THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 12
Jun 1/03
2K12
27-30-00
3 Position cable pulleys on their mounting bracket and install clevis pin, washer and
cotter pin.
4 Connect forward cable to aft cable at turnbuckle in aft section of fuselage. If aft cable
has not been installed, refer to Aft Stabilator Trim Controls, Installation, below.
5 Install cable guard at cable pulleys in aft lower section of fuselage forward of cable
turnbuckles.
6 Install cable guard plate at underside of pulley cluster located in aft area of aft floor
tunnel. Secure with screws.
7 Install pin type cable guard at underside of pulleys located in forward area of aft floor
tunnel. Secure with a tinnerman nut.
8 Install cable rub blocks located on aft side of main spar housing. Secure with screws.
9 Remove blocks that secure aft trim cable. Check that cables are seated on their
pulleys.
10 Set cable tension. Check rigging and adjustment. Check safety of all turnbuckles.
11
Install tunnel cover on forward tunnel. Secure with screws.
12
Install carpet over floor tunnel.
13 Install heat deflectors on each side of floor tunnel.
14 Install cover over trim control wheel and secure with screws and special washers.
15
Install fuel selector knobs and secure with set screws.
16
Install seat belts removed from top of floor tunnel. Secure with bolt, washer and nut.
17 Install floor panel and seat belt attachments aft of main spar. Secure panel with
screws.
18
Install aft floor tunnel and secure with screws.
19 Install carpet over aft floor tunnel.
20
Install trim plate on top of forward end of aft floor tunnel.
21 Install panel to aft section of airplane.
22
Install seats.
B. Aft Stabilator Trim Assembly
(1) Removal
(a) Remove access panel to aft section of the fuselage.
(b) Block trim cables at the first set of pulleys forward of cable turnbuckles in the aft section of
the fuselage by method shown in Figure 5.
(c) Disconnect cable at the turnbuckles in aft section of fuselage.
(d) Remove cable guard from pulley cluster.
(e) Remove tail cone by removing attachment screws.
(f) Disconnect link between trim screw and trim control arm by removing nut, washer and bolt
connecting link to screw.
(g) Remove cotter pin from top of trim screw. Turn screw down and out of barrel.
(h) Remove snap ring, washer and thrust washer from the bottom of barrel.
(i) Disconnect diagonal rib from the horizontal rib that supports trim assembly by removing
four attachment nuts, washers and bolts.
(j) Draw trim cable from fuselage.
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