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PIPER CHEROKEE WARRIOR SERVICE MANUAL
e. Remove the tee bar attaching bolts with their washers and nuts which are through each side of the
floor tunnel. Pull the lower end of the tee bar aft.
f. Disconnect the rudder control cable (19) ends from the arms on the torque tube (3) by removing
the cotter pins, washers, nuts and bolts (20).
g. Disconnect the rudder trim from the torque tube assembly by removing the cotter pin, washers and
bolt that connects the arm to the trim. [(36) and Figure 5-20 (7)]
h . Disconnect nose wheel steering bungees or push rods (21) at the inboard rudder bars (14) by
r e m o ving nuts and bolts (24).
i.
Disconnect the brake cylinders (12) at the lower end of each cylinder rod (11) by removing the
cotter pins and clevis pins (13).
j.
Disconnect the vee braces (29) from the torque tube by removing nuts, washers and bolts (27) that
secure the strap bracket (28) to the vee brace.
k . Disconnect the torque tube support bracket (35) where it attaches to floor by removing attachi n g
bolts.
1. Remove the two bolts (25 and 26) that extend through the torque tube and are located at the center
of the tube assembly over the floor tunnel. Compress the tubes.
m. Disconnect the torque tube support blocks (7 and 8) from their support brackets on each side of the
fuselage by removing the attaching nuts, washers and bolts (6).
n. Remove the trim side panels, if desired.
o. Remove the assembly from the airplane. Note the spacer washer (9) on each end and between the
support blocks.
5-28.
INSTALLATION OF RUDDER AND STEERING PEDAL ASSEMBLY. (Refer to Figure 5-15.)
Prior to installation, S/N's 28-74150001 thru 28-7415495 refer
to Piper Kit No. 760 935. S/N's 28-7716001 thru 28-8416095
refer to Piper Kit No. 764 975 .
a. Assemble the torque tube assembly (1, 2, 3 and 4) as shown in Figure 5-15. Do not at this time
install the two bolts (25 and 26) through the center of the tube assembly.
b. Place the upper support blocks (7) on the ends of the torque tube assembly. Note that a washer (9)
is required on each end of the tube.
c. Position the support blocks (7 and 8) on their mounting brackets at each side of the fuselage and
secure with bolts, washers and nuts. Note that a bushing is required in the bolt holes of the upper support
block, a plate (5) on top of the upper block, between the upper and lower blocks, and under the block mounting
bracket.
d. Align the bolt holes in the center area of the torque tube assembly, install bolts, washers and nuts
(25 and 26) and tighten.
e. Position the torque tube support bracket (35) on the floor tunnel and secure with bolts.
f. Position the vee braces (29) on the torque tube; install the strap bracket (28) around the torque tube
and brace and secure with bolts, washers and nuts (27).
g. Connect the ends of the brake cylinder rods (11) and clevis rods (15) to the idler arms (10) and
secure with clevis and cotter pins (13).
h. Connect the nose wheel steering bungees or push rods (21) to the rudder pedals (32 and 33) and
secure with bolts and nuts (24). Check nose wheel steering bungee or push rod adjustment per Alignment of
Nose Gear, Section VII.
Revised: February 28, 1995
NOTE
1H14
Island Enterprises
SURFACE CONTROLS
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