Honeywell CAS-100 Maintenance Manual page 156

Collision avoidance system
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CAS-100 COLLISION AVOIDANCE SYSTEM
Table 1004. System and Input Faults
Front Panel Text
Top Ant Fail
Top Ant E1
Top Ant E2
Top Ant E3
Top Ant E4
Bott Ant Fail
Bott Ant E1
Bott Ant E2
Bott Ant E3
Bott Ant E4
Radio Alt 1
Radio Alt 2
Radio Alt 1
Radio Alt 2
Transponder 1
Transponder 2
Roll Att Data
Pitch Att Data
Heading Data
TA/VSI 1
TA/VSI 2
RA Display 1
RA Display 2
CMC Bus
CMC Bus
ATC Ctl Panel
ATC Ctl Panel
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
MAINTENANCE MANUAL
Fault Description
1. TX Cal Delta 24 or 31 Top (Antenna Failure)
1.1 Top Antenna Element 1 failed
1.2 Top Antenna Element 2 failed
1.3 Top Antenna Element 3 failed
1.4 Top Antenna Element 4 failed
2. TX Cal Delta 24 or 31 Bot (Antenna Failure)
2.1 Bottom Antenna Element 1 failed
2.2 Bottom Antenna Element 2 failed
2.3 Bottom Antenna Element 3 failed
2.4 Bottom Antenna Element 4 failed
3. Radio Altitude 1 (for A330, A340, and Boeing)
4. Radio Altitude 2 (for A330, A340, and Boeing)
3a. Radio Altitude 1 (for A320)
4a. Radio Altitude 2 (for A320)
5. Mode-S Transponder 1
6. Mode-S Transponder 2
7. Roll Angle
8. Pitch Angle
9. Magnetic Heading
10. TA/VSI 1
11. TA/VSI 2
12. RA/VSI 1
13. RA/VSI 2
14. CFDIU (for A320)
14. CMC (for A330, A340, and Boeing)
15. Mode-S Control Panel (for A330 and A340)
15.1 Mode-S Control Panel (for A320 and Boeing)
34-45-47
Page 1015
1 Dec 2003

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