Raytheon Beech Baron E55 - Utility Baggage Door (Optional)

Raytheon
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
ADJUST LATCH BOLT
BY
LOOSENING
ROTATE THE OPERATING TUBE
THESE SCREWS
(4)
TO
ADJUST BOLT PROTRUSION
BOLT
Hft
ttt
TUBE
INSIDE DOOR LOOKING
OUTBOARD
C
045234AA.AI
Cabin
Door
Latch Points
Figure
21
(Sheet
4
of
4)
UTILITY
BAGGAGE
DOOR
(OPTIONAL)
The
utility
baggage
compartment
door is
located
on
the
right
hand
side
of the
fuselage,
aft
of
the
wing,
below
the
rear
window.
The door is
opened
by
turning
a
"D"
shaped
handle and is held
in
the
open
position by
a
support
rod
in
the
upper
right
hand
corner.
A small
stop
chain
prevents
the door
from
being
opened
too
far
and
striking
the
trailing
edge
of the
flap.
The
latching
mechanism
incorporates
a
bayonet
type
latching
mechanism.
When
the
mechanism
is
actuated
(by
turning
the
handle)
the
bayonet points
enter
the
door
facing
and
hold
the
door
securely
in the closed
position.
A
locking
mechanism,
actuated
by
a
key
from
outside
the
airplane,
prevents
the handle
from
turning.
UTILITY
BAGGAGE
DOOR
REMOVAL
AND
INSTALLATION
NOTE:
Parts that
rotate,
swivel
or
slide
(metal
to
metal)
and that
have
no
provisions
or
instructions for
lubrication,
should be
lubricated
with
SAE
20W
oil,
1
0W30
oil
or
equivalent
(5,
Consumable
Materials
Chart,
Section
2).
a.
Open
the
door
to
the
full
open
position.
b. Disconnect
the
stop
chain
at
the
upper
right
hand
corner
of
the door.
c.
Remove
the
piano hinge
wire
at
the
right
hand
side
of
the
door
and
remove
the door.
Installation
of
the
baggage
door
is the
reverse
of
the
removal
procedure.
Page
46Dec
31/04
SECTION
3
E23