Piper Aircraft Corporation Malibu Mirage PA-46-350P, Airplane Maintenance Manual

Page: 379 / 1956

PAGE 13
Feb 28/07 2G5
22-10-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
105129
1045
8 5
1014 8 6
101 3 49
.005 MIN GAP BETWEEN CLAMP
HALVE
S AFTER TORQUING
TORQUE CLAMP BOLT S
TO 55 ± 5 IN. LB S
BULKHEAD F. S . 17 8 .60
(VIEW LOOKING DOWN AT IN S TALLATION)
BOLT, AN 3 -4A
WA S HER, NA S 1149F0 3 6 3 P
NUT, NA S 679A 3 W
(4 EACH REQ'D)
CABLE CLAMP DETAIL
CABLE CLAMP
AILERON BALANCE CABLE
(BRIDLE CABLE BEHIND)
ROLL S ERVO
( S EE DETAIL BELOW FOR
BRIDLE CABLE WRAP INFORMATION.)
LEFT
FWD
BULKHEAD F. S . 171.40
CHAFE BLOCK
AILERON CABLE
AILERON
BALANCE CABLE
PULLEY
CABLE CLAMP
L OF A/C
C
AILERON
BALANCE
CABLE
ADJU S T AUTOPILOT
BRIDLE CABLE TEN S ION
TO 15 ± 2 LB S .
BRIDLE CABLE WRAPPING DETAIL
(VIEW LOOKING UP, CAP S TAN COVER AND CABLE GUARD S REMOVED FOR CLARITY.)
LOCATION OF CENTER-BALL WITH AILERON S
IN NEUTRAL PO S ITION. DEPRE SS CENTER-BALL
TO BOTTOM OF HOLE AND TIGHTEN S ET S CREW.
ROLL S ERVO
WRAP LONG END 2 8 0°
AND INBOARD
WRAP S HORT END 440°
AND OUTBOARD
AUTOPILOT
BRIDLE
CABLE
AFT
10
°
Effectivity
System 55X shown
System 55 similar
Roll Servo Installation
Figure 3