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BATTERY START (EXTERNAL OR APU
ELECTRICAL POWER NOT AVAILABLE)
Wheels.............................................................................................CHOCKED
Tow Bar...............................................................................DISCONNECTED
Parking Brakes ............................................................................................SET
The red PARKING BRAKE ON light will not illuminate until the battery switch
is turned ON. The brakes pressure gauge is inoperative until AC power is
applied.
DC Meter Selector (23 V Minimum) .......................................................BAT
Battery Switch............................................................................. ON/CAPPED
Electric Hyd Pumps....................................................................................OFF
Landing Gear Lever........................................................... DOWN/3 GREEN
Radar Switch...............................................................................................OFF
Circuit Breakers and Emergency Equipment ........................... CHECKED
Air Conditioning and Pressurization ........................................................SET
Fire Control Panel ......................................................................... CHECKED
Conduct a fire test (wheel well fire warning is not powered at this time).
IRS Mode.....................................................................................................OFF
Before Start Checklist............................................................ACCOMPLISH
The door lights and pneumatic pressure gauge are inoperative.
When Ready to Start:
External Air...............................................................................CONNECTED
If APU is source of start air:
APU..................................................................................................START
APU Bleed Air .......................................................................................ON
Standby Power Switch ...............................................................................BAT
Selecting BAT powers the standby bus and provides AC power for the right
ignition and VHF communications on the #1 radio.
(Continued)
ENGINES, APU
Sec. 2.7 Page 6
Rev. 11/15/02 #41
Continental
737
Flight Manual
Ignition Selector Switch ........................................................................RIGHT
Only the N1 and EGT instruments and LOW OIL PRESSURE low lights operate.
The engine start switch must be held to GRD. Move the engine start lever to
IDLE after 30 seconds. Release the ENGINE START switch at 16-17% N1.
If APU air is being used, starter cutout can be confirmed by a definite drop
in APU EGT.
Starting No. 1 engine first will allow greater safety to ground personnel
handling external air/elec.
If the isolation valve cannot be opened, start No. 2 engine first and advise
ground personnel to use extreme caution. It is preferred to wait for external
electrical power rather than to start No. 2 engine with external air and
battery.
Engine No. 1 Start ..................................................................ACCOMPLISH
Generator No. 1 Switch................................................................................ON
Standby Power Switch ........................................................................... AUTO
Engine Instruments.............................................................................CHECK
IRS Mode Selectors ................................................................................... NAV
FMC/CDU....................................................................................................SET
External Air..............................................................................DISCONNECT
Receiving Aircraft Checklist......................................................COMPLETE
Engine No. 2 Start .............................................................USE APU AIR OR
CROSSBLEED PROCEDURE
After Engines are Started:
Wheel Well Fire Warning............................................................. CHECKED
After Start Checklist ...................................................................COMPLETE
* * * *
737
Flight Manual
Continental
ENGINES, APU
Sec. 2.7 Page 7
Rev. 11/15/02 #41
BCD EEC ALTERNATE MODE
An EEC ALTN light illuminated indicates the EEC is in alternate control
mode.
IF On Ground:
Consult MEL Section 73 for effectivity. If aircraft is not in compliance
according to the MEL, Do Not Takeoff.
EEC Mode Switches (Both).....................................................ALTN
　
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