737 Flight Crew Operations Manual
13.10
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
13.10
LOW PRESSURE - Hydraulic Pump - System A and B
1 System A and B FLT CONTROL
switches (both) . . . . . Confirm. . . . . .STBY RUD
2System A and B
HYD PUMPS switches (all) . . . . . . . . . . . . . . OFF
3 Plan to land at the nearest suitable airport.
4 Plan a flaps 15 landing.
5 Set VREF 15.
6 Plan to extend flaps to 15 using alternate flap
extension.
7 Plan for manual gear extension.
8 Check the Non–Normal Configuration Landing
Distance table in the Advisory Information section
of the Performance Inflight chapter.
▼
Continued on next page
▼
MANUAL REVERSION
or
LOSS OF SYSTEM A AND SYSTEM B
MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
FLT CONTROL HYD PUMPS
A B ENG 1 ELEC 2 ELEC 1 ENG 2
LOW
PRESSURE
LOW
PRESSURE
LOW
PRESSURE
LOW
PRESSURE
Condition:
Hydraulic system A and B pressures are low.
Note: The drag penalty with the leading edge
devices extended may make it impossible to
reach an alternate field.
Note: When the gear has been lowered manually, it
cannot be retracted. The drag penalty with
gear extended may make it impossible to
reach an alternate field.
March 18, 2016
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