Honeywell CAS-100 Maintenance Manual page 171

Collision avoidance system
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Discrete Pin
Number
RMP5K
Air/Ground 1
RMP6D
Performance Limit
RMP7E
TA Display No. 1 Status
RMP7J
TA Display No. 2 Status
RMP14C
RA Display No. 1 Status
RMP13E
RA Display No. 2 Status
RMP13F
Landing Gear
NOTE: Advisory Inhibit and TCAS Mode Data is shown in Table 1009.
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
MAINTENANCE MANUAL
CAS-100 COLLISION AVOIDANCE SYSTEM
Table 1008. Discrete Pin Numbers (cont)
Display Text
Discrete Description
The Air/Ground Discrete Input for the Air/Ground relay.
The normal failure mode is the airborne condition.
The following applies:
RMP5K
RTP5J
1
1
a/c on ground, don't inhibit ATCRBS replies
1
0
a/c on ground, don't inhibit ATCRBS replies
0
1
a/c on ground, inhibit ATCRBS replies
0
1
a/c airborne, don't inhibit ATCRBS replies
Where 0 = Open
1 = Ground
The performance limit shows to TCAS when the
aircraft can no longer get a 1500 feet per minute climb.
When the input is GROUND the performance is not
limited. When the input is OPEN the climb is limited if
the altitude of the aircraft is above the value set by the
Altitude Limit Program (See below).
Limit Input
RMP6D
Relative Altitude
Yes
Open
Below
Yes
Open
Above
No
Gnd
Below
No
Gnd
Above
The TA Display Status input are connected to their
related Traffic Display Status output (valid).
If any of the Display Status discretes are not
necessary they must be attached to ground as
necessary for the installation.
The RA Display 1 and 2 Status discretes indicate the
validity of the resolution displays. They are connected
to their respective RA Display Status output (valid).
This pin shows the position of the landing gear. The
usual mode is the RETRACTED position.
Where 0 = Gear Retracted = Open
1 = Gear Extended = Ground
34-45-47
Definition
Climb Limited
No
Yes
No
No
Page 1030
1 Dec 2003

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