Honeywell BENDIX/KING KAP 140 Maintenance Manual page 105

ERR# TEXT MESSAGE(S)
DESCRIPTION OF ERROR
242 Acc Mon trim clutch eng failed
An attempt to engage the trim clutch during PFT failed. No current was sensed
in the trim clutch. This error code is not present in software flavors --0103,
and --0104. Pitch Axis operation will be disallowed.
243 Acc Mon roll clutch diseng failed
The accelerometer monitor did not disengage the roll clutch during PFT. Probable
fault in clutch engagement logic. This error code is not present in software
flavors --0103, and --0104. Pitch Axis operation will be disallowed.
244 Acc Mon pitch clutch diseng failed
The accelerometer monitor did not disengage the pitch clutch during PFT. Probable
fault in clutch engagement logic. This error code is not present in software
flavors --0103, and --0104. Pitch Axis operation will be disallowed.
245 Acc Mon trim clutch diseng failed
The accelerometer monitor did not disengage the trim clutch during PFT. Probable
fault in clutch engagement logic. This error code is not present in software
flavors --0103, and --0104. Pitch Axis operation will be disallowed.
246 Acc HP fails self test
PFT failed due to insufficient response from high passed acceleration value
during self test The input should have been saturated, but was below the minimum
saturation value. This error code is not present in software flavors --0103,
--0104, and --0105. Pitch Axis operation will be disallowed.
247 Acc HP does not settle
PFT failed due to the high passed acceleration value not settling in the flight
computer. This error code is not present in software flavors --0103, --0104,
and --0105. Pitch Axis operation will be disallowed.
248 Acc HP has high gain
PFT failed due to the gain of the high passed acceleration being too high in
the flight computer. This error code is not present in software flavors --0103,
--0104, and --0105. Pitch Axis operation will be disallowed.
249 Acc HP has low gain
PFT failed due to the gain of the high passed acceleration being too low in
the flight computer. This error code is not present in software flavors --0103,
--0104, and --0105. Pitch Axis operation will be disallowed.
250 Acc HP has short time constant
PFT failed due to the time constant of the high passed acceleration being too
short in the flight computer. This error code is not present in software flavors
--0103, --0104, and --0105. Pitch Axis operation will be disallowed.
Revision 2, Dec/2002
CS:15574F02.IDU
BENDIX/KING
KAP 140
POSSIBLE FAILED UNIT(S)
KC 140, KS 272C, harness wiring
KC 140, KS 271C, harness wiring
KC 140, KS 270C, harness wiring
KC 140, KS 272C, harness wiring
KC 140
KC 140
KC 140
KC 140
KC 140
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