Raytheon Beech Baron E55 - Page 195

Raytheon
nircraft
Company
BARON
55
AND
58
SHOP
MANUAL
UTILITY
BA
GGA GE DOOR RIGGING
I
a.
Remove
the
door
(Ref.
Figure
22).
b.
For
ease
of
maintenance,
place
the door
on
a
bench.
c.
Remove the
upholstery
panel
and
turn
the handle
to
the
closed
position
and
note
that
the
vertical
legs
on
the
latching
mechanism
’7"
bracket
of
the
door travels
20 10"
past
the
center
position
with
a
slight
retraction
of
all
three
bayonet
points.
In this
position (20
10"
past
center)
the
latching
mechanism
’T’
bracket
should
fuliy
engage
the
stop
and the "D" handle should be
in
a
horizontal
position.
d.
if
the
vertical
legs
of
the
latching
mechanism
’T’ bracket
do
not
travel
20
~t
10"
past
center
with
full
engagement
of the
stop,
adjust
the
length
of the
bayonet
post
or
the
position
of
the
stop
until
this
reading
is attarned.
e.
After
the
proper
alignment,
lubricate all
moving
parts
of
the
latching
system
with
a
mixture
of
oil
(16.
Consumable
Materials
Chart,
Section
2),
and
graphite (27,
Consumable
Materials
Chart,
Section
2).
Apply
door-ez
to
the
bayonet
attach
points
in
the
area
of
the
striker
plates
and
guide
blocks.
f.
After
lubricating
the
designated
areas,
actuate
the
handle
several
times. A
maximum
pull
of
40
inch-pounds
of
torque
should
be
required
to
actuate
the door
handle
to
the closed and
latched
position.
g.
Install
the
interior
upholstery
panel
and
install the
door
on
the
airplane.
AFT
BAGGA
GE DOOR
The aft
baggage
door is
located
on
the
right
hand
side
of
the
fuselage just
aft
of
the
trailing edge
of
the
wing.
The
door is
opened
by pushing
in
the
latch
button which releases the
locking
mechanism
and
allows
the door
to
open.
The door
may
be locked
by
the
key
furnished
with
the
airplane.
AFT
BA
GGA
GE
DOOR REMOVAL
A ND
INSTALLA
TION
NOTE:
Parts that
rotate,
swivel
or
slide
(metal
to
metal)
that
have
no
provisions
or
instructions
for
lubncation
should
be lubricated
with
SAE
20W
oil,
10W30
oil
or
equivalent (5,
Consumable
Materials
Chart,
Section
2).
a.
Open
the door
to
the
full
open
position.
b. Remove the
piano
wire
hinge
at
the
edge
of
the door.
c.
Remove the door
from
the
airplane.
d. Installation
of
the
aft
baggage
door
is
the
reverse
of
the removal
procedure.
AFT
BAGGA GE DOOR ADJUSTMENT
Adjustment
of the
door is
accomplished by readjusting
the
position
of the
latching
mechanism
striker
plate
at
the
rear
edge
of
the
door
frame.
Turn
the
attach
screws
on
the striker
plate
and
move
the striker
plate
either
in
or
out
to
obtain the
desired
holding
tension of the door
in
the closed
position.
E23
SECTION 3Page
47