Piper PA-28-161, Maintenance Manual

Page: 1064 / 1104

NC
C
NO
NC
NO
2
6
B
A
A
B
AVIONIC S MA S TER
PR1B10
PR2A20
X2
A4
X1
PR1A10
A 3
PR2B20
CB10
15
PITOT
HEAT
BLACK
P6C20
P6D20N
3
2
BLK
GRN
R FWD FU S ELAGE S IDEWALL
P6B20 1 RED
LOW VOLT
P 3 10
P 3 24
W 8 A20
H2B16
H
3 B16
TO P 3 15-7 *
PITOT HEAT S WITCH
3
1
2
OFF
W 8 B20
AVIONIC S MA S TER
1
ON
2
3
OFF
MAIN BU S
AVIONIC S BU S
PR2B20
PR1B10
PR1A10
IN S TRUMENT PANEL
3 5
3 4
BU S
MAIN
1A
P6A20
TO P 3 16-16 *
TO P 3 15- 8 *
W11A20
W 8 C20
H2B16
H1C16
H2C16
P 3 11
WHT
BLK
TO S TROBE LT S W **
PITOT S EN S OR A SS Y
WHT
WHT
WHT
WHT
GRN
GRN
BLK
BLK
3
5
4
1
H1B16
H1B16
5
4
6
ON
H1A14
PITOT
S TATIC
TO CB12 *
GB
GB4-C
A
B
MON
S WITCH
101902-
S
HT 1
3
-H/U
* S EE 91- 3 1-50, FIGURE 1, S HEET 5
TO 91- 33 -10, FIGURE 4, S HEET 2
** S EE 91- 33 -10, FIGURE 5, S HEET 2
BAG AND S TOW CONNECTOR AND WIRING
(AIR COND. OPTION WIRING)
PIPER AIRCRAFT
,
INC.
P
A
-28-161,
W
ARRIOR III
MAINTENANCE MANU
AL
P
A
GE 2
No
v 30/06
5I4
91-30-30
Pitot Heat
Figure 1 (Sheet 2 of 2)
Eff
ectivity with A
vidyne Enteg
ra