Copyright . The Boeing Company. See title page for details.
June 1, 2005 NP.21.39
Normal Procedures -Amplified Procedures 737 Flight Crew Operations Manual
Pilot Flying Pilot Monitoring
Verify V1 speed. YA721, YA722 Call “V1.” YA801 - YC413, YK101 - YK104 Verify the automatic V1 callout or call “V1.”
At VR, rotate toward 15° pitch attitude. After liftoff, follow F/D commands. Establish a positive rate of climb. At VR call “ROTATE.” Monitor airspeed and vertical speed.
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.
Above 400 feet radio altitude, call for a roll mode as needed. Select or verify the roll mode.
At thrust reduction height, call “SET CLIMB THRUST.” Push the N1 switch.
Verify that climb thrust is set.
At acceleration height, call “SET FLAPS UP SPEED.” Set the flaps up maneuvering speed.
Verify acceleration. Call “FLAPS ___” according to the flap retraction schedule. Set the FLAP lever as directed. Monitor flaps and slats retraction.
After flaps and slats retraction is complete, call “VNAV.” Push the VNAV switch.
Engage the autopilot after minimum altitude for autopilot engagement.
After flap retraction is complete: . Set or verify engine bleeds and air conditioning packs are operating . Set the engine start switches as needed . Set the AUTOBRAKE selector to OFF . Set the landing gear lever to OFF after landing gear retraction is complete
Call “AFTER TAKEOFF CHECKLIST.” Do the AFTER TAKEOFF checklist.
Copyright . The Boeing Company. See title page for details.
NP.21.40 June 1, 2005
Normal Procedures -Amplified Procedures 737 Flight Crew Operations Manual
CAUTION: Do not allow the shoulder harness straps to retract quickly. Buckles can pull or damage circuit breakers.
Takeoff Flap Retraction Speed Schedule
Takeoff Flaps At Speed (display) Select Flaps
25 V2 + 15 “15” “5” “1” 15 5 1 UP
15 or 10 V2 + 15 “5” “1” 5 1 UP
5 V2 + 15 “1” 1 UP
1 “1” UP
Limit bank angle to 15° until reaching V2 + 15
Copyright . The Boeing Company. See title page for details.
March 28, 2005 NP.21.41
Normal Procedures -Amplified Procedures
Climb and Cruise Procedure [AD 2002-19-52 and AD 2002-24-51]
Complete the After Takeoff Checklist before starting the Climb and Cruise Procedure.
Pilot Flying Pilot Monitoring
If the center tank fuel pump switches were OFF for takeoff and the center tank contains more than 500 kilograms, position both center tank fuel pump switches ON above 10,000 feet or after the pitch attitude has been reduced to begin acceleration to a climb speed of 250 knots or greater.
During climb, position both center tank fuel pump switches OFF when center tank fuel quantity reaches approximately 500 kilograms.
At or above 10,000 feet MSL, set the LANDING light switches to OFF.
Set the passenger signs as needed.
At transition altitude, set and crosscheck the altimeters to standard.
When established in a level attitude at cruise, if the center tank contains more than 500 kilograms and the center tank fuel pump switches are OFF, position the center tank fuel pump switches ON again. Position both center tank fuel pump switches OFF when center tank fuel quantity reaches approximately 500 kilograms.
During the last hour of cruise on all ETOPS flights, do a Fuel Crossfeed Valve check.
Before the top of descent, modify the active route as needed for the arrival and approach.
Copyright . The Boeing Company. See title page for details.
NP.21.42 March 28, 2005
Normal Procedures -Amplified Procedures
Climb and Cruise Procedure [Alternate Method of Compliance (AMOC) to AD 2002-24-51]
Complete the After Takeoff Checklist before starting the Climb and Cruise Procedure.
Pilot Flying Pilot Monitoring
If the center tank fuel pump switches were OFF for takeoff and the center tank contains more than 950 kilograms, position both center tank fuel pump switches ON above 10,000 feet or after the pitch attitude has been reduced to begin acceleration to a climb speed of 250 knots or greater.
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本文链接地址：737NG机组操作手册Flight Crew Operations Manual FCOM 1(59)
