Honeywell BENDIX/KING KAP 140 Maintenance Manual page 98

Flight control system
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ERR# TEXT MESSAGE(S)
DESCRIPTION OF ERROR
53
Acc mon failed clutch interrupt
The accelerometer monitor did not disengage the pitch, roll, or trim clutch
during PFT. Probable fault in clutch engagement logic. This error code is not
present in software flavors --0105, --0106, and --0201. Pitch Axis operation
is disallowed.
54
Trim mon failed clutch interrupt
During preflight test, the trim clutch was not disabled by a trim monitor failure.
This preflight test step fails the trim monitor and checks that the trim clutch
is disabled. Manual Electric Trim and Autotrim operation is disallowed.
55
GPS armed w/ other snsr req
An error has occurred in the mode logic.
56
LOC armed w/ other snsr req
An error has occurred in the mode logic.
57
VOR armed w/ other snsr req
An error has occurred in the mode logic.
58
Lat armed illegal xsit mode
An error has occurred in the mode logic.
59
Lat armed illegal mode detail
An error has occurred in the mode logic.
60
GPS tracked w/ other snsr req
An error has occurred in the mode logic.
61
LOC tracked w/ other snsr req
An error has occurred in the mode logic.
62
VOR tracked w/ other snsr req
An error has occurred in the mode logic.
63
GPS tracked w/ GPS track req
An error has occurred in the mode logic.
64
LOC tracked w/ LOC track req
An error has occurred in the mode logic.
65
VOR tracked w/ VOR track req
An error has occurred in the mode logic.
Revision 2, Dec/2002
CS:15574F02.IDU
BENDIX/KING
KAP 140
POSSIBLE FAILED UNIT(S)
KC 140, KS 270C, KS 271C, KS 272C, harness
wiring
KC 140, KS 272C, harness wiring
KC 140
KC 140
KC 140
KC 140
KC 140
KC 140
KC 140
KC 140
KC 140
KC 140
KC 140
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