Aborted Engine Start L, R
Condition: On the ground, an aborted engine start is needed
FUEL CONTROL switch….CUTOFF
Dual Eng Fail/Stall
Condition: Engine speed for both engines is below idle.
FUEL CONTROL switches (both)… CUTOFF, then RUN
RAM AIR TURBINE switch… Push and hold for 1 second
Cabin Altitude
Condition: Cabin altitude is excessive
Don the oxygen masks
Establish crew communications
Check cabin altitude and rate
If cabin altitude is uncontrollable
PASS OXYGEN switch…Push to ON and hold for 1 second
Without delay, descend to the lowest safe altitude or 10,000 ft (highest). If fuel is critical, descend to 14,000 ft
Thrust Levers…Idle
Extend Speedbrakes
If structural integrity at doubt, limit airspeed and avoid high manoeuvring loads
Descend at Vmo/Mmo
If cabin altitude is controllable, continue normal operation
Eng Autostart L,R
Condition: Autostart did not start the engine
FUEL CONTROL switch (affected side)… Confirm… CUTOFF
Eng Limit Exceed L,R
Condition: An engine limit exceedance occurs.
A/T ARM switch (affected side)…Confirm…OFF
Thrust lever (affected side)…Confirm…Retard until ENG LIMIT EXCEED message blanks or the thrust lever is at idle
Eng Surge L,R
Condition: An engine surge or stall that requires Crew action is detected.
A/T ARM switch (affected side)…Confirm…OFF
Thrust lever (affected side)…Confirm …Retard until the ENG SURGE message blanks or the thrust lever is at idle.
Eng SVR Damage/Sep L,R
Condition: One or more of these occur:
-Airframe vibrations with abnormal indications
-Engine separation
A/T ARM switch (affected side)…Confirm…OFF
Thrust Lever (affected side)…Confirm…Idle
FUEL CONTROL switch (affected side)…Confirm…CUTOFF
Engine Fire switch (affected side)…Confirm…Pull
FIRE ENG L,R
Condition: fire is detected in the affected engine.
Choose one:
–On the ground: go to step 13
-In Flight:
A/T ARM switch (affected side)… Confirm… OFF
Thrust lever (affected side)…Confirm …Idle
FUEL CONTROL switch (affected side)…Confirm …CUTOFF
Engine fire switch (affected side)…Confirm …Pull
If the FIRE ENG message stays shown:
Engine fire switch (affected side)…Rotate to the stop and hold for 1 second
STABILIZER
Condition: One of these occurs,
-Stabilizer movement without a signal to trim
-The stabilizer is failed
STAB cutout switches (both)…CUTOUT
Do not exceed the current Air speed
AIRSPEED UNRELIABLE
Condition: The airspeed or Mach indications disagree with AOA calculated airspeed
Auto pilot disconnect switch …Push
A/T ARM switches (both) …OFF
F/D switches (both)…OFF
Set the following gear up pitch attitude and thrust:
-Flaps extended … 10° and 85% N1
-Flaps up … 4° and 70% N1

Approach to Stall or Stall recovery
RECOVERY
PF - INITIATE THE RECOVERY
•Smoothly apply nose down elevator to reduce the angle of attack until buffet or stick shaker stops
CONTINUE THE RECOVERY
•Roll in shortest direction to wings level if needed
Advance thrust levers as needed
Retract the speedbrakes
Do not change gear or flap except during liftoff, if flaps are up, call for Flaps 1
COMPLETE THE RECOVERY
•Check airspeed and adjust thrust as needed
Establish pitch attitude
Return to desired flight path
•Re-engage the autopilot and auto throttle if desired
PM
•Monitor altitude and airspeed
•Verify all required actions have been done and callout any omissions
•Callout any trend towards terrain contact
•Monitor altitude and airspeed
•Verify all required actions have been done and callout any omissions
•Callout any trend towards terrain contact
•Set the flap lever as desired
•Monitor altitude and airspeed
•Verify all required actions have been done and callout any omissions
•Callout any trend towards terrain contact
Rejected Takeoff
Prior to 80 kts reject for:
Master caution
System failure
Unusual noise or vibration
Tire failure
Abnormally slow acceleration
Takeoff config warning
Fire
Windshear
Unsafe conditions
Prior to V1
Fire
Engine failure
Windshear
Airplane is unsafe or unable to fly
PF
**Close thrust levers
Verify max brakes** either with Autobrake or manual braking
Apply reverse thrust up to the max amount consistent with conditions
Verify speedbrakes extended
Continue braking until certain the airplane can stop on the runway
When stopping is assured:
Start movement of the reverse thrust levers to reach reverse idle detent before taxi speed. After the engines are at reverse idle move the reverse thrust levers to full down.
PM
**Verify -
Thrust levers closed
Autothrottle’s disengaged
Maximum brakes applied
Reverse thrust applied**
SPEEDBRAKES UP
NO SPEEDBRAKES
REVERSERS NORMAL
NO REVERSER RIGHT
60 knots
Call ATC
Stopped
REMAIN SEATED AND AWAIT FURTHER INSTRUCTIONS
ATTENTION ATTENTION CABIN CREW AT STATIONS
Consider:
Wheel fuse plugs melting.
They need to clear the runway.
The requirement for remote parking
Wind Direction in case of fire.
Alerting fire equipment.
Not setting the part brake unless passenger evacuation is needed.
Advising the ground crew of hot brake hazard
Advising passengers of the need to remain seated or evacuate
Completion of non normal checklists
GPWS
Disengage autopilot
Disengage auto throttle
Aggressively apply max thrust
Wings level, Pitch 20°
Retract speedbrakes
Do not change configuration
Monitor RA
RECOVERY
Select speed
Adjust pitch and thrust
Engage automatics
Recover flight path
TCAS
TA
Look for traffic, manoeuvre as needed
RA
TCAS RA
Disengage AP
Disengage AT
Follow command, pitch and thrust
Clear of conflict
Climb RA in landing config
TCAS RA
Disengage AP
Disengage AT
Max Thrust
Flaps 20
Positive climb gear up
Clear of conflict
Upset recovery
Recognise and confirm
Disengage autopilot
Disconnect auto throttle
NOSE HIGH
Nose down elevator
Trim
Reduce thrust
Roll
Recover wings level
Adjust speed and thrust
NOSE LOW
Stall recovery?
Roll in shortest direction
Recover
Nose up
Trim
Adjust thrust and drag
PM
Call-out attitude, airspeed and altitude
Verify actions have been completed
Windshear
Manual flight
WINDSHEAR TOGA
Discon AP
Push TOGA
Aggressively apply max thrust
Disconnect A/Thr
Wings level, Pitch 15°
Speedbrakes retracted
Follow FD toga guidance
Automatic flight
WINDSHEAR TOGA
Push TOGA
Verify toga FMAs
Verify GA thrust
Verify Speedbrakes retracted
Monitor system performance
BOTH
-Do not change gear or flap configuration until windshear is no longer a factor.
-Maintain wings level to maximise climb gradient unless a turn is required for obstacle clearance.
-Monitor vertical speed and altitude.
-Do not attempt to regain lost airspeed until wind is no longer a factor.
-When wind is no longer a factor call CLEAR OF WINDSHEAR
Cleaning up…
(Can set 85% N1 and 10 degrees)
Bug speed
A/T on with…FLCH, VNAV
If windshear is suspected on take off then use OPT calc under RTG for WINDSHEAR
Engine failure in the cruise
EFATO
Missed approach
RNP approach
ILS approach
Divert
RLP
When should you land at the nearest suitable airport?
When the checklist states it
Fire or smoke continues
Only 2 AC power sources remain (2 main engine generators or one main generator and both APU generators)
Any other situation as determined by flight crew to have an affect on safety
QRH CI.2.7
Requirements of an Adequate Aerodrome and
EDTO Alternate Aerodrome
RG1 OPS.15
Adequate Aerodrome
-Rescue Fire
-Runway length and strength
-Visual or electronic glideslope
EDTO alternate Aerodrome
-facilities for passengers and crew
-authorised in Ops Specs
-has a passenger recovery plan for over EDTO180
-met forecast available
-one instrument approach procedure
-ATC or flight service available 30 min before use
-Rescue Fire min cat 4
-Visual or electronic glideslope
-Sufficient lighting. At night medium intensity and runway threshold lighting is minimum unless low intensity light is authorised. Plus standby power available unless day or another alternate carried.
