Honeywell International Inc. 9PGTPA-100A Manuale Utente
MAINTENANCE MANUAL
CAS-100 COLLISION AVOIDANCE SYSTEM
Page 2105
1 Dec 2003
34-45-4
7
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NOTES:
1.
PIN TO RBP-7K = DISPLAY TA/RA/PROXIMITY TRAFFIC (DURING RA OR TA ONLY).
OPEN = DISPLAY ALL TRAFFIC (FULL TIME).
OPEN = DISPLAY ALL TRAFFIC (FULL TIME).
2.
OPEN = SYSTEM GOES TO TA ONLY MODE (RAs ARE INHIBITED) WHEN THE AIRCRAFT
IS ON THE GROUND.
PIN TO RBP-7K = SYSTEM GOES TO STANDBY WHEN THE AIRCRAFT IS ON THE
GROUND.
IS ON THE GROUND.
PIN TO RBP-7K = SYSTEM GOES TO STANDBY WHEN THE AIRCRAFT IS ON THE
GROUND.
3.
1500 FPM PERFORMANCE LIMIT IS DETERMINED BY: CLIMB INHIBIT NO. 1 AND NO. 2 =
LOW OR CLIMB INHIBIT NO. 3 AND NO. 4 = LOW OR THE AIRCRAFT IS ABOVE THAT OF
THE ALTITUDE LIMIT PROGRAM PINS.
2500 FPM PERFORMANCE LIMIT IS DETERMINED BY: INCREASE CLIMB INHIBIT NO. 1
AND NO. 2 OR NO. 3 AND NO. 4 = LOW
PERFORMANCE LIMITS ARE DETERMINED BY THE FOLLOWING INPUT:
LOW OR CLIMB INHIBIT NO. 3 AND NO. 4 = LOW OR THE AIRCRAFT IS ABOVE THAT OF
THE ALTITUDE LIMIT PROGRAM PINS.
2500 FPM PERFORMANCE LIMIT IS DETERMINED BY: INCREASE CLIMB INHIBIT NO. 1
AND NO. 2 OR NO. 3 AND NO. 4 = LOW
PERFORMANCE LIMITS ARE DETERMINED BY THE FOLLOWING INPUT:
CLIMB INHIBIT
INCREASED CLIMB INHIBIT
PERFORMANCE LIMIT DISCRETE
FLIGHT/PERFORMANCE MANAGEMENT COMPUTER
AIRCRAFT ALTITUDE LIMIT PROGRAM PINS
INCREASED CLIMB INHIBIT
PERFORMANCE LIMIT DISCRETE
FLIGHT/PERFORMANCE MANAGEMENT COMPUTER
AIRCRAFT ALTITUDE LIMIT PROGRAM PINS
IF A 2500 FPM CLIMB RATE IS MORE THAN THE CAPABILITY OF THE AIRCRAFT, EITHER
INCREASE CLIMB INHIBIT NO. 1 AND NO. 2 OR NO. 3 OR NO. 4 MUST BE HARDWIRED TO
GROUND.
IF AN AIRCRAFT CONFIGURATION, FOR EXAMPLE FLAPS OR GEAR EXTENDED,
DECREASES THE AIRCRAFT PERFORMANCE BELOW 2500 FPM OR 1500 FPM, AN
ISOLATED SWITCHED GROUND DISCRETE, SHOWING THAT ACTIVE CONFIGURATION
MUST BE CONNECTED TO ONE INHIBIT DISCRETE. FOR EXAMPLE, NO. 1 AND NO. 3.
THE REMAINING INHIBIT DISCRETE INPUT, FOR EXAMPLE, NO. 2 OR NO. 4 MUST BE
HARDWIRED TO GROUND.
IF AN AIRCRAFT CAN KEEP 1500 FPM CLIMB RATE REGARDLESS OF THE AIRCRAFT
CONFIGURATION, THE "CLIMB INHIBIT" DISCRETES ARE NOT CONNECTED.
IF THE AIRCRAFT CAN KEEP 2500 FPM CLIMB RATE REGARDLESS OF THE AIRCRAFT
CONFIGURATION, THE "INCREASED CLIMB INHIBIT" DISCRETES ARE NOT CONNECTED.
INCREASE CLIMB INHIBIT NO. 1 AND NO. 2 OR NO. 3 OR NO. 4 MUST BE HARDWIRED TO
GROUND.
IF AN AIRCRAFT CONFIGURATION, FOR EXAMPLE FLAPS OR GEAR EXTENDED,
DECREASES THE AIRCRAFT PERFORMANCE BELOW 2500 FPM OR 1500 FPM, AN
ISOLATED SWITCHED GROUND DISCRETE, SHOWING THAT ACTIVE CONFIGURATION
MUST BE CONNECTED TO ONE INHIBIT DISCRETE. FOR EXAMPLE, NO. 1 AND NO. 3.
THE REMAINING INHIBIT DISCRETE INPUT, FOR EXAMPLE, NO. 2 OR NO. 4 MUST BE
HARDWIRED TO GROUND.
IF AN AIRCRAFT CAN KEEP 1500 FPM CLIMB RATE REGARDLESS OF THE AIRCRAFT
CONFIGURATION, THE "CLIMB INHIBIT" DISCRETES ARE NOT CONNECTED.
IF THE AIRCRAFT CAN KEEP 2500 FPM CLIMB RATE REGARDLESS OF THE AIRCRAFT
CONFIGURATION, THE "INCREASED CLIMB INHIBIT" DISCRETES ARE NOT CONNECTED.
4.
SHOWS AIRCRAFT STATUS: AIRBORNE OR GROUND.
5.
STRAP LOGIC: OPEN PINS ARE SET. THE PIN JUMPERED TO RBP-7K ARE NOT
SELECTED.
SELECTED.
6.
THIS PIN SUPPLIES A GROUND WHEN XPNDR CTL PANEL IS IN A TCAS OR TEST MODE
(TA ONLY, TA/RA) WHICH SETS THE PPI DISPLAY.
(TA ONLY, TA/RA) WHICH SETS THE PPI DISPLAY.
CAS-100 Interwiring Diagram
Figure 2015 (Sheet 11 of 16)