Piper Malibu Meridian PA-46-500TP Airplane Maintenance Manual page 1953

TRANSPONDER
HARNESS
GPS/ENC 2 FUNCTION
DME COMMON
2 X 5 MHZ A
2 X 5 MHZ C
2 X 5 MHZ D
2 X 5 MHZ E
2 X 5 0.1 MHZ A
2 X 5 0.1 MHZ C
2 X 5 0.1 MHZ D
2 X 5 0.1 MHZ E
2 X 5 50 KHZ
1 ALTITUDE A1
2 ALTITUDE A2
3 ALTITUDE A4
4
5 ALTITUDE B1
6 ALTITUDE B2
7 ALTITUDE B4
8
9 ALTITUDE C1
10 ALTITUDE C2
11 ALTITUDE C4
12
13 ALTITUDE D4
14 ALTITUDE COMMON
15
COMM AUDIO HI
COMM AUDIO LO
NAV AUDIO HI
NAV AUDIO LO
MIC AUDIO
MIC KEY
TRANSMIT INTERLOCK
DATA CROSSFILL TRANSMIT
DATA CROSSFILL RECEIVE
GROUND
28V DIM
429 OUT A
429 OUT B
429 IN A
429 IN B
429 OUT A
429 OUT B
429 IN A
429 IN B
GROUND
GROUND
+28 VDC POWER
+28 VDC POWER
GROUND
GROUND
+28 VDC GPS POWER
+28 VDC GPS POWER
9G17
PIPER AIRCRAFT, INC.
PA-46-500TP, MALIBU MERIDIAN
MAINTENANCE MANUAL
GNS 530
NAV/COMM/GPS
TRANSCEIVER
P1001-2 P1002-2 P1006-2
22
14
21
33
20
37
40
42
39
43
69
68
67
66
65
64
63
62
61
70
60
7
19
16
17
6
4
14
41
42
40
39
24
23
48
49
46
47
36
35
21
22
11
12
77
78
19
20
GNS-530 COM/NAV/GPS #2
Figure 2 (Sheet 2 of 3)
DME COMM/NAV 1
HARNESS HARNESS
J602 C/N 2
10
1
2
3
4
5
6
7
8
9
NOTE: ALL WIRING IS
22 GAUGE,
UNLESS
OTHERWISE
INDICATED.
102302 N
2
1
5
6
3
4
22 BLK
22 BLK
22 BLU
22 BLK
18 BLK
18 BLK
18 RED
18 RED
22 BLK
22 BLK
22 RED
22 RED
91-34-50
ENGINE
AUDIO EFIS
INSTRUMENTS
HARNESS HARNESS
DAU
P1 NAV2-EFIS
GPS2/DAU
11
12
13
20
21
22
14
15
16
1
2
3
7
8
9
4 1
5
2
6 3
*
SEE 34-50-00, FIGURE 1.
P6-A1
COM-2
*
P6-A2
COM-2
P6-B1
GPS/N-2
*
P6-B2
GPS/N-2
Effectivity
4697001 thru 4697037
PAGE 7
Apr 15/07