User Manual

system components 523-0 809018
Table 2-2. ECU Installation Strapping Data. - Continued
Description Values Recommend (Function U sing Setting)
Default Altitude Limit B Range 0 - 12 7 decimal Recommend: 99 (9,900 ft) (TCAS)
Aural Files Used 1 = Aural Files Used
0 = Aural Files Not Used
(TCAS)
Aural Advisory Discrete Delay 1 = Add delay to Aural Advisory discrete
output
0=Nodelay
(TCAS)
In Air Volume 000 = 16 dBm 40 mW
001 = 13 dBm 20 mW
010 = 10 dBm 10 mW
011=7dBm5mW
100 = 4 dBm 2 .5 mW
101 = 1 dBm 1.25 mW
110 = -2 dBm 0.625 mW
111 = 19 dBm 80 mW
NOTE
This value is o nly applicable if
using the TSS’s 600 ohm output.
Audio power output tolerance is
+35%/-25% of power outputs show
in Watts (TCAS)
On Ground Volume 000 = Match “In Air Volume”
001 = 13 dBm 20 mW
010 = 10 dBm 10 mW
011=7dBm5mW
100 = 4 dBm 2 .5 mW
101 = 1 dBm 1.25 mW
110 = -2 dBm 0.625 mW
111 = 19 dBm 80 mW
NOTE
This value is o nly applicable if
using the TSS’s 600 ohm output.
Audio power output tolerance is
+35%/-25% of power outputs show
in Watts (TCAS)
Maximum Climb Altitude Range 0 - 31 decima l (TCAS)
Aircraft Category (maximum takeoff
weight)
0000 = Not available
0001 = < 15,500 lbs
0010 = 15,500 to 75,000
0011 = 75,000 to 300,000
0100 = High Vortex Large
0101 = > 300,000
0110 = High Performance
0111 = Rotorcraft
1000 through 1111 = Reserved for Set
“B”
(ADS-B)
Maximum Cruising Airspeed 000 = Not available
001 = 0 to 75 knots
010 = 75 to 150 knots
011 = 150 to 300 knots
100 = 300 to 600 knots
101 = 600 to 1200 knots
110 = more than 1200 knots
111 = not used
(ADS-B)
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