Copyright . The Boeing Company. See title page for details.
NP.21.50  March 28, 2005

Normal Procedures -Amplified Procedures

Go–Around and Missed Approach Procedure
Pilot Flying  Pilot Monitoring 
At the same time: . push the TO/GA switch . call “FLAPS 15”  Position the FLAP lever to 15 and monitor flap retraction 
Verify: . the rotation to go–around attitude . that the thrust increases 
Verify that the thrust is sufficient for the go-around or adjust as needed. 
Verify a positive rate of climb on the altimeter and call “GEAR UP.”  Verify a positive rate of climb on the altimeter and call “POSITIVE RATE.” Set the landing gear lever to UP. 
Verify that the missed approach altitude is set. 
Above 400 feet, select appropriate roll mode and verify proper mode annunciation.  Observe mode annunciation. 
Verify that the missed approach route is tracked. 
At acceleration height, call “FLAPS ___” according to the flap retraction schedule.  Set the FLAP lever as directed. Monitor flaps and slats retraction. 
After flap retraction to the planned flap setting, select LVL CHG. VNAV may be selected if the flaps are up. 
Verify that climb thrust is set. 
Verify that the missed approach altitude is captured. 
Set the landing gear lever to OFF after landing gear retraction is complete. Set the engine start switches as needed. 
Call “AFTER TAKEOFF CHECKLIST.”  Do the AFTER TAKEOFF checklist. 

Copyright . The Boeing Company. See title page for details.
March 28, 2005  NP.21.51
Normal Procedures -Amplified Procedures

Landing Roll Procedure
Pilot Flying  Pilot Monitoring 
Disengage the autopilot. Control the airplane manually. 
Verify that the thrust levers are closed. Verify that the SPEEDBRAKE lever is up.  Verify that the SPEEDBRAKE lever is UP. Call “SPEEDBRAKES UP.” If the SPEEDBRAKE lever is not UP, call “SPEEDBRAKES NOT UP.” 
Verify correct autobrake operation. 
WARNING:After the reverse thrust levers are moved, a full stop landing must be made. If an engine stays in reverse, safe flight is not possible. 
Without delay, move the reverse thrust levers to the interlocks and hold light pressure until the interlocks release. Then apply reverse thrust as needed. 
By 60 knots, start movement of the reverse thrust levers to be at the reverse idle detent before taxi speed.  Call “60 KNOTS.” 
After the engines are at reverse idle, move the reverse thrust levers full down. 
Before taxi speed, disarm the autobrakes. Use manual braking as needed. 

After Landing Procedure
Start the After Landing Procedure when clear of the active runway.
Pilot Flying  Pilot Monitoring 
The captain moves or verifies that the SPEEDBRAKE lever is DOWN. 
Start the APU. 
Set the PROBE HEAT switches to OFF. 
Set the LANDING, TAXI, and STROBE light switches as needed. 

Copyright . The Boeing Company. See title page for details.
NP.21.52  March 28, 2005

Normal Procedures -Amplified Procedures 737 Flight Crew Operations Manual
Pilot Flying  Pilot Monitoring 
Set the ENGINE START switches to OFF. 
Set the weather radar to OFF. 
Set the AUTOBRAKE selector to OFF. 
Set the flap lever to UP. 
Set the transponder mode selector as needed. At airports where ground tracking is not available, select STANDBY. At airports equipped to track airplanes on the ground, select an active transponder setting, but not a TCAS mode. 

Copyright . The Boeing Company. See title page for details.
September 29, 2005  NP.21.53
Normal Procedures -Amplified Procedures

Shutdown Procedure 
Start the Shutdown Procedure after taxi is complete. 
Parking brake ....................................................................Set  C 
Verify that the parking brake warning light is illuminated. 
If towing is not needed: 
FASTEN BELTS switch ............................................OFF  F/O 
Electrical power ................................................................Set  F/O 
If APU power is needed: 

Verify that the APU GENERATOR OFF BUS light is illuminated. APU GENERATOR bus switches – ON Verify that the SOURCE OFF lights are extinguished. If external power is needed:
Verify that the GRD POWER AVAILABLE light is illuminated.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NG機組操作手冊Flight Crew Operations Manual FCOM 1(62)