Aileron Control Cables Removal - Piper PA-32R-301 SARATOGA SP Maintenance Manual

AILERON CONTROLS (cont)
C Control Column Installation (cont)
(3) To Install Flex Joint Replacement (Refer to Figure 6 and 7) (cont)
(c) Ream drilled hole, in steps, with a #1 reamer, checking to insure proper depth for taper pin
and sufficient pin thread protrusion for proper installation.
Reamer may be purchased from Enstice Tool Co., Palm Bay,
Florida.
(d) Install pin through tube and shaft.
1 If pin shoulder does not protruded past tube surface, install a AN960-10 washer
2 If pin shoulder does protruded past tube surface, install a MS20364-1032C washer
(e) Install nut. Torque 35 - 40 inch-pounds.
D. Aileron Control Cables Removal (Refer to Figure 8)
(1) To remove any of the control cables in the fuselage or either wing:
(a) Remove center seats and seat belt attachments
(b) Remove screws securing floor panel located directly aft of the main spar. Lift panel and
remove from airplane.
(c) Remove tunnel plate just aft of the tee bar by laying back enough tunnel carpet to remove
plate attachment screws.
(d) Remove forward heat duct from side of floor tunnel from which the cable is to be removed
by removing trim control wheel cover, heater baffles from side of duct, floor carpet and the
duct attachment screws.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
– NOTE –
WASHER (P/N 407 564 [AN960-10])
0.098 DIA. SEE SAFE HOLE
TO ENSURE PROPER SHAFT
INSERTION
Flex (Universal) Joint Assembly
Figure 7
2B11
TAPER PIN (P/N 480 730)
OR
WASHER (P/N 494 093 {AN975-3])
NUT (P/N 484 835 [MS20364-1032C])
SHAFT (P/N 62716-07)
FWD
27-10-00
Page 27-13
Reissued: July 1, 1993