737 Flight Crew Operations Manual
Maneuvers -
Non-Normal Maneuvers
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA MAN.1.5
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 needed to obtain a positive
terrain separation. Use smooth, steady control to avoid a pitch
attitude overshoot and stall.
Note: Do not use flight director commands.
Note: *Maximum thrust can be obtained by advancing the thrust levers
to the takeoff or go-around limit. If terrain contact is imminent,
advance thrust levers full forward.
Note: If positive visual verification is made that no obstacle or terrain
hazard exists when flying under daylight VMC conditions before
a terrain or obstacle warning, the alert may be regarded as
cautionary and the approach may be continued.
Pilot Flying Pilot Monitoring
Disengage autopilot.
Disengage autothrottle.
Aggressively apply maximum* thrust.
Simultaneously roll wings level and
rotate to an initial pitch attitude of 20.°
Retract speedbrakes
If terrain stays a threat, continue
rotation up to the pitch limit indicator
(if available) or stick shaker or initial
buffet.
Assure maximum* thrust.
Verify all needed actions have been
completed and call out any omissions.
Do not change gear or flap
configuration until terrain separation is
assured.
Monitor radio altimeter for sustained
or increasing terrain separation.
When clear of terrain, slowly decrease
pitch attitude and accelerate.
Monitor vertical speed and altitude
(radio altitude for terrain clearance and
barometric altitude for a minimum safe
altitude.)
Call out any trend toward terrain
contact.
December 15, 2017
To Next Page
Loading...
