EasyManua.ls Logo

Boeing 737-800 - AFS Failures; Flight Director Display

Boeing 737-800
1636 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
737 Flight Crew Operations Manual
Automatic Flight -
System Description
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-866-EGP 4.20.3
loss of electrical power or a sensor input which prevents proper
operation of the engaged A/P and mode
loss of respective hydraulic system pressure.
Note: Loss of the system A engine-driven hydraulic pump, and a heavy demand
on system A, may cause A/P A to disengage.
AFS Failures
Power interruption or loss may cause disengagement of the AFDS and/or A/T.
Re–engagement is possible after power is restored.
Dual channel A/P operation is possible only when two generators are powering the
busses.
Two independent radio altimeters provide radio altitude to the respective FCCs.
With a radio altimeter inoperative, the autopilot will disconnect two seconds after
LOC and GS capture.
Flight Director Display
Turning a F/D switch ON displays command bars on the respective pilot’s attitude
indicator if command pitch and roll modes are engaged. If command pitch and roll
modes are not engaged, the F/D command bars do not appear. The F/Ds can be
operated with or without the A/P and A/T. F/D command modes can be used with
an A/P engaged in CWS.
F/D commands operate in the same command modes as the A/P except:
the takeoff mode is a F/D only mode
dual F/D guidance is available for single engine operation
the F/D has no landing flare capability. F/D command bars retract from
view at approximately 50 feet RA on an ILS approach.
Normally, FCC A drives the captain’s command bars and FCC B drives the first
officers command bars. With both F/D switches ON, the logic for both pilots’
F/D modes is controlled by the master FCC, and both FMA displays show the
same mode status.
The master FCC is indicated by illumination of the respective master (MA) F/D
indicator light. The master FCC is determined as follows:
with neither A/P engaged in CMD, the FCC for the first F/D turned on is
the master
with one or both A/Ps engaged in CMD, the FCC for the first A/P in
CMD is the master FCC, regardless of which F/D is turned on first.
September 15, 2016

Table of Contents

Related product manuals