RUDDER AND TRIM CONTROLS. (cont)
(2) To Install Rudder Trim Control. (Refer to Figure 17.) (cont)
(c) Before attaching assembly to mounting channel, check that:
1
Clips are installed so safety wire will be on top.
2
Threaded bushing is installed on assembly shaft with welded attachment bushing forward
or toward housing.
(d) Attach housing lug to arm provided on rudder pedal torque tube. Secure with bolt, washer
and nut. Tighten nut only finger tight and safety with cotter pin.
(e) Clamp rudder pedals in neutral. Position threaded bushing and shaft extension in mounting
channel.
1
Install the clevis pin and cotter pin.
2
Check that dimensions noted in Figure 17 are maintained.
(f) Install fuel selector panel cover and cover attachment screws.
(g) Install rudder trim knob
(h) Ensure that neutral indicator aligns with neutral position on cover placard.
0.25 must be held when trim assembly
installedwith rudder pedals in neutral posit ion
0.25
(3) Rigging and Adjustment of Rudder Trim Controls
No adjustments are necessary, other than those required during installation of assembly in the air-
plane. Refer to Installation of Rudder Trim Controls, paragraph E, (2).
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
12
11
1
6
12
11
15
13
4
9
1 4
5
3
2
Rudder Trim Control
Figure 17
2B24
7
1 . COVER
2 . RUD DER TRIM C ON TR OL KNOB
8
3 . LOCK SC REW
10
4 . BUSH IN G
5 . CLEVIS PIN
6 . CONTROL SHA FT HOUSING
7 . BOLT ASSYMBLY
8 . MOU NTIN G CH ANN EL
9 . SCREW
10 . SCREW
11 . CLIPS
12 . SAFETY WIR E
13 . IN DICATOR WA SHER
14 . SPACER PLATE
15 . CONTROL SHA FT
27-20-00
Page 27-26
Reissued: July 1, 1993