Copyright . The Boeing Company. See title page for details.
NP.20.30 June 4, 2004
Normal Procedures -Amplified Procedures 737 Operations Manual
Landing Procedure
PILOT FLYING PILOT NOT FLYING
When on localizer intercept heading, verify ILS tuned and identified, LOC and G/S pointer displayed, arm APP mode and engage the second autopilot. Set transponder mode selector to desired TCAS mode. (TCAS equipped airplanes.)
Verify mode annunciation.
At localizer capture, verify proper mode annunciation and set appropriate heading. Verify proper mode annunciation.
At glide slope “alive,” announce “GEAR DOWN,” “FLAPS 15." Arm the speed brakes and check green light illuminated. Call “LANDING CHECKLIST DOWN TO FLAPS.” Position landing gear lever DN, and FLAP lever to the 15 detent. Position engine start switch to CONT. Check RECALL.
Accomplish the LANDING checklist down to flaps. State “HOLDING AT FLAPS.”
At glide slope capture, verify proper mode annunciation, check N1 cursor at the go–around limit and set missed approach altitude.
Call “FLAPS __” as required for landing. Set MCP speed selector at VREF + 5 kts. Position FLAP lever as directed.
At final approach fix/OM, verify crossing altitude.
Call “COMPLETE THE LANDING CHECKLIST.” Complete the LANDING checklist.
Monitor approach progress and guard the controls. At 500 feet AGL, verify FLARE is armed. At approximately 50 feet AGL, verify FLARE is engaged. Ensure the autothrottle retards the thrust levers to idle by touchdown.
Copyright . The Boeing Company. See title page for details.
June 4, 2004 NP.20.31
Normal Procedures -Amplified Procedures 737 Operations Manual
Go–Around Procedure
PILOT FLYING PILOT NOT FLYING
Push TO/GA switch. Call “FLAPS 15.” If full GA thrust is required, push TO/GA switch again after reduced GA thrust is established. Monitor N1 indication. Position FLAP lever to 15 and monitor flap retraction.
Confirm rotation to go–around attitude and monitor autopilot.
Verify mode annunciation.
When positive rate of climb is indicated, call “GEAR UP” and monitor acceleration. Verify positive rate of climb. Position landing gear lever UP.
Check flight instrument indications (MCP speed window blanks.)
Call “TUNE RADIOS FOR MISSED APPROACH.” Tune radios as directed.
Above 400 feet, select appropriate roll mode and verify proper mode annunciation. Observe mode annunciation.
Retract flaps on flap speed schedule. Position FLAP lever as directed and monitor flaps and slats retraction.
Verify airplane levels off at selected altitude and maintains flap maneuvering speed.
Call “AFTER TAKEOFF CHECKLIST.” Accomplish the AFTER TAKEOFF checklist.
Copyright . The Boeing Company. See title page for details.
NP.20.32 June 4, 2004
Normal Procedures -Amplified Procedures
Landing Roll Procedure
PILOT FLYING PILOT NOT FLYING
Ensure thrust levers at idle.
Disengage autopilot and control airplane manually. Verify autothrottle disengages automatically. Verify autothrottle is disengaged.
Verify SPEED BRAKE lever (ground spoilers) - UP. Verify SPEED BRAKE lever UP. Call out “SPEEDBRAKES UP.” If SPEED BRAKE lever is not UP, call “SPEEDBRAKES NOT UP.”
Verify proper autobrake operation.
Without delay, raise reverse thrust Monitor engine instruments and
levers to the interlocks, hold light announce any engine limit being
pressure until release, and then approached, exceeded or any other
apply reverse thrust as required. abnormalities.
At 60 knots, reduce reverse thrust to be at IDLE reverse when reaching taxi speed. Call “60 KNOTS.”
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本文鏈接地址：737-300機(jī)組操作手冊(cè)Flight Crew Operations Manual FCOM 1(42)
