Manuevers

Question 0

Stall Recovery

Answer 0

Pilot Flying
• Initiate the recovery
• Hold the control column firmly
• Disconnect autopilot and autothrottle
• Smoothly apply nose down elevator to reduce the angle of attack until
buffet or stick shaker stops. Nose down stabilizer trim may be needed*
• 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

Pilot Monitoring
• Monitor altitude and airspeed
• Verify all required actions have been done and call out any omissions
• Call out any trend toward terrain contact
• Monitor altitude and airspeed
• Verify all required actions have been done and call out any omissions
• Call out any trend toward terrain contact
• Set the FLAP lever as directed
• Monitor altitude and airspeed
• Verify all required actions have been done and call out any omissions
• Call out any trend toward terrain contact

Question 1

Windshear Escape Recovery

Answer 1

Pilot Flying
• Disconnect autopilot.
• Push either go–around switch.
• Aggressively apply maximum* thrust.
• Disconnect autothrottle.
• Simultaneously roll wings level and rotate toward an initial pitch attitude of 15°.
• Retract speedbrakes.
• Follow flight director GA 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 no longer a factor.

Pilot Monitoring
• Verify maximum* thrust.
• Verify all required actions have been completed and call out any omissions.
• Monitor vertical speed and altitude.
• Call out any trend toward terrain contact, descending flight path, or significant airspeed changes.
Note: Aft control column force increases as the airspeed decreases. In all cases, the pitch attitude that results in intermittent stick shaker or initial buffet is the upper pitch attitude limit. Flight at intermittent stick shaker may be required to obtain positive terrain separation. Smooth, steady control will avoid a pitch attitude overshoot and stall.
Note: * Maximum thrust can be obtained by advancing the thrust levers to the takeoff or go- around limit. On airplanes with EECs operating normally, the pilot may advance the thrust levers full forward. If terrain contact is imminent, advance thrust levers full forward.