EasyManua.ls Logo

Boeing 737 - Page 312

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
13.12
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
13.12
Continued on next page
MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
continued
Note: Inoperative Items
Autopilots A and B inop
All flight spoilers inop
Roll rate will be reduced and speedbrakes will not
be available in flight.
Yaw damper inop
Trailing edge flaps normal hydraulic system
inop
The trailing edge flaps can be operated with the
alternate electrical system. Alternate flap
extension time to flaps 15 is approximately 2
minutes.
Leading edge flaps and slats normal hydraulic
system inop
The leading edge flaps and slats can be extended
with standby hydraulic pressure. Once extended,
they can not be retracted.
Normal landing gear extension and retraction
inop
Manual gear extension is needed.
Autobrake inop
Ground spoilers inop
Landing distance will be increased.
Normal and alternate brakes inop
Inboard and outboard brakes have accumulator
pressure only. On landing, apply steady brake
pressure without modulating the brakes.
March 18, 2016

Table of Contents

Other manuals for Boeing 737

Related product manuals