Fault Display Format - Honeywell SPZ-8000 Maintenance Manual

Digital automatic flight control system for gulfstream iv
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MAINTENANCE
Honeywell YJW&.
EFIS Fault
Codes
-413/414
-415/416
Cent ro 1ler
Contro 1ler
Fault
Description
None
None
No fault
01
21
Azimuth scanning incorrectly (> 2.5 degrees for > 2 seconds)
01
31
Antenna
Elevation
error
(> 2 degrees
for > 2 seconds)
02
03
Analog
to
Digital
Converter
Failure
02
22
STAB reference
(< 1/2 A/D scale
for
> 2 seconds)
02
32
NAV Computer
High Speed
ARINC429
Failure
03
13
+15
Volts
Failure
(> *1.5
Volts)
03
23
Automatic
Gain Control
Failure
(c
03
33
-1 V or > 9.73
V for
8 seconds)
-15
Volts
Failure
(> *1.5
Volts)
04
16
Magnetron
Voltage
Failure
(< 1500 Volts
min or > 2700 Volts
max)
04
24
Mixer
Current
Failure
05
25
AFC Lock Failure
05
35
AFC Sweep Failure
06
26
Fan Voltage
Abnormal
07
07
07
07
07
07
07
07
07
04
07
14
17
27
34
36
37
30
Digital
Air
Oata Failure
Pulse
Pair
Processor
Failure
Parallel
Altitude
Failure
EPROM Test
Failure
VLSI Test
Failure-Loss
of Video
Ready Interrupt
DADC Altitude
Failure
Analog
Altitude
Failure
-
If
input
is > 60,000
feet
RAM Test
Failure
Nonvolatile
!krnory Failure
~:
When reporting
fault
codes,
it
is essential
that
the type of controller
(e. g.,
-413)
be reported.
Fault Display
Format
Table
8-6
22-14-00
Page
198.97/198.98
Aug
15/91
Use ordisclosure
OfInformation
on this p agek subject 10therestrictions
on thetitle
pageofthis d ocument.

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