Non-normal Manoeuvres Flashcards
Memorise QRH non-normal manoeuvres
Approach to Stall Recovery
PF
Initiate the recovery:
Hold the control column firmly.
Disconnect the AP and AT.
Smoothly apply nose down elevator to reduce the angle of attack until buffet or stick shaker stops. Nose down stab trim may be needed.
Continue the recovery:
Roll in the shortest direction to wings level.
Advance thrust levers as needed.
Retract the speed brakes.
Do not change gear or flap configuration, except during lift off, if flaps are up, call for flaps 1.
Complete the recovery: Check airspeed and adjust thrust as needed. Establish pitch attitude. Return to the desired flight path. Re-engage the AP and AT if desired.
PM
Monitor Altitude and airspeed.
Verify all actions completed and call out any omissions.
Call out any trend toward terrain contact.
Set the FLAP lever as directed.
Rejected Takeoff (First Officer)
Verify the actions as follows:
Thrust levers closed.
AT disengaged.
Maximum brakes applied.
Verify speed brake lever is UP and call “SPEED BRAKES UP”. If speed brake lever is not up call “SPEED BRAKES NOT UP”
Verify reverse thrust applied. When both REV indicators are green, call “REVERSERS NORMAL”. If there is no REV indicated or the indicator remains amber, call “NO REVERSER LEFT/RIGHT ENGINE”, or “NO REVERSERS”.
Call out any omitted action items.
Call out 60 knots
Communicate the reject decision to the control tower as soon as practicable.
When the airplane is stopped, perform procedures as required (non normal checklist, brake cooling schedule etc)
GPWS Caution
Correct the flight path or the airplane configuration
GPWS Warning (PULL UP, OBSTACLE OBSTACLE PULL UP, TERRAIN TERRAIN PULL UP)
PF
Disconnect AP
Disconnect AT
Aggressively apply maximum thrust
Simultaneously roll wings level and rotate to an initial pitch attitude of 20 degrees
Retract speed brakes
If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet.
Do not change gear or flap configuration until terrain seperation is assured
Monitor radio altimeter for sustained or increasing terrain seperation.
When clear of terrain, slowly decrease pitch attitude and accelerate.
PM
Verify Maximum thrust
Verify all required actions have been completed and call out any omissions.
Monitor VS and altitude and call out any trend towards terrain.
After the recovery is completed, the aircraft position and LSALT must be crosschecked.
Note: if positive visual verification is made that no terrain hazard exists when flying daylight VMC prior to warning, the alert may be regarded as cautionary and approach continued.
TA
Look for traffic using traffic display as a guide. Call out any conflicting traffic.
If traffic is sighted, manoeuvre if needed.
RA (except a climb in landing configuration)
If maneuvering is required, disengage the autopilot and autothrottle.
Smoothly adjust pitch and thrust to satisfy the RA command.
Follow the planned lateral flight path unless visual contact with the conflicting traffic requires other action.
Both pilots should attempt to establish visual contact. Call out any conflicting traffic.
Climb RA in landing configuration
PF
Disengage the AP and disconnect AT.
Advance thrust levers forward to ensure maximum thrust is attained and call for FLAPS 20.
Smoothly adjust pitch to satisfy the RA command.
Follow the planned lateral flight path unless visual contact with the conflicting traffic requires other action.
Verify a positive rate of climb on the altimeter and call “GEAR UP”.
PM
Verify Maximum thrust is set. Position flap lever to 20 detent.
Verify a positive rate of climb on the altimeter and call “POSITIVE RATE”.
Set the landing gear lever to UP.
Both pilots should attempt to establish visual contact. Call out any conflicting traffic.
Upset Recovery Nose High
Recognise and confirm the developing situation.
Disconnect the AP and AT Recover by: Apply nose down elevator (as much as needed to obtain positive nose down pitch rate) Apply appropriate nose down stab trim Reduce thrust Roll to obtain nose down pitch rate Complete the recovery: When approaching the horizon, roll wings level Check airspeed and adjust thrust Establish pitch attitude
Upset Recovery Nose Low
Recognise and confirm the developing situation.
Disconnect the AP and AT Recover: Recover from stall if needed Roll in the shortest direction to wings level. If bank angle more than 90, unload and roll Complete the recovery: Apply nose up elevator Apply nose up trim if needed Apply thrust and drag if needed
Predictive Windshear Caution (WINDSHEAR AHEAD)
Manoeuvre as required to avoid the Windshear.
If on takeoff below V1, reject. After V1 perform Windshear escape manoeuvre.
Windshear Escape Manoeuvre (manual flight)
Disconnect AP
Push either go-around switch
Aggressively apply maximum thrust
Disconnect AT
Simultaneously roll wings level and rotate towards an initial pitch attitude of 15 degrees.
Retract speed brakes
Follow FD go around guidance if available.
Do not change gear or flap configuration until Windshear is no longer a factor.
Monitor vertical speed and altitude.
Do not attempt to regain lost airspeed until windshear is not a factor.
