Piper 6X User Manual

TO OIL PRESSURE SENSOR
(SEE 91-77-40, FIGURE 2)
TO MAP TRANSDUCER
(SEE 91-77-40, FIGURE 1)
P901
P10A-WHT/BL
19
1110
TO
ALTERNATOR
SHUNT
(SEE 91-24-30,
FIGURE 1)
98
P10A-WHT
P8C-WHT/BL
P8C-WHT
BATT AMP (+)
POWER GROUND
28 VDC POWER
120
BATT AMP (-)
SHIELD
ALTNR AMP (+) ALTNR AMP (-)
3625 7 624
DATA ACQUISITION UNIT
P1
4
P20B20
P20A20
P20E20N
GB1-H
P902
28 VDC POWER
1
P20C20
POWER GROUND
20
P20D20N
GB2-H
CB-4
DAU
1A
Q5A20
Q5R20
E9K22
TO
BATTERY SHUNT
(SEE 91-24-30,
FIGURE 1)
101849 3.0 NEW
THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 6
Feb 19/04
5K8
91-77-40
Data Acquisition Unit (DAU)
Figure 6 (Sheet 1 of 2)
Eff
ectivity
with Avidyne Entegra option
3232014 & up
3255015 & up

Piper 6X Specifications

General

Brand	Piper
Model	6X
Category	Aircrafts
Language	English