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Rotate to the stop and hold until the respective BOTTLE DISCHARGED light
illuminates.
IF FIRE Light Or ENG OVERHEAT Light Remains Illuminated:
Note: If high airframe vibration occurs and continues after engine is
shut down:
Without delay, reduce airspeed and descend to a safe altitude
which results in an acceptable vibration level. If high vibration
returns and further airspeed reduction and descent are not
practicable, increasing airspeed may reduce vibration.
Continue The Checklist.
Isolation Valve ...................................................................................... CLOSE
Note: If Cabin is Pressurized Using APU Bleed Air, DO NOT Close the
APU Bleed Valve or turn the Left Pack Switch OFF.
Pack Switch (Affected Side) ......................................................................OFF
APU Bleed Switch.......................................................................................OFF
APU (If Available)............................................................START & ON BUS
>>@ APU starts are not assured above 25,000 feet.
Fuel ...................................................................................................BALANCE
Normally, if center tank fuel is available and the pumps are on, no action is
required. If center tank fuel is not available opening of the CROSSFEED
switch allows fuel to feed from both main tanks, however any pressure
differential from the operating pumps may cause an imbalance. Continue to
monitor fuel and balance fuel as necessary to maintain within aircraft
limitations.
Transponder Mode Selector.........................................................................TA
TCAS equipped transponders communicate between aircraft to provide
appropriate coordinated avoidance maneuvers. When performance is
limited, such as with an inoperative engine, select TA ONLY to prevent
receiving RAs beyond the aircraft’s capabilities, and to prevent
communicating to other aircraft an ability to perform a RA maneuver.
(Continued)
737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 Page 11
Rev. 11/15/02 #41
IF Wing Anti-Ice Is Required:
Do not open isolation valve unless the fire has been extinguished.
Isolation Valve Switch .....................................................................AUTO
IF Emergency Occurred During Takeoff or Missed Approach,
Abbreviated AFTER TAKEOFF checklist Items Are:
Gear .............................................................. OFF, LIGHTS CHECKED
>>@ Red gear lights will remain illuminated if either or both
throttles are at IDLE. Advance throttle(s) to ensure gear lights.
Flaps................................................................................. AS REQUIRED
Position flaps as required for maneuvering.
Land At Nearest Suitable Airport.
IF Considering a restart of the engine, refer to ENGINE START – IN FLIGHT
checklist, this section.
* * * *
IF Not considering a restart accomplish the ONE ENGINE INOPERATIVE
APPROACH AND LANDING checklist at the appropriate time.
Logbook entries, if time and conditions permit:
1. Windmill RPM
2. Windmill time
3. Windmill oil pressure
4. Length of time engine windmilled without oil pressure
5. Oil pressure at time of shutdown
Note: Coordinate any procedure requiring an engine shutdown with ATC as
soon as possible. If the shutdown occurs at an altitude above the single
engine ceiling, initiate driftdown procedures. FMC information is
available on the engine-out climb or cruise pages as applicable. Use
these pages for driftdown speeds and power settings.
* * * *
OR
ENGINES, APU
Sec. 2.7 Page 12
Rev. 11/15/02 #41
Continental
737
Flight Manual
Engine Failure After V1 Procedure
If engine failure occurs at or after V1, follow this procedure:
PILOT FLYING (PF) PILOT MONITORING (PM)
Maintain directional control, rotate to
takeoff attitude at VR.
Call “ROTATE” at VR.
When a positive rate of climb is indicated,
call “GEAR UP.”
Call “POSITIVE RATE” when positive
rate of climb indicated. Position the
landing gear lever UP on command.
* Climb at V2, limit bank angle to 15
degrees.
Monitor engine and flight instruments.
400 feet AGL, call “HEADING SELECT.” Select HDG SEL.
** At flap retraction altitude “SET TOP
BUG,” retract flaps (as required on the
flap/speed schedule). Maintain pitch
attitude indicated by F/D. (See Note
below.)
Set airspeed cursor to VM Flaps 0. Retract
the flaps on command. Monitor flap
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