Honeywell CAS-100 Maintenance Manual page 159

CAS-100 COLLISION AVOIDANCE SYSTEM
Front Panel Text
PP RMP 6E
PP RMP 6F
PP RMP 6G
PP RMP 6H
PP RMP 6J
PP TARA <3 Intrd
PP Alt Limit Opn
PP RBP 7K
PP RMP 6K
PP RBP 8A
PP RBP 8B
PP RBP 8C
PP RBP 4G
PP RBP 6J
PP RBP 6K
PP RMP 5E
(4) Unit, System, and Input Active Fault Relationship
Table 1006 shows the relation in unit, system, input active faults, and the status on the
display. The asterick (*) shows that the text is selectable.
The display screen shows START TEST or TEST INHIBIT. See Figure 1004. The test
is prevented in specific conditions when the Air/Ground Discrete = Air. When the
Air/Ground Discrete = Ground, START TEST is shown.
To push the Select button when the caret is adjacent to the Start Test selectable item,
causes the Test In Progress screen to come into the view and the test to start.
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
MAINTENANCE MANUAL
Table 1005. Program Pin Faults (cont)
Altitude Limit Prgm, RMP 6E
Altitude Limit Prgm, RMP 6F
Altitude Limit Prgm, RMP 6G
Altitude Limit Prgm, RMP 6H
Altitude Limit Prgm, RMP 6J
TA/RA Display Limit Program Pins set less than 3
Intruders
Altitude Limit Program Pins All Open
Program Pin Common, RBP 7K
Aircraft Alt. Limit Prgm Common, RMP 6K
Audio Level On Ground, RBP 8A
Audio Level On Ground, RBP 8B
Audio Level On Ground, RBP 8C
RA Valid Discrete Disable Program Pin, RBP 4G
Transponder Interface Select, RBP 6J
Rad Alt Interface Select, RBP 6K
ADS-B (Intruder File Enable) Program Pin
Fault Description
34-45-47
Page 1018
1 Dec 2003