Aborted Engine start
Engine start lever (affected engine) ….. cutoff
Airpseed Unreliable
1 A/P if engaged … disengage
2 A/T if engaged … disengage
3 F/D switches (both) … OFF
4 Flaps extended … 10° and 80%
Flaps up … 4° and 75%
APU Fire
1 APU fire switch … confirm … pull, rotate and hold for 1 sec
2 APU switch … Off
Cabin Altitude Warning
1 Don O2 masks and set regulators to 100%
2 Establish crew communications
3 Pressurisation mode selector … Man
4 Outflow VALVE switch … hold in CLOSE until fully closed
5 If cabin altitude is uncontrollable:
Passenger signs … ON
PASS OXYGEN switch … ON
6 Go to emergency decent checklist
Emergency decent
1 Announce the emergency decent:
PM - ATC
PF - Cabin Crew
2. Passenger signs … ON
3. Without delay descend to 10000ft or MSA
4. ENGINE START switches both … CONT
5. Thrust levers both … reduce to minimum
6. Speedbrake … Flight Detent
7. Set target speed to Vmo/Mmo
Engine Fire
- Autothrottle … disengage
- Thrust lever … confirm … close
- Engine start lever … confirm … cutoff
- Engine fire switch … confirm … pull
- If the engine fire switch or ENG OVERHEAT light is illuminated:
Engine fire switch … rotate to the stop and hold for 1 second
Engine limit surge or stall
- Autothrottle … disengage
- Thrust lever … confirm … retard until engine indications stay within limits or the thrust lever is closed.
Engine overheat
- Autothrottle … disengage
- Thrust lever … confirm … close
- If engine overheat light stays illuminated:
Go to the ENGINE FIRE or engine severe damage or seperation checklist.
Landing configuration
- Assure correct airplane landing configuratio
Takeoff configuration
- Assure correct airplane takeoff configuration
Loss of thrust on both engines
- ENGINE START switches (both) … FLT
- Engine start levers (both) … CUTOFF
- When EGT decreases :
Engine start levers (both) … IDLE detent - If EGT reaches a redline or there is no increase in EGT within 30 seconds:
Engine start lever … confirm … CUTOFF then IDLE detent.
If EGT again reaches a redline or there is no increase in EGT within 30 seconds repeat as needed.
Runaway Stabilizer
- Control column … gradp firmly
- Autopilot … disengage
- Autothrottle … disengage
- Control column and thrust levers control airplane pitch attitude and airspeed
- Main Electric stabilizer trim … reduce control column forces
- If the runaway stops after the autopilot is disengages:
Do not re-engage the autopilot or autothrottle - 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
