Piper CHEROKEE WARRIOR PA-28-151 1995 Maintenance Manual page 166

PIPER CHEROKEE WARRIOR SERVICE MANUAL
5-9. INSTALLATION OF FLEX JOINT REPLACEMENT. (Refer to Figures 5-6 and 5-7.)
a. Carefully lay out location for hole to be drilled in flex joint tube to match hole in control column
shaft.
b. Using a #5 (0.2055) drill bit, drill hole through flex joint tube at location determined in paragraph
(1).
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.
5-10. AILERON CONTROLS.
5-11. REMOVAL OF AILERON CONTROL CABLES. (Refer to Figure 5-8.)
a. For the removal of either the control cables in the fuselage or the wings, first remove the rear seat
bottom.
b. To remove either the right or left primary control cables (14 or 15) that are located in the fuselage,
the following procedure may be used:
1. Remove the two front seats from the airplane.
2. Remove the tunnel cover located aft of the tee bar assembly by removing the rudder trim
control knob and trim cover attaching screws. Roll back the carpet from the tunnel and remove the tunnel
plate that is located just aft of the tee bar assembly by removing the plate attaching screws.
Revised: February 28, 1995
NOTE
WASHER (P/N 407 564 [AN960-10])
WASHER (P/N 494 093 {AN975-3])
NUT (P/N 484 835 [MS20364-1032C])
0.098 DIA. SAFE HOLE TO
VISUALLY ENSURE PROPER
SHAFT INSERTION
Figure 5-7. Flex (Universal) Joint Assembly)
1G22
Island Enterprises
TAPER PIN (P/N 480 730)
OR
SHAFT (P/N 62716-07)
FWD
SURFACE CONTROLS