directions. Verify full travel, freedom of movement and controls return to center. Hold nose wheel steering wheel during rudder check to prevent nose wheel movement.
Flaps ..........................................................................______ Green light Flap position indicator and FLAP lever – Set for takeoff LEADING EDGE FLAPS EXTENDED green light – Illuminated
Stabilizer trim .......................................................................______units Verify stabilizer trim is set for takeoff. Cabin door ....................................................................................... Lock
 CABIN DOOR UNLOCKED light – Extinguished Takeoff briefing ........................................................................... Review The pilot taxiing calls “BEFORE TAKEOFF CHECKLIST DOWN TO
THE LINE.”
Normal Procedures -Amplified Procedures

737 Operations Manual
The pilot not taxiing accomplishes the BEFORE TAKEOFF checklist down to the line. – – – – – – – – – – – CLEARED FOR TAKEOFF – – – – – – – – – – – ENGINE START switches ............................................................ CONT Autothrottle ..................................................................................... ARM When approaching the takeoff runway, arm the autothrottle.
Transponder........................................................................................ ON LANDING lights and STROBE light switches .......................................................... As desired
 ON unless weather conditions make it undesirable. FMC position update ............................................................... As desired Enter runway offset on TAKEOFF REF page of FMC/CDU.
The pilot taxiing calls “BEFORE TAKEOFF CHECKLIST BELOW
THE LINE.”
The pilot not taxiing completes the BEFORE TAKEOFF checklist.

Copyright . The Boeing Company. See title page for details.
NP.20.24  June 4, 2004

Normal Procedures -Amplified Procedures 737 Operations Manual
Takeoff Procedure
PILOT FLYING  PILOT NOT FLYING 
Advance thrust levers to approximately 40% N1. 
Observe engine instruments stabilized and normal. 
Press either TO/GA switch to advance the thrust levers to takeoff N1. 
Verify mode annunciation.  Ensure thrust levers advance to takeoff N1. Observe mode annunciation. Note: In cases of extreme headwind, the thrust levers may not advance to full N1. In this case, manually advance the thrust levers as required. 
Note: After takeoff thrust is set, the captain’s hand must be on the thrust levers until V1. 
Monitor airspeed.  Monitor airspeed indications and call out any abnormalities. 
Hold light forward pressure on the control column, maintain directional control.  Monitor engine instruments. Verify oil pressure is not in the yellow band. 
Verify 80 knots.  Call “80 KNOTS.” Verify that A/T annunciation changes to THR HLD by 84 knots. 
Verify V1 speed. Rotate smoothly at VR.  Call “V1,” and call “ROTATE” at VR. Monitor flight instruments. 
When a positive rate of climb is indicated, call “GEAR UP” and continue rotation to takeoff pitch attitude.  Verify positive rate of climb. Position landing gear lever UP. 
Check flight instrument indications. 

Copyright . The Boeing Company. See title page for details.
June 4, 2004  NP.20.25
Normal Procedures -Amplified Procedures

After Takeoff Procedure
PILOT FLYING  PILOT NOT FLYING 
Maintain a minimum of V2 + 20 kts during initial climb. At light gross weight, a higher speed (up to V2 + 25) may be selected, to synchronize F/D pitch command and avoid objectionable body attitude.  Monitor engine instruments and cross–check flight progress. 
Above 400 feet, call for appropriate roll mode, if required. Verify proper mode annunciation.  Select/verify roll mode. Verify proper mode annunciation. 
Above 1,000 feet, call for N1 and flaps up maneuvering speed. Verify flight and thrust mode annunciations.  Select N1 and set flaps up maneuvering speed. Verify climb thrust is set. Verify proper mode annunciation. 
When above minimum altitude for autopilot engagement, engage A/P. Verify flight mode annunciation.  Verify autopilot engaged. 
Retract flaps on takeoff flap retraction speed schedule.  Position FLAP lever as directed and monitor flaps and slats retraction. 
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300機組操作手冊Flight Crew Operations Manual FCOM 1(40)