Copyright . The Boeing Company. See title page for details.
NP.20.12 June 4, 2004
Normal Procedures -Amplified Procedures
737 Operations Manual
Parking brake .......................................................................................Set
Parking brake warning light –Illuminated STABILIZER TRIM cutout switches ..................................... NORMAL Wheel well fire warning system ........................................................ Test Note: Delete this test if AC busses were powered during the fire
warning check. Alert ground personnel before this test is accomplished with the APU operating. The fire warning light flashes and the horn sounds on the APU ground control panel.
Test switch – Hold to OVHT/FIRE Verify fire warning bell sounds, master FIRE WARNING lights, MASTER CAUTION lights and OVHT/DET annunciator illuminate.
Fire warning BELL CUTOUT switch – Push
Verify WARN lights and fire warning bell cancel.
WHEEL WELL fire warning light – Illuminated
VHF comm radios ...............................................................................Set
VHF NAV radios ...........................................................Set for departure
EFIS control panel ...............................................................................Set
EHSI range selector – As desired
EHSI mode selector – MAP
Weather radar switch – OFF
Map switches – As desired
ADF radios ..........................................................................................Set
FLOOD and PANEL light controls .........................................As desired
Transponder .........................................................................................Set
RUDDER and AILERON trim ..............................................Free & zero
Check trim for freedom of movement, set trim at zero units.
Normal Procedures -Amplified Procedures
737 Operations Manual
HF radio .............................................................................................. Set
WARNING:Do not key the HF radio while airplane is being fueled. Injury to personnel or fire may result.
STABILIZER TRIM override switch .....................................NORMAL Seat ................................................................................................ Adjust Verify positive horizontal (fore and aft) seat lock. Rudder pedals ................................................................................ Adjust Adjust rudder pedals to permit full rudder deflection and brake application. Hold nose wheel steering wheel while moving rudder
pedals. Papers ........................................................................................... Aboard FMC/CDU ........................................................................................... Set
IDENT page – Check Verify airplane and engine MODEL and NAV DATA ACTIVE dates are correctly displayed. POS INIT page – Set Verify GMT is correct. Enter local time if desired. RTE page – Select Enter route by company route identifier or origin and destination airports, then waypoints and/or airways. DEPARTURES page – Select Select the active runway and departure/transition procedures, if known. RTE page – Select Verify selected departure and route. Correct route discontinuities, ACTIVATE and EXEC. PERF INIT page – Select
Copyright . The Boeing Company. See title page for details.
NP.20.14 June 4, 2004
Normal Procedures -Amplified Procedures 737 Operations Manual
Verify total fuel quantity is displayed on the CDU and that the fuel quantity indicators agree, and are adequate for the planned flight. Enter gross weight or zero fuel weight, fuel reserve and cost index. Enter cruise altitude and verify transition altitude. If desired, enter cruise wind and ISA deviation or top–of–climb temperature. EXEC.
DEPARTURES page – Select (if not previously entered)
Select appropriate runway and departure/transition procedures. Select the RTE page. Verify selected departure. Correct any route discontinuities and EXEC.
Thrust mode display – Check
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