Piper Cherokee Six - Page 88

MOUNTING
BRACKET
PIPER
CHEROKEE
SIX
SERVICE
MANUAL
TRIM WHEEL BOLT
T
Figure
3-3.
Flap
Control
Cable
Attachment
Bolt
Inspection.
3-10.
INSPECTION
OF FLAP
CONTROL
CABLE
ATTACHMENT
BOLT.
(Refer
to
Figure
3-3.)
a. This
inspection
should
be
accomplished
at the
next
100
hours
or annual
inspection
and repeated
at each
500
hours
thereafter.
b. The
inspection
is
required
to
detect
any
possible
wear
and replacement
of
attachment
bolt,
should
evidence
of
wear be
detected.
c. Remove
the royalite
flap or
flap/trim
cover.
d. On
aircraft
having
the
flap
handle
only,
proceed
as follows:
1.
Remove
flap
handle
mounting
bracket
attachment
bolts.
2.
Raise
flap
handle
and
bracket
assembly
to
gain
access
to
the
control
cable
attachment
bolt.
e. On
aircraft
having
the
flap
handle
and
trim
wheel
mounted
together,
proceed
as
follows:
1. Loosen
the
trim
wheel
attachment
bolt.
2.
Remove
the
trim
wheel
bracket
attachment
bolts
and
remove
bracket
from
top
of
tunnel.
3.
Remove
flap
handle
mounting
bracket
attachment
bolts
and
raise
handle
and
bracket
assembly
to gain
access
to control
cable
attachment
bolt.
f. Remove
and
inspect
cable
attachment
bolt
for
possible
wear.
Should
wear
be
detected.
replace
bolt
with
new AN23-1
I clevis
bolt.
g.
Reinstall
all
parts
that
were
removed.
INSPECTION
Revised:
6/18/76
1D16