CAUTION: To avoid the possibility of shoulder harness buckles snapping back and pulling or damaging circuit breakers, hold both straps before releasing and then allow straps to retract slowly to the stowed position.
Copyright . The Boeing Company. See title page for details.
NP.20.26 June 4, 2004
Normal Procedures -Amplified Procedures
Takeoff Flap Retraction Speed Schedule
T/O FLAPS SELECT FLAPS At & below 117,000 Lbs (53,070 Kgs) Above: 117,000 Lbs (53,070 Kgs) up to 138,500 Lbs (62,823 Kgs) Above 138,500 Lbs (62,823 Kgs)
15 5 1 UP V2 + 15 170/F 190/F V2 + 15 180/F 200/F V2 + 15 190/F 210/F
5 1 UP V2 + 15 190/F V2 + 15 200/F V2 + 15 210/F
1 UP 190/F 200/F 210/F
. “F” – Minimum flap retraction speed, existing flap. Note: Limit bank angle to 15 degrees until reaching V2 + 15.
Normal Procedures -Amplified Procedures
Climb and Cruise Procedure
PILOT FLYING PILOT NOT FLYING
Position landing lights OFF passing through 10,000 feet.
Set altimeters to standard at transition altitude.
Approaching selected FMC cruise altitude, verify level off and proper mode/N1 limit annunciation.
Position center tank fuel pump switches OFF when both pump LOW PRESSURE lights illuminate.
During the last hour of cruise on all extended range (more than one hour from an adequate airport) flights, perform the Fuel Crossfeed Valve Check.
Set MCP altitude selector for descent. Prior to top of descent, select and verify the planned arrival procedure on the FMC.
At top of descent point observe descent initiated and verify proper mode annunciation.
Note: If a center tank LOW PRESSURE light(s) illuminates during takeoff or initial climb, the center tank pump(s) may remain on until the climb attitude is reduced and the light(s) extinguishes or workload allows for the pump(s) to be positioned OFF.
Note: When established in a level attitude at cruise, if the center tank contains usable fuel and the center tank pump switches are off, the center tank pump switches should be positioned ON again. If the center tank contains more than 1000 lbs/453 kgs, the center tank pump switches must be turned ON. Verify the LOW PRESSURE lights extinguish and position both switches OFF when both LOW PRESSURE lights illuminate.
Copyright . The Boeing Company. See title page for details.
NP.20.28 June 4, 2004
Normal Procedures -Amplified Procedures 737 Operations Manual
Descent and Approach Procedure
PILOT FLYING PILOT NOT FLYING
Check and set VREF and approach speeds as required.
Set anti–ice as required.
Verify pressurization is set for destination airport elevation and system operating normally.
Set AUTOBRAKE select switch to desired brake setting.
Set and crosscheck altimeters at transition level.
Set and crosscheck course selection and DH REF/radio altimeters as required for approach.
Set and verify ADF and VHF NAV radios for approach.
Position inboard landing lights ON passing through 10,000 feet.
Call “DESCENT–APPROACH CHECKLIST.” Accomplish the DESCENT – APPROACH checklist.
Announce “FLAPS __” according to flap speed schedule. Position FLAP lever as directed and monitor flap and slat extension. Accomplish standard callouts.
Approaching selected FMC altitude verify level off and mode annunciation.
Copyright . The Boeing Company. See title page for details.
June 4, 2004 NP.20.29
Normal Procedures -Amplified Procedures
Approach Procedure
Using flaps as speedbrakes is not recommended.
The following procedures are used for flap extension:
.
Select flaps 1 when decelerating through the flaps–up maneuvering
speed, displayed on the speed tape as a green “0.”
.
When appropriate, select the next flap position and then set the
airspeed cursor to that flap maneuver speed.
Note: Flap maneuver speeds provide approximately 15 to 20 knots
above the minimum maneuvering speed for each flap setting.
Note: If performance requires use of flaps 15 for landing, place the GROUND PROXIMITY flap inhibit switch to FLAP INHIBIT. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737-300机组操作手册Flight Crew Operations Manual FCOM 1(41)
