BENDIX/KING
KAP 140
Page 5--15
Revision 2, Dec/2002
CS:15574F02.IDU
ERR# TEXT MESSAGE(S) POSSIBLE FAILED UNIT(S)
DESCRIPTION OF ERROR
242 Acc Mon trim clutch eng failed KC 140, KS 272C, harness wiring
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 KC 140, KS 271C, harness wiring
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 KC 140, KS 270C, harness wiring
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 KC 140, KS 272C, harness wiring
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 KC 140
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 KC 140
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 KC 140
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 KC 140
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 KC 140
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.
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