(Tj-3 And After) - Raytheon BEECH BARON 58P Maintenance Manual

BEECHCRAFT
BARON 58P AND BARON 58TC
MAINTENANCE MANUAL
CHECK-RELIEF VALVE REMOVAL
c.
Disconnect the nipple from the tank and cap the
(TJ- 123 and after) nipple
and the tank
opening.
d.
Remove the tank from the airplane.
a.
Gain
access
to the
check-relief valve through the
large
access
door
on
the
LH side of the airplane.
The
check-relief valve is
located under the door seal
pressure
PRESSURE TANK INSTALLATION
tank
on
the RH side of the
airplane just
ah of F.S. 190.00
(TJ-210, TJ-~9 and after)
b.
Unscrew the nuts from
both ends of the check-
relief valve and
remove
the
valve.
a.
Place the tank in position and
secure
to
the
c.
Cap
the
open ends of both swivel tees where the
airplane
structure with the attach
screws.
nuts
are
attached
to
prevent foreign matter
from entering.
b.
Remove the caps from the tank opening and the
nipple.
c.
Wrap tape (62,
Chart
207, 91-00-00) around the
CHECK-RELIEF VALVE /NSTALL4T/ON
threads of the nipple and connect it
to
the tank.
(TJ-123 and after)
d.
Secure the
access
door.
a.
Remove the caps from the ends of both swivel
tees.
DOOR SEAL AUTOMAT/C DEFLATE SW/~CH
b.
Place the check-relief valve in
position and
screw
REMOVAL (TJ-3 and after)
the nuts onto
both ends of the valve.
a.
Gain
access
to
the automatic deflate switch by
removing the
upholstery panels
at
the aft edge
of the door
PRESSURE TANK REMOVAL
frame.
(TJ-3
thru
T~-228, except
TJ-210)
b. Tag and
remove
electrical wires.
a.
Gain
access
to
the pressure tank through the
nose
baggage compartment
door.
NOTE
b.
Locate the
pressure
tank,
ah of FS 10.00, and
remove
floorboard panels ah of the
pressure
tank.
Ensure that the door is open,
so
that the switch
c.
Disconnect pressure tubing
from the ah side
of
actuator
will
not
be damaged.
the tank. Install dust
caps on
tubing
and tank opening.
d. Remove the attaching
hardware from the
top
of
the tank and
remove
the tank.
c.
Remove attaching
hardware and
remove
the
automatic
deflate switch.
I
PRESSURE
TANK
/NSTALLAT/ON
DOOR 'SEAL AUTOMAT/C DEFLATE SW/~CH
(TJ-3 thru TJ-223, except TJ-210)
/NSTALLAT/ON (TJ-3
and
after)
a.
Place the pressure tank in the proper position.
b.
Install the attaching hardware and
secure
the
NOTE
tank.
c.
Remove dust caps and
connect
pressure
tubing
Ensure that the door is open,
so
that the switch
to
the tank.
actuator will not be damaged.
d.
Install the floorboard panels in the
nose
baggage
compartment.
Close and
secure
the
nose
baggage
compartment
door.
a.
Place the automatic deflate switch in the
proper
position
and
secure
with attaching hardware.
b. Remove
tags
and
connect
electrical wires.
PRESSURE TANK REMOVAL
c.
Adjust
the automatic deflate switch
as
described in
(TJ-~10,
TJ-229 and after)
DOOR SEAL AUTOMATIC DEFLATE SWITCH
ADJUSTMENT.
a.
Gain
access
to
the pressure
tank thru the
large
d.
Conduct the PRESSURIZATION TEST
access
door
on
the LH side of the tail
section. The tank is
PROCEDURE
as
described in Chapter 21-30-00. Determine
located just
ah of FS
190.00
on
the RH side of the airplane.
that the door seal is inflating. If
not,
adjust the automatic
b. Remove the
screws
attaching the tank bracket
to deflate switch
as necessary.
the airplane structure.
a.
Install upholstery panels.
213100
Page 202
Mar 21/80