Radio Altitude Comparator - Honeywell SPZ-8000 Maintenance Manual

Digital automatic flight control system for gulfstream iv
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A miscompare condition occurs when one of the above parameters
deviate greater than the allowed threshold.
When a miscompare
is detected, the FGC reversion will be dependent upon whether
the
IRS
monitor resident in the
AHRS or IRS 3 is
valid.
With
the
IRS
monitor invalid, all
FD
modes
will
be dropped,
the
AP
and YD will disengage, and the
IRS
miscompare will be
annunciated.
A heading miscompare with the
IRS
monitor invalid
will cause the aircraft to revert to wings level from
HDG hold
and annunciate the IRS
miscompare.
With the
IRS
monitor valid, a miscompare in the FGC
will
cause
the FGC to look
at the miscompare
discretes
from the
IRS
monitor.
The
IRS
monitor compares the parameters listed below
between
IRS 1
and
IRS 2.
Parameter
Allowed Error Threshold
Pitch/Roll
Pitch Rate
Yaw Rate
0.3°/sec +Avg
Rate /32
Roll Rate
Normal Accel
Lateral Accel
0.05 g + Avg Delta Accel /32
Fore-Aft Accel
Heading
N/A
A miscompare condition in the
IRS
monitor occurs whenever the
above parameters deviate greater than the allowed threshold
between the
IRS
monitor and
IRS
1 or
the
IRS
monitor
and
IRS 2.
The IRS
monitor will set the appropriate discrete to the FGC
(either
IRS 1
miscompare or
IRS 2
miscompare).
The FGC does not use the miscompare discretes from the IRS
monitor until the FGC has detected a miscompare.
At that point
the FGC uses the
IRS
monitor as a voter by looking at the
miscompare discretes.
The FGC will stop using data from the
IRS
with which the
IRS
monitor has miscompared and EICAS will
annunciate "FGC NOT
USING IRS (X)".
3.
B.
(6)
(c)
Radio Altitude Comparator
The parameter compared by the
FGC is
shown below.
Parameter
Allowed Error Threshold
Radio Alt
5 ft + ALT Avg /8
22-14-00
Page
298.86
Apr 15/93
USe
or
disclosure
of
information
on
this
page
is subject
to
the
restrictions
on
the
title
page
of
this
document,

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