EasyManua.ls Logo

Boeing 737 - AUTO SLAT FAIL; Elevator Tab Vibration

Boeing 737
752 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
737 Flight Crew Operations Manual
9.8
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
9.8
AUTO SLAT FAIL
1 Continue normal operation.
1 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
3 Consider landing at the nearest suitable airport.
4 Stay at or below the reduced airspeed at which the
vibration stopped for the rest of the flight. Limit
bank angle to 15° until below 20,000 feet.
5 Do not deploy speedbrakes in flight.
Continued on next page
AUTO SLAT
FAIL
AUTO SLAT FAIL
Condition:
The auto slat system is failed.
Elevator Tab Vibration
Condition:
An elevator tab vibration occurs in flight.
One or more of the following may be an
indication of an elevator tab vibration:
Vibration that originates, and is strongest,
in the aft part of the airplane but can be
felt throughout the airplane
Vibration that is felt in the control wheel
and rudder pedals
Vibration that causes items attached to
the airplane, such as sun visors, to move.
Do not use speedbrakes or change aircraft
configuration to reduce airspeed. Do not reduce
airspeed below the minimum speed for the
existing flap setting and gross weight.
2
Smoothly reduce airspeed until the vibration
stops.
March 18, 2016

Table of Contents

Other manuals for Boeing 737

Related product manuals