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.
D6-27370-866-EGP SP.4.5
Ensure appropriate navaids (VOR, LOC or NDB) are tuned and
identified before commencing the approach.
Before descent to MDA(H):
At descent point:
Desired V/S .............................................................................. Set
Set desired V/S to descend to MDA(H). Use a V/S that results in
no level flight segment at MDA(H).
Verify V/S mode annunciates.
Pilot Flying Pilot Monitoring
Use LNAV or other roll mode to
intercept the final approach course as
needed.
Approximately 2 NM before the final
approach fix, set the first intermediate
altitude constraint or MDA(H).
If the constraint or MDA(H) does not
end in zero zero (00), for example,
1820, set the MCP ALTITUDE window
to the closet 100 foot increment above
the constraint or MDA(H).
When the current constraint is assured,
set the next constraint before ALT
HOLD is engaged to achieve a
continuous descent path.
Approximately 2 NM before the final
approach fix, call “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.
Pilot Flying Pilot Monitoring
Call "FLAPS ___" as needed for
landing.
Set the flap lever as directed.
September 15, 2016
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