737 Flight Crew Operations Manual
6.11
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
6.11
12 Choose one:
13 Choose one:
14 BUS TRANSFER switch . . . . . . . . . . . . . . . AUTO
This restores power to the remaining transfer
bus.
15 ELEC HYD PUMP switches
(both) . . . . . . . . . . . . . . . . . . ON, one at a time
16 YAW DAMPER switch . . . . . . . . . . . . . . . . . . . ON
17 Plan to land at the nearest suitable airport. Only
one main AC power source remains.
►►Go to step 22
▼
Continued on next page
▼
▼LOSS OF BOTH ENGINE DRIVEN GENERATORS continued▼
APU can be connected to bus 2:
►►Go to step 13
APU can not be connected to bus 2:
APU GEN switch. . . . . . . . . . . . ON bus 1
►►Go to step 13
A single BUS OFF light extinguishes:
►►Go to step 14
Both BUS OFF lights stay illuminated:
►►Go to step 18
December 15, 2017
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