737 Flight Crew Operations Manual
Supplementary Procedures -
Automatic Flight
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
SP.4.10 D6-27370-866-EGP
Use LNAV and VNAV or other pitch mode for initial descent. VNAV is required
FAF inbound.
Some approach procedures may require use of VNAV from the IAF onward.
On intercept heading, select or verify LNAV.
Before established on the final
approach course, call “FLAPS ___”
according to the flap extension
schedule or approach speed constraint.
Set the flap lever as directed. Monitor
flaps and slats extension.
Approximately 2 NM before the FAF
and after ALT HOLD or VNAV PTH or
VNAV ALT (as installed) is
annunciated:
• set DA(H) on the MCP
• select or verify VNAV
• select or verify speed intervention
(as installed)
Maximum Lateral Deviation (XTK ERROR): 1 x RNP
Maximum Vertical Deviation - FAF to DA: 75 feet
Monitor RNP PROGRESS page
Approaching glide path, call:
• “GEAR DOWN”
• “FLAPS 15”
Set the landing gear lever to DN.
Verify that the green landing gear
indicator lights are illuminated.
Set the flap lever to 15.
Set the engine start switches to CONT.
Set the speed brake lever to ARM.
Verify that the SPEED BRAKE
ARMED light is illuminated.
Beginning the final approach descent,
call “FLAPS ___” as needed for
landing.
Set the flap lever as directed.
Call “LANDING CHECKLIST.” Do the LANDING checklist.
When at least 300 feet below the
missed approach altitude, set the
missed approach altitude on the MCP.
At the final approach fix, verify the crossing altitude and crosscheck the
altimeters (maximum 100 feet difference between primary altimeters).
Pilot Flying Pilot Monitoring
March 26, 2015
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