737 Flight Crew Operations Manual
7.9
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
7.9
16 When engine parameters have stabilized:
ENGINE START switch
(operating engine) . . . . . . . . . . . . .As needed
Thrust lever
(operating engine) . . . . . . . . . Advance slowly
Engine GEN switch
(operating engine side). . . . . . . . . . . . . . . ON
►►Go to step 26
17 Thrust levers (both) . . . . . . . . . . . . . . . . . Close
18 WING ANTI–ICE switch . . . . . . . . . . . . . . . . OFF
19 PACK switches (both) . . . . . . . . . . . . . . . . . OFF
20 APU BLEED air switch . . . . . . . . . . . . . . . . . . ON
21 Ignition select switch . . . . . . . . . . . . . . . . BOTH
22 Engine start
lever (either) . . . . . . Confirm. . . . . . . CUTOFF
23 ENGINE START switch . . . . . . . . . . . . . . . . . GRD
24 When N2 is at or above 15%:
Engine start lever. . . . . . . . . . . . .IDLE detent
The engine can accelerate to idle very
slowly especially at high altitudes or in
heavy precipitation. If N2 is steadily
increasing and EGT stays within limits, do
not interrupt the start.
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Continued on next page
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▼Loss Of Thrust On Both Engines continued▼
March 18, 2016
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