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Honeywell BENDIX/KING KAP 140 - Page 96

Honeywell BENDIX/KING KAP 140
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BENDIX/KING
KAP 140
Page 5--6
Revision 2, Dec/2002
CS:15574F02.IDU
ERR# TEXT MESSAGE(S) POSSIBLE FAILED UNIT(S)
DESCRIPTION OF ERROR
39 Trim mon 4 -- auto failed KC 140, KS 270C, KS 272C, harness wiring
Preflight test failed due to improper response of the runaway/autotrim monitor.
The monitor did not detect (i.e. fail) a trim down drive with a valid MET UP condition. This
indicates a probable failure in the trim runaway/autotrim monitor of the flight computer.
Manual Electric Trim and Autotrim operation is disallowed.
40 Trim mon 5 -- auto failed KC 140, KS 270C, KS 272C, harness wiring
Preflight test failed due to improper response of the runaway/autotrim monitor.
The monitor did not detect a trim up drive with a trim DN command. This indicates
a probable failure in the trim runaway/autotrim monitor of the flight computer.
Manual Electric Trim and Autotrim operation is disallowed.
41 Trim mon 6 -- auto failed KC 140, KS 270C, KS 272C, harness wiring
Preflight test failed due to improper response of the runaway/autotrim monitor.
The monitor failed for a valid trim down drive with a trim down command. This
indicates a probable failure in the trim runaway/autotrim monitor of the flight
computer. Manual Electric Trim and Autotrim operation is disallowed.
42 Trim mon 7 -- auto failed KC 140, KS 270C, KS 272C, harness wiring
Preflight test failed due to improper response of the runaway/autotrim monitor.
The monitor failed for a null trim drive condition. This indicates a probable
failure in the trim runaway/autotrim monitor of the flight computer. Manual
Electric Trim and Autotrim operation is disallowed.
43 Trim mon 0 -- MET failed KC 140
Preflight test failed due to improper response of the MET latent switch monitor.
This monitor was failed prior to beginning the preflight test sequence. This
indicates a probable failure in the MET monitor of the flight computer. Manual
Electric Trim and Autotrim operation is disallowed.
44 Trim mon 3 -- MET failed KC 140
Preflight test failed due to improper response of the MET latent switch monitor.
The monitor did not detect (i.e. fail) a MET UP switch without an ARM switch.
This indicates a probable failure in the MET monitor of the flight computer.
Manual Electric Trim and Autotrim operation is disallowed.
45 Trim mon 4 -- MET failed KC 140
Preflight test failed due to improper response of the MET latent switch monitor.
The monitor failed for a valid MET UP condition. This indicates a probable
failure in the MET monitor of the flight computer. Manual Electric Trim and
Autotrim operation is disallowed.

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