Piper COMANCHE PA-24-180 Service Manual page 148

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COWTSOL CAUL ATTYACEMIT BOLT
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PIPER COMANCHE SERVICE MANUAL
AILS
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FIGURE 5-3 INSTALLATION
OF
BELLCRANK CHECKING TOOL
FIGURE 54. AILERON ADJUSTING POINTS
6. If the forward conrol cables in the fuelage aue inaled, connect the
rap
fitma (7) of the
cables a sation 126.5 uing bolt, ut and cotter pi.
c lIntlnaion
of the left and/or right primay control cable(s) within the fuselage may be
accomplished by the following procedure:
1. From the pulley chsuer within the fuseage at suion 115.0, draw the primry cable forwrd
through the floor support bulkbhead, nder the pulley cduser t staion 50.0 and up co the vercal sprocket
chain.
CAUTION
When stringing the cables on the front pulley duser just aft of fire wall,
be sue o tohred cable in the pulley groove and not over top of either
the front or bottom cable guards. (Refer to View A-A of Figure 5-2.)
2. Connect the cable with turnbuckle to the verical chain using clevis bolt, bushing, nut Lnd
cotter pin.
3. Connect the fuselage primry cable with the wing primary cable by use of bol, washer and
nut through a shackle at fuselage staon 126.3.
4. Replace the cable gurd (15) a the pulley cluster ft of the rar spar and the two cable guards
at the pulley cluster at staion 50.0, safety the pards.
d. Set cable tension per Table V-l, check rgig
and adjumnent per Paragraph 5-11 and ascertain
that all turnbuckles are safeied.
e.
Insll acces plates and panels, carpets, seat rcks and seas.
SURFACE CONTROLS
ISSUED: 1/18/72
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