressing or stalling the aircraft in severe turbulence.

Question 15

When should an engine start be aborted?

Answer 15

If…

1. N1 or N2 increases very slowly after the EGT increases (Hung start)
2. No oil pressure indication by the time that the engine is stable at idle (Mechanical damage)
3. EGT does not increase by 15 seconds after the engine start lever is moved to IDLE (Wet start)
4. EGT quickly nears or exceeds the start limit/ REDLINE (Hot start)

—————————
Remember S.P.E.L causes Hot, wet, Hung Mechanical damage):

S- SLOW rotation
P- PRESSURE indication low
E- EGT anomalies
L- LIMITS exceeded (EGT Redline)

Question 16

If an engine fire or Engine Limit occurs at V1, when should the memory items be initiated?

Answer 16

No lower than 400 feet AGL, when the flight path is under control and the gear has been retracted.

Question 17

Engine Failure (Flame out) in cruise

Answer 17

***Remember ACMLA (CALMA reworded)
MATE!! (”I have control”)
1. Identify failure (Confirm effected engine)
Control Aircraft (Aviate)
2. Auto Throttle DISENGAGE (THIS MUST BE DONE FIRST TO PREVENT A/T from going down when LVL CHNG selected)
Set MCT (CON) - AMBER indication in N1
SLOW DOWN TO OEI speed (230/230):

3. MCP: …….. Set LSALT/FL100
   ……… Select LVL CHG
4. Re-engage Autopilot if needed

Check CDU for EO speed and altitude

1. Move into FORDEC

Question 18

Engine FIRE in cruise

Answer 18

Aviate, Navigate, Communicate

“I have control” & Disconect A/T
“Identify the failure” (Ask PM):

1. Auto Throttle DISENGAGE (Must be done first to prevent levers closing when selecting LVL CHNG)
2. Complete Engine FIRE NNC memory items:
   - T/L (PF) …. Confirmed (PM) ….. CLOSE
   - Eng St Lever (PM) … confirmed (PF) …. CUTOFF
   - Eng Fire Sw (PM … confirmed (PF) …. PULL
   - Rotate if necessary if either RED fire warning or AMBER ‘OVERHEAT’ lights stay illuminated.
3. SSET MCT on operating Engine Only
4. MCP: …….. Set LSALT/FL100
   ……… Select LVL CHG

Consider:
ACMLA (CALMA re ordered) ====> (A/T disengage, CON, MCP, LVL CHNG, A/P)

Check CDU for EO speed and altitude

Check and Re-engage autopilot on operational side

Move onto FORDEC

Question 19

All engine Go around procedure (PF):

FCTM 5.66

Answer 19

1. Simultaneously call “Going AROUND” & Push the TO/GA switch
2. Verify THRUST increasing (Above 80% N1)
3. Call “FLAPS 15°”
4. Rotate to 15º P.A
5. Wait for call “POSITIVE RATE” from PM, Verify ‘positive rate’ on altimeter, & Call “GEAR UP”
6. Above 400ft AGL, VNAV should engage
7. Call FMA’s
8. Follow F/D’s
9. Confirm Missed Approach altitude and track
10. At Acceleration altitude (1000 AGL), call “BUG UP” (LVL CHNG) or confirm speed change (VNAV SPD - recommended)
11. At ‘FLAPS UP’ & UP speed (Flaps UP manoeuvering speed)
12. Engage A/P - SPD INTV if necessary

NOTE: A/P cannot be engaged until FINAL G/A flaps selected and either LVL change or VNAV SPD is engaged

Question 20

Can the aircraft withstand higher gust loads with the flaps extended or with the flaps retracted?

FCOM SP.16.26 & FCTM 1.57

Answer 20

The airplane can withstand higher gust loads in the clean configuration

Turbulent air penetration speeds provide high/low speed margins in severe turbulent air.

Question 21

Single engine Go Around

Answer 21

1.Simultaneously: Call “Going Around” AND Push TO/GA

Auto Pilot will disengage - CHECK THRUST INCREASES

2. Call Flaps 1
3. Manually conduct G/A: Rotate to EOTA (Approximately 10º)
4. PM calls “THRUST SET ….. POSITIVE RATE”
5. PF Call’s “Gear Up”
6. Follow F/D’s (As climb rate increases, F/D
   pitch commands maintain a target speed.)
7. @400ft call FMA’s (VNAV ‘bump’)
   Follow F/D
8. At ACCELARATION HT (1000ft AGL)
9. Call “BUG UP”
10. Once speed is above ‘F1 SPD’ (1) Call ‘FLAPS UP’
    9.When flaps UP:
    - Verbalise “Autothrottle Off, Set Max Continuous Thrust”
    - VNAV continues to target VREF40+70 (Flaps UP)

Check CALMA - Clean up, A/T off, LVL CHANGE or VNAV SPD, MCT, A/P engage

11. !!Engage A/P (Maintain ‘UP’ speed to LSALT) !!

Question 22

If you have an engine failure (flame out) at V1, when should the engine failure NNC (Memory items) be actioned?

FCTM 3.33 & 8.16

Answer 22

Accomplish the appropriate memory checklist items as soon as the flight path is under control, the gear has been retracted and a safe altitude (minimum 400ft AGL). Reference items should be accomplished by the PM as soon as practical: Recommendation is flaps UP + MCT + IAS=Vref40+70 (manoeuvre spd) + A/P engaged ——> CALMA

Question 23

If you have an engine Fire at V1, when should the engine fire NNC be completed?

FCOM 8.16

Answer 23

Above 400ft AGL, if the flight path is under control, and the gear has been retracted, if safe to do so, accomplish the NNC memory items.

Question 24

Will an engine tailpipe fire cause the fire alarm to go off?

Answer 24

No

Question 25

After discharging a fire bottle during an Engine Fire emergency, how long should you wait before discharging the second bottle?

Answer 25

30 Seconds Note: Boeing has removed the need to discharge a second bottle as part of the memory items as it can sometimes take longer than 30 seconds for the fire light to go out (temperature threshold)