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500 SERIES INSTALLATION MANUAL Page 4-1
P/N 190-00181-02 Rev G
4. SYSTEM INTERCONNECTS
4.1 PIN FUNCTION LIST
P5001
View of J5001 connector from back of unit
1 2 3 4 5 6 7 8 9 1011121314151617181920
21 22 23 24 25 26 27
28 29
30 31 32 33 34 35 36 37 38 39
40
41 42
43 44 45 46 47 48 49 50 51 52 53 54 55 56
57
58 59
60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78
Pin Pin Name I/O
1 VLOC ANNUNCIATE Out
2 GPS ANNUNCIATE Out
3 WAYPOINT ANNUNCIATE Out
4 TERMINAL ANNUNCIATE Out
5 APPROACH ANNUNCIATE Out
6 MESSAGE ANNUNCIATE Out
7 OBS ANNUNCIATE Out
8 SPARE ANNUNCIATE Out
9 INTEGRITY ANNUNCIATE Out
10 ANNUNCIATE D Out
11 ANNUNCIATE E Out
12 ALTITUDE ALARM ANNUNCIATE (Not implemented at time of publication) Out
13 ANNUNCIATE F (Not implemented at time of publication) Out
14 ILS/GPS APPROACH Out
15 AIRCRAFT POWER 2* In
16 TIME MARK OUT Out
17 MAIN LATERAL SUPERFLAG Out
18 MAIN VERTICAL SUPERFLAG Out
19 AIRCRAFT POWER 1 In
20 AIRCRAFT POWER 1 In
21 MAIN +LEFT Out
22 MAIN +RIGHT (2.5V COMMON) Out
23 MAIN LATERAL +FLAG Out
24 MAIN LATERAL -FLAG (2.5V COMMON) Out
25 MAIN +TO Out
26 MAIN +FROM (2.5V COMMON) Out
27 MAIN +UP Out
28 MAIN +DOWN (2.5V COMMON) Out
29 MAIN VERTICAL +FLAG Out
30 MAIN VERTICAL -FLAG (2.5V COMMON) Out
31 MAIN OBS ROTOR C Out
32 MAIN OBS ROTOR H (GROUND) Out
33 MAIN OBS STATOR D In
34 MAIN OBS STATOR E (2.5V COMMON OBS) Out
35 MAIN OBS STATOR F In
36 MAIN OBS STATOR G (2.5V COMMON OBS) Out
* Applies only to GNS 530 part numbers 011-00550-30, GNS 530A 011-00835-10, and GPS 500 part
number 011-00562-10. For applications requiring secondary or alternate power bus input.