Piper 6XT - Page 224

THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 2
Feb 19/04
1K8
APPENDIX 1
(BLK)
(WHT)
(WHT)
(ENC. ALT.)
ANNUNCIATOR
ANNUNCIATOR
TURN
COORDINATOR
(RED)
(BLK)
(WHT)
(RED)
(WHT)
(OPTIONAL)
ALTITUDE
SELECTOR / ALERTER
ALT. SEL.
(BLK)
P1
PROG/COMP
(12 PIN)
MOLEX
F/D 2
A/C GND
TURN COORDINATOR
ANNUN
TO A/P DISC
TO AIRFRAME GND
TO T&B C/B
(5 AMP MAX.)
TO AVIONICS BUSS
TO JB1-E
(BLK)
TO A/C GND
TO JB3 & JB4
TO A/C GND
CONTROL WHEEL CONN)
TO A/P DISC (PIN 11 OF
TO JB7-F
NAV/HDG
(BLK)
TO A/C GND
COMPUTER
PROGRAMMER/
HORN
P2
(WHT)
TO A/C GND
(WHT)
(WHT)
TO JB1-J
SWITCH
MASTER
TO DIMMER LIGHT RHEOSTAT
MONITOR
TRIM
(WHT)
TRIM
PILOT'S CONTROL WHEEL
OPTION-F/D A/S
TO JB1-N
(6 PIN
MOLEX)
T3
(4 PIN MOLEX)
A/S 1
(6 PIN MOLEX)
F/D 1
(3 PIN MOLEX)
(3 PIN MOLEX)
PROG/COMP
TRIM MONITOR
(RED)
TRIM MASTER SW
TO A/C GND
(BLK)
A/P A+ (RED)
(BLK)
TO
A/C GND
(RED) TRIM CB
TRIM
2 AMP C/B
A/C BUSS
39328-3
39236-8
T1
T2
SEE SHEET 3 FOR EXCEPTIONS WHEN
AVIDYNE ENTEGRA OPTION IS INSTALLED.
A
B
C
TRANSDUCER
TRANSDUCER
PRESSURE
(WHT)
TO JB8-H
System 55X Autopilot Installation
Figure 1 (Sheet 1 of 3)
Effectivity
3232003 & up
3255001 & up