NC
C
NO
NC
NO
2
6
B
A
A
B
AVIONICS MASTER
PR1B10
PR2A20
X2
A4
X1
PR1A10
A3
PR2B20
CB10
15
PITOT
HEAT
BLACK
P6C20
P6D20N
3
2
BLK
GRN
R FWD FUSELAGE SIDEWALL
P6B20
1
RED
LOW VOLT
P310
P324
W8A20
H2B16
H3B16
TO P315-7 *
PITOT HEAT SWITCH
3
1
2
OFF
W8B20
AVIONICS MASTER
1
ON
2
3
OFF
MAIN BUS
AVIONICS BUS
PR2B20
PR1B10
PR1A10
INSTRUMENT PANEL
35
34
BUS
MAIN
1A
P6A20
TO P316-16 *
TO P315-8 *
W11A20
W8C20
H2B16
H1C16
H2C16
P311
WHT
BLK
TO STROBE LT SW **
PITOT SENSOR ASSY
WHT
WHT
WHT
WHT
GRN
GRN
BLK
BLK
3
5
4
1
H1B16
H1B16
5
4
6
ON
H1A14
PITOT
STATIC
TO CB12 *
GB
GB4-C
A
B
MON
SWITCH
101902-SHT 13-H/U
* SEE 91-31-50, FIGURE 1, SHEET 5
TO 91-33-10, FIGURE 4, SHEET 2
** SEE 91-33-10, FIGURE 5, SHEET 2
BAG AND STOW CONNECTOR AND WIRING
(AIR COND. OPTION WIRING)
PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 2
Nov 30/06
5I4
91-30-30
Pitot Heat
Figure 1 (Sheet 2 of 2)
Eff
ectivity
with Avidyne Entegra