Table of Contents
Advertisement
Honeywell !!i!r."
For engagement, the A/T requires the following components
valid:
.
FGC 1 or FGC 2
c
IRS 1 or IRS 2 (or both)
.
DADC 1 or DADC 2 (or both)
.
DAU 1A or DAU lB (or both)
.
DAU 2A orDAU
2B (or both)
.
DC 1 orDC
2 (or both)
At least one bus controller
For engagement on the ground, the following additional criteria
must be met:
. The flight director takeoff mode must be selected with the
power lever mounted TO/GA switches.
.
Engine EPRmust be set greater than 1.17 EPR.
The fault warning computer provides a signal to the tone
generator for manual and automatic A/T disconnects.
Additionally, an A/T OFF light is annunciated for each
disengagement. The light is active for 1 second on a pilot-
activated disconnect and flashes steady
for any automatic
disconnect. The steady annunciation can be cancelled by
engaging the A/T or depressing the A/T DISC switch on either
power lever.
In the event of failure of the selected autothrottle, an amber
AT annunciation is displayed in the autothrottle mode
annunciation box (center) on the PFD.
22-14-00
Page 298.187/298.188
Aug 15/91
Use or
disclosure
of
information
on
this
page
is
subject
to
the
restrictions
on
the
title
page
of
this
document.
- Quick Links:
- Spz-8000 System Flow Diagram
Hide quick links:
Advertisement
Table of Contents
