KSD100_CTRL_PANEL_RS232_RX
KSD100_CTRL_PANEL_RS232_TX
KSD100_CTRL_PANEL_PWR_15VDC
KSD100_CTRL_PANEL_PWR_RTN
NOTES:
1
2
3
4
5
89000109-002
Rev 2
For Use in Non-Certified Aircraft
KSD 100
J1
ADAHRS1_A429_RX_A
36
ADAHRS1_A429_RX_B
35
ADAHRS1_A429_TX_A
38
37
ADAHRS1_A429_TX_B
J2
77
76
5
78
59
APM_PWR_3P3VDC
69
APM_PWR_RTN
70
APM_DATA_CS_N
67
APM_DATA_MOSI
65
APM_DATA_MISO
64
APM_CLK
66
APM_WP_N
68
Single Conductor Wire
x
All wires shall be 22 AWG unless otherwise noted power wires
x
Wiring shall meet AS22759/16/XX/Y (Where XX is gauge and Y is color)
Twisted Shielded Pair/Triplet and Shielded Single Wire
x
All wires shall conform to ANSI/NEMA WC 27500
x
Do not remove any wiring between other active aircraft systems. Leave those systems installed as they are.
All shield grounds are to be grounded at the closest grounding point to their respective connectors . This includes connector grounding points.
For metallic backshells with grounding capability, ground shield directly to the backshell.
Drawing Symbols:
- Single
Over Braid will be installed between all wires from J2 of the KSD 100
Figure B-6 KSD 100EXP LRU Interconnect Diagram
© Honeywell International Inc. Do not copy without express permission of Honeywell.
KG 71
J71
40
A429_TX0_A
41
A429_TX0_B
34
A429_RX0_A
35
A429_RX0_B
KCP 100
J1
2
RS232_TX_OUT
3
RS232_RX_IN
9
15VDC_PWR_IN
8
15VDC_PWR_RTN
E6 (Red)
APM_PWR_3P3VDC
E7 (Black)
APM_PWR_RTN
E4 (Green)
APM_CS_N
wiring is to be contained
APM_SI
E2 (Blue)
E1 (Orange)
APM_SO
in P2 unit backshell
E3 (Yellow)
APM_SCLK
E5 (White)
APM_WP_N
-
Shielded Twisted Pair
and P1 of the KCP 100
. Terminate Braid within connector backshells.
xVue Touch Installation Manual
Page B-6
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