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IRS display unit by selecting HDG/STS.]
If both BUS OFF lights remain illuminated:
ALL EXTERIOR LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . .OFF
[Conserves battery power.]
Avoid icing conditions.
Note: Flight in icing conditions may result in erroneous
flight instrument indications.
Plan to land at the nearest suitable airport. A fully
charged battery will provide a minimum of 30 minutes of
standby power.
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

6.8
6.8
Condition: The STANDBY PWR OFF light illuminated indicates
the AC standby bus is not powered.
STANDBY POWER SWITCH . . . . . . . . . . . . . . . . . . . . . . . . BAT
[A fully charged battery provides a minimum of 30 minutes of standby
power.]
If either generator bus is re-established:
STANDBY POWER SWITCH . . . . . . . . . . . . . . . . . . . . AUTO
Condition: A TRANSFER BUS OFF light illuminated indicates the
related transfer bus is not powered.
BUS TRANSFER SWITCH . . . . . . . . . . . . . . .OFF THEN AUTO
STANDBY POWER OFF
TRANSFER BUS OFF
June 3, 2005
737 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Engines, APU Section 7
Copyright © The Boeing Company. See title page for details.
 TOC.7.1
Table of Contents
NNAC.B7 NOoRn-NToErmDal EChNecGkliIsNts-EEn gSinTeAs, ARPTU . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.1
APU DET INOP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.1
APU FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.2
APU HIGH OIL TEMPERATURE/FAULT . . . . . . . . . . . . . . . . . . . 7.2
APU LOW OIL PRESSURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.2
APU OVERSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.3
ENGINE FAILURE/SHUTDOWN . . . . . . . . . . . . . . . . . . . . . . . . . 7.4
ENGINE FIRE, SEVERE DAMAGE OR SEPARATION . . . . . 7.6
ENGINE FIRE/OVERHEAT DETECTOR FAULT . . . . . . . . . . . . . 7.8
ENGINE HIGH OIL TEMPERATURE . . . . . . . . . . . . . . . . . . . . . . 7.8
ENGINE IN-FLIGHT START . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10
ENGINE LIMIT/SURGE/STALL . . . . . . . . . . . . . . . . . . . . . . . 7.12
ENGINE LOW OIL PRESSURE . . . . . . . . . . . . . . . . . . . . . . . . . . 7.13
ENGINE OIL FILTER BYPASS . . . . . . . . . . . . . . . . . . . . . . . . . . 7.14
ENGINE OVERHEAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.15
ENGINE TAILPIPE FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.16
HIGH ENGINE VIBRATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.17
LOSS OF THRUST ON BOTH ENGINES . . . . . . . . . . . . . . . . 7.18
LOW IDLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.19
ONE ENGINE INOPERATIVE LANDING . . . . . . . . . . . . . . . . . 7.20
POWER MANAGEMENT CONTROL (PMC)
INOPERATIVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.21
REVERSER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.22
REVERSER UNLOCKED (IN FLIGHT) . . . . . . . . . . . . . . . . . . . 7.22
START VALVE OPEN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.23
VOLCANIC ASH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.24
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.7.2
Non-Normal Checklists -
Engines, APU
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 7.1
7.1
NNC.7 Non-Normal Checklists-Engines, APU
Condition: During a ground start, and abort engine start
conditions occurs.
If the ENGINE START switch is in GRD:
Motor the engine for 60 seconds.
ENGINE START switch . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If the ENGINE START switch is in OFF:
After N2 decreases below 20%:
ENGINE START switch . . . . . . . . . . . . . . . . . . . . . . . GRD
Motor the engine for 60 seconds.
ENGINE START SWITCH . . . . . . . . . . . . . . . . . . . . . .OFF
Condition: The APU DET INOP light illuminated indicates the
APU fire detection loop has failed.
APU SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
CAUTION: Do not operate the APU. An APU fire would not
be detected and the APU would continue to run.
　
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