Raytheon Beech Baron E55 - Page 289

Raytheon
Aircraft
BEECH BARON
55 AND 58
SHOP
MANUAL
FLAP
SHAFT
INSTALLA
TIOIV
FIGURE
4-32
a.
Pull
the
flap
shaft and
housing through
the
wing
and attach
the
actuator
to
the
wing
flap
and
wing
spar
section.
b.
Settheflaps
inthe
neutral
position.
NOTE
A
retainer
has
been
added
to the
flap
cables
where
they
join
the
flap
gearbox.
This
retainer
may
have
been
on
production
airplanes
or
added
by
Beech
Service
Bulletin
No.
2460.
c.
Connect
the
flap
drive
cables
to
the
flap
drive
motor
in
accordance
with
FLAP
DRIVE
CABLE
CONNECTION.
I
d.
Install
the
clamps
securing
the
shaft
housing
to
the
wing
structure.
e.
Install
the
dust
cover
in the
rear
section
of
the wheel well.
f.
Run
the
flaps through
fully
up
and
fully
down
travel
to
check
flap
rigging.
g.
Lower
the
landing
gear
and
remove
the
airplane
from
the
jacks.
h.
Installthe
sparcover.
i.
Install
the
front
seat
assemblies.
FLAP
INNER
FLEX
SHAFT REMOVAL
FIGURE
4-32
a.
Place
the
airplane
on
jacks
and
retract
the
landing
gear
(using
the
circuit
breaker)
until the
inboard
door
is
open.
b.
Remove
the front
seat
assemblies.
c.
Remove the
spar
cover.
NOTE
A
retainer
has
been
added
to
the
flap
cables
where
they
join
the
flap gearbox.
This retainer
may
have
been
on
production
airplanes
or
added
by
Beech
Service
Bulletin No. 2460.
d.
Loosen
the
two set
screws
on
cable
retainer.
e.
Rotatethecable retainer90".
f.
Remove
the
dust
cover
in
the
rear
of
the
wheel
well
to
gain
access
to
the
actuator.
g.
Remove
the
two
bolts
holding
the
forward
end
of
the
actuator
in
place.
NOTE
The
first
clamp
which
secures
the
flex drive
to
the
wing
may
have
to
be removed
to
allow
more
flexibility
to
the flex
drive.
The
position
transmitter
may
need
to
be
removed from
the left
flap.
E16
4-81