Honeywell BendixKing KT 76C Installation Manual page 29

B
Main Connector - J1 Front View
Pin Number.............................. Description
1............................................... Aircraft Ground
2............................................... 14 V Lighting (See Note)
3............................................... 28 V Lighting
4............................................... Suppression In/Out
5............................................... +5 Vdc Test Point
6............................................... -6.2 Vdc Test Point
7............................................... Reserved
8............................................... Gillham Altitude D4
9............................................... Suppression In
10............................................. External Standby
11............................................. 11-33 V dc Aircraft Power
12............................................. 11-33 V dc Aircraft Power
A .............................................. Aircraft Ground
B .............................................. Gillham Altitude B4
C .............................................. Gillham Altitude B2
D .............................................. Gillham Altitude C1
E .............................................. Gillham Altitude B1
F .............................................. External Ident
H .............................................. Gillham Altitude C4
J............................................... Gillham Altitude A4
K .............................................. Gillham Altitude A2
L............................................... Gillham Altitude C2
M.............................................. Gillham Altitude A1
N .............................................. +9 Vdc Test Point
Antenna Connector - J2
Pin Number .................................. Description
1 ................................................... Antenna
Rev 3, May 2004
ATCRBS TRANSPONDER
FIGURE 2-2 KT 76C Interconnect Diagram
(Sheet 3 of 3)
IM 006-10545-0003.dwd
KT 76C
Page 2-13