Raytheon Beech Baron E55 - Flaps

Raytheon
Aircraft
BEECH
BARON
55
AND
58 SHOP
MANUAL
FLAPS
FLAP
REMOVAL
FIGURE
4-28
a.
Remove
the
bolt from the
flap
actuating
arm.
b.
Remove
the
bonding
cable from the
flap.
c.
Remove
the
bolts from the
rollers
in
the
flap
track
and
remove
the
flap.
FLAP
INSTALLA
TION
FIGURE
4-28
a.
Hold
the
flap
in
position
and install
the rollers
and
bolts in
the
flap
track.
NOTE
Install
the
flap
track
rollers
(four
rollers
per
flap
and
two
rollers
per
trackj
in the
flap
track with
the
flanges
of
the rollers
in
one
track
facing
the
flanges
of
the
rollers in the
other
track.
b.
Connect
the
bonding
cable
and install
the
bolt
in the
flap
actuating
arm.
FLAP
TRACK
WEAR LIMITS
The
allowable
track
wear on
the
bearing
surfaces
is
0.032
inch,
resulting
in
a
maximum
dimension of
0.785
inch
for
the
slot
in
the
flap
track. The allowable
wear
into
the track side surface is
0.050
inch.
Track
wear
within
the
preceding
limitations
can
be
dressed smooth
with
fine
emery
cloth
to
prevent
roller
binding.
Lubricate
the
tracks
with
Molykote
Z
mixed
with
naphtha (12
and
18,
Consumable
Materials
Chart,
Section
2),
brushed
on
the
flap
tracks.
FLAP
ACTUATOR
FLAP
DRIVE
SHAFT
AND
HOUSINGFLAP
ACTUATOR
LIMIT
MOTOR
FLAP
DRIVE
SHAFT
SWITCHES
AND
HOUSING
FLAP
ACTUATOR
58-161-17
Flap
System
Figure
4-28
E16
4-73