737 Flight Crew Operations Manual
14.26
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
14.26
11 System A
FLIGHT CONTROL switch . . . Confirm . .STBY RUD
12 System A
HYD PUMP switches (both). . . . . . . . . . . . . . OFF
Warning! Do not repressurize hydraulic system
A in flight or on the ground because
the landing gear may retract.
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Continued on next page
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▼Manual Gear Extension continued▼
Note: Inoperative Items
Autopilot A inop
Autopilot B is available.
Inboard flight spoilers inop
Roll rate and speedbrake effectiveness may be
reduced in flight.
Normal landing gear extension and retraction
inop
Manual gear extension after system A is
depressurized is needed.
Ground spoilers inop
Landing distance will be increased.
Alternate brakes inop
Normal brakes are available.
Engine 1 thrust reverser normal hydraulic
pressure inop
Thrust reverser will deploy and retract at a slower
rate and some thrust asymmetry can be
anticipated during thrust reverser deployment.
Nose wheel steering inop
March 24, 2017
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