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

Page: 385 / 1956

PAGE 19
Feb 28/07 2G11
22-10-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
105129
1045
8 5
1014 8 6
101 3 49
YAW S ERVO
BRIDLE CABLE WRAPPING DETAIL
(CAP S TAN COVER AND CABLE GUARD S OMITTED FOR CLARITY)
WRAP 450° AND UP
LOCATION OF CENTERBALL WITH RUDDER
IN NEUTRAL. DEPRE
SS CENTERBALL TO
BOTTOM OF HOLE & TIGHTEN S ET S CREW.
BRIDLE CABLE
WRAP 450° AND UP
BOLT, AN 3 -5A
WA S HER, NA S 1149F0 3 6 3 P
NUT, NA S 679A 3 W
(4 EACH REQ'D)
CABLE CLAMP
(2 REQ"D)
BULKHEAD F. S . 2 8 2.00
(RUDDER PULLEY S OMITTED FOR CLARITY)
VIEW DOWN AND AFT
EA
YAW S ERVO
VIEW EA-EA
(LOOKING LEFT)
S EE DETAIL (BELOW)
FOR BRIDLE CABLE
WRAP INFORMATION.
EA
L OF AIRCRAFT
C
FWD
UP
ADJU S T BRIDLE
CABLE TEN S ION
PER NOTE 1.
RIGHT
RUDDER CABLE
(LEFT OMITTED
FOR CLARITY)
CABLE
GUARD
S
CAP S TAN
COVER
RIGHT
RUDDER CABLE
LEFT
RUDDER CABLE
NOTE 1: S Y S TEM 55 ( S /N' S 46 3 6160 AND 46 3 624 8 THRU 46 3 6 3 1 3 ONLY) = 15 ± 2 LB S .
S Y S TEM 55X ( S /N' S 46 3 6 3 14 AND UP) = 3 0 ± 2 LB S .
BRIDLE CABLE
WRAP 450° AND UP
(ORIENTATION FOR S /N' S 46 3 6 3 75 AND UP )
Yaw Servo Installation
Figure 5
Effectivity
System 55X shown
System 55 as noted