Piper Comanche PA-24 Service Manual page 266

4. Through the access hole in the wing at station 115.5, position the cable on the lower pulley of
the cluster and install the cotter pin cable guard.
5. Attach the cable to the aft end of the cable bellcrank by assembling turnbuckle and/or securing
with clevis bolt, washer, nut and cotter pin.
NOTE: Do not tighten turnbuckle fork ends on the bellcrank so tight that the end cannot
rotate.
6. If the forward control cables in the fuselage are installed, connect the strap fitting (7) of the
cables at station 126.5 using bolt, nut and cotter pin.
C. Installation of the left and/or right primary control cable(s) within the fuselage may be
accomplished by the following procedure:
CAUTION: WHEN STRINGING THE CABLES ON THE FRONT PULLEY CLUSTER JUST
AFT OF FIRE WALL, BE SURE TO THREAD CABLE IN THE PULLEY GROOVE
AND NOT OVER TOP OF EITHER THE FRONT OR BOTTOM CABLE GUARDS.
(REFER TO VIEW A-A OF FIGURE 5-6.)
1. From the pulley cluster within the fuselage at station 115.0, draw the primary cable forward
through the floor support bulkhead, under the pulley cluster station 50.0 and up to the vertical
sprocket chain.
2. Connect the cable with turnbuckle to the vertical chain using clevis bolt, bushing, nut and
cotter pin.
3. Connect the fuselage primary cable with the wing primary cable by use of bolt, washer and nut
through a shackle at fuselage station 126.3.
4. Replace the cable guard (15) at the pulley cluster aft of the rear spar and the two cable guards
at the pulley cluster at station 50.0, safety the guards.
D. Set cable tension per Table V-I, check rigging and adjustment per Paragraph 5-11 and ascertain that
all turnbuckles are safetied.
E. Install access plates and panels, carpets, seat tracks and seats.
V - SURFACE CONTROLS
PIPER COMANCHE SERVICE MANUAL
1G6
04/01/09