Manoeures Flashcards
Approach to Stall or Stall 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 the shortest direction to wings level if needed* • Advance thrust levers as needed • Retract the speedbrakes • Do not change gear or flap configuration, 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 the desired flight path • Re-engage the autopilot and autothrottle if desired
RTO - Captain
Without delay: Simultaneously close the thrust levers, disengage the autothrottles, and apply maximum manual wheel brakes or verify operation of RTO autobrake. If RTO autobrake is selected, monitor system performance and apply manual wheel brakes if the AUTOBRAKE message is displayed or deceleration is not adequate. Apply reverse thrust up to the maximum amount consistent with conditions. Verify the speedbrakes are extended. Continue maximum braking until certain the airplane will stop on the runway.
When stopping is assured: Start movement of the reverse thrust levers to reach the reverse idle detent before taxi speed. After the engines are at reverse idle, move the reverse thrust levers to full down.
RTO - FO
Verify actions as follows: Thrust levers closed. Autothrottles disengaged. Maximum brakes applied. Reverse thrust applied. Verify speedbrake lever UP and call “SPEEDBRAKES UP.” If speedbrake lever not UP call “SPEEDBRAKES NOT UP.” When both REV indications are green, call “REVERSERS NORMAL.” If there is no REV indication(s) or the indication(s) stays amber, call “NO REVERSER LEFT ENGINE,” or “NO REVERSER RIGHT ENGINE,” or “NO REVERSERS.” Call “AUTOBRAKES” when EICAS message AUTOBRAKES is displayed. Call out any omitted action items.
Call out “60 KNOTS”.
Communicate the reject decision to the
control tower and cabin as soon as
practical.
GPWS caution
Correct the flight path or the airplane configuration.
GPWS warning
• Disconnect autopilot • Disconnect autothrottle(s) • Aggressively apply maximum* thrust • Simultaneously roll wings level** and rotate to an initial pitch attitude of 20° • Verify the speedbrakes are retracted • 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 separation is assured
• Monitor radio altimeter for sustained or
increasing terrain separation
• When clear of the terrain, slowly
decrease pitch attitude and accelerate
TA
Look for traffic using traffic display as a guide. Call out any conflicting traffic
If traffic is sighted, manoeuvre if
needed.
RA
If manoeuvring 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.
Attempt to establish visual contact. Call out any conflicting traffic.
FOR CLIMB IN LANDING COFIG
Disengage the autopilot and autothrottle. 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.”
Attempt to establish visual contact. Call out any conflicting traffic.
UPSET nose HIGH recover
• Recognize and confirm the developing situation
• Disconnect autopilot and autothrottle Recover: • Apply nose down elevator. Apply as much elevator as needed to obtain a nose down pitch rate • Apply appropriate nose down stabilizer trim* • Reduce thrust • Roll (adjust bank angle) to obtain a nose down pitch rate.* Complete the recovery: • When approaching the horizon, roll to wings level • Check airspeed and adjust thrust • Establish pitch attitude.
UPSET Nose LOW recover
• Recognize and confirm the developing situation’
• Disconnect autopilot and autothrottle Recover: • Recover from stall, if needed • Roll in the shortest direction to wings level. If bank angle is more than 90 degrees, unload and roll.* Complete the recovery: • Apply nose up elevator • Apply nose up trim, if needed* • Adjust thrust and drag, if needed.
WINDSHEAR caution
Manoeuvre as required to avoid the windshear
WINDSHEAR escape manoeuvre
MANUAL FLIGHT • Disconnect autopilot • Push either TO/GA switch • Aggressively apply maximum* thrust • Disconnect autothrottle(s) • Simultaneously roll wings level and rotate toward an initial pitch attitude of 15° • Verify the speedbrakes are retracted • Follow flight director TO/GA guidance (if available)**
AUTOMATIC FLIGHT • Push either TO/GA switch.*** • Verify TO/GA mode annunciation • Verify GA* thrust • Verify the speedbrakes are retracted • Monitor system performance****
MANUAL OR AUTOMATIC FLIGHT • 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 no longer a factor