Position the FLAP lever to agree with the FLAPS position indicator. Emergency equipment .............................................................. Check Circuit breakers ........................................................................ Check Flight recorder ............................................................................... Set Rain repellent ........................................................................... Check
Crash axe .................................................................................Stowed On the Captain's command, the First Officer reads and the Captain accomplishes the following items:
Oxygen & interphone ............................................................... Check
Standby power ............................................................................. BAT
GALLEY power ............................................................................ON
EMER EXIT LIGHTS..........................................................ARMED
Passenger signs .............................................................................. Set
HYD PUMP switches....................................................................ON
Supplementary Procedures -Engines, APU 737 Operations Manual
Air conditioning & pressurization ..................1 Pack, bleeds ON, set Parking brake ................................................................................. Set Note: The wheels should be chocked in case the brake pressure
has bled down. Papers ...................................................................................... Aboard
Cleared for Start PACK switches ............................................................................OFF ANTICOLLISION light switch .................................................... ON Ignition select switch ............................................................... IGN-R
Engine Start Engine No. 1 should be started first. Engine No. 1 start ............................................................Accomplish
(Airplanes with EIS) Only N1, N2, EGT and fuel flow
indications are displayed. (Airplanes with conventional engine instruments) Only the N1 and EGT instruments 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.
Generator No. 1 switch ................................................................. ON
IRS mode selectors ..................................................................... NAV
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 No. 2 switch ................................................................. ON After Start
Copyright . The Boeing Company. See title page for details.
SP.7.2 June 4, 2004
Supplementary Procedures -Engines, APU 737 Operations Manual
Complete the preliminary flight deck preparation by checking the following items: MACH AIRSPEED WARNING test switches ......................Push STALL WARNING TEST switches ......................................Push REVERSER lights .............................................................. Check PMC switches ..........................................................................ON Passenger oxygen switch ............................................. NORMAL
Crew oxygen ....................................................................... Check Accomplish panel scan to ensure that the flight deck preparation procedure is complete.
AFTER START checklist ........................................... Accomplish IRS alignment .............................................. Complete & no flags The airplane is ready for taxi. Refer to the normal checklists for subsequent checks.
Engine Crossbleed Start
Prior to using this procedure, ensure that the area to the rear is clear.
Engine BLEED air switches ...............................................................ON
APU BLEED air switch.................................................................... OFF
PACK switches ................................................................................. OFF
ISOLATION VALVE switch .........................................................AUTO
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本文鏈接地址：737-300機(jī)組操作手冊(cè)Flight Crew Operations Manual FCOM 1(58)
