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

Page: 387 / 1956

PAGE 21
Feb 28/07 2G13
22-10-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
105129
1045
8 5
1014 8 6
101 3 49
COTTER PIN S ,
M S 24665-1 3 4,
IN S TALLED A S
CABLE GUARD S
(2 PLC S )
77.25
W.L.
PITCH S ERVO
( S EE DETAIL, BELOW, FOR BRIDLE
CABLE WRAP INFORMATION.)
BOLT, AN 3 -4A
WA S HER, NA S 1149F0 3 6 3 P
NUT, NA S 679A 3 W
(4 EACH REQ'D)
VIEW LOOKING LEFT FROM CENTERLINE OF AIRCRAFT
(ELEVATOR S ECTOR OMITTED FOR CLARITY)
EXI S TING ELEVATOR TRIM CABLE
AUTOPILOT S ECTOR A SS EMBLY
ADJU S T BRIDLE CABLE TEN S ION:
- 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 .
EXI S TING ELEVATOR CABLE
3 11.00
F. S .
TURNBUCKLE
LOCKING CLIP,
M S 21256-1 (2 REQ'D)
FWD
UP
EXI S TING PITCH CABLE
COTTER PIN S
IN S TALLED A S
CABLE GUARD S
(2 PLC S )
CLEVI S PIN, (2 REQ'D)
WA S HER, NA S 1149F0 3 6 3 P (4 REQ'D)
COTTER PIN, M S 24665-1 3 4 (2 REQ'D)
(CUT TO LENGTH)
BRIDLE CABLE WRAPPING DETAIL
(CAP S TAN COVER AND CABLE GUARD S OMITTED FOR CLARITY)
WRAP FORK END 495° AND AFT
PITCH S ERVO
BRIDLE CABLE
WRAP TERMINAL END 3 15° AND UP
PO S ITION OF BRIDLE CABLE CENTER BALL
WITH ELEVATOR CONTROL IN FULL DOWN
PO
S ITION. DEPRE SS CENTER BALL TO
BOTTOM OF HOLE AND TIGHTEN S ET S CREW.
AFT
UP
45°
Pitch Servo Installation
Figure 6
Effectivity
System 55X shown
System 55 as noted