Position the flap lever to agree with the flap position. APU (bleed air source if available) .................................................. Start Flap Lever ........................................................................................... Set
Position the FLAP lever to agree with the FLAPS position indicator.
Emergency equipment ................................................................... Check Fire extinguisher - Checked and stowed Crash axe - Stowed Escape ropes - Stowed Other needed equipment - Checked and stowed.
Flight recorder switch ......................................................... Guard closed Circuit breakers .............................................................................. Check Accomplish the Interior and Exterior Inspection if required, except for
items requiring electrical or hydraulic power.
Accomplish the following Preflight Procedure - First Officer items:
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Supplementary Procedures -Engines, APU 737 Flight Crew Operations Manual
Overheat and fire protection panel............................................Check TEST switch - Hold to FAULT/INOP TEST switch - Hold to OVHT/FIRE EXTINGUISHER TEST switch - Check
APU switch
(bleed air source, if available) ................................................ START On the captain's command, the first officer reads and the captain does the following items:
Oxygen ............................................................................. Test and set YD651 - YK104 CAB/UTIL power switch.............................................................. ON YD651 - YK104 IFE/PASS seat power switch......................................................... ON YA613 - YC413 GALLEY power switch ................................................................ ON EMERGENCY EXIT LIGHTS switch..........................Guard closed Passenger signs .............................................................................. Set HYDRAULIC PUMP switches .................................................... ON Air conditioning panel ................................................................... Set APU BLEED air switch - ON PACK switches - AUTO or HIGH Engine BLEED air switches - ON Parking brake ................................................................................. Set Note: The wheels should be chocked in case the brake pressure has bled down. Papers ...................................................................................... Aboard When cleared for Engine Start, do the following: Air conditioning PACK switches.................................................OFF ANTICOLLISION light switch .................................................... ON
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Supplementary Procedures -Engines, APU 737 Flight Crew Operations Manual
Ignition select switch ................................................................IGN-R Engine Start Engine No. 1 start ............................................................ Accomplish Only N1, N2, and oil quantity are displayed until the EEC’s are
powered. Generator 1 switch ........................................................................ON IRS mode selectors .....................................................OFF, then NAV
Verify that the ON DC lights illuminate, then extinguish Verify that the ALIGN lights are illuminated. FMC/CDU ................................................................ Set IRS position
WARNING:If engine No. 1 was started using a ground air source, to minimize the hazard to ground personnel, the external air should be disconnected and engine No. 2 started using the Engine Crossbleed Start procedure.
Engine No. 2 start ............................................................ Accomplish Generator 2 switch ........................................................................ON Complete the Preliminary Preflight Procedure - Captain or First Officer
by doing the following items:
PSEU light ........................................................... Verify extinguished
GPS light ............................................................. Verify extinguished
SERVICE INTERPHONE switch ............................................... OFF
ENGINE panel ...............................................................................Set
Verify that the REVERSER lights are extinguished Verify that the ENGINE CONTROL lights are extinguished EEC switches - ALTN then ON
Oxygen panel..................................................................................Set CREW OXYGEN pressure indicator - Check
Copyright . The Boeing Company. See title page for details.
Supplementary Procedures -Engines, APU 737 Flight Crew Operations Manual
Verify that the pressure meets dispatch requirements. Note: PASSENGER OXYGEN switch activation causes deployment of the passenger oxygen masks. PASSENGER OXYGEN switch - Guard closed
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本文链接地址：737NG机组操作手册Flight Crew Operations Manual FCOM 1(78)
