EasyManua.ls Logo

Raytheon Beech Baron E55 - Page 112

Raytheon Beech Baron E55
903 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
ReYnReeER
nircraft
Company
BARON
55
AND
58
SHOP
MANUAL
PNEUMA
TIC
PRESSURE
SYSTEM
(TC-1
AND
AFTER;
TE-
I
AND
AFTER;
TH-
I
AND
AFTER)
FILTER
REPLACEMENT
The
pneumatic
system
has
four
filters
which
need
to
be
replaced
periodically.
NOTE:
Any
time
a
pump
is
replaced,
the
inline
filter
must
be
replaced.
The
inline
filters
are
located
directly
down
stream
from
the
pressure
regulators
in
each
engine
compartment
and
should
be
replaced
in
accordance
with
the
OVERHAUL
AND
REPLACEMENT
SCHEDULE
in
Section
15.
For
TC-1
thru
TC-2002;
TE-1
thru
TE-936;
TH-1
thru
TH-372
that
have
not
complied
with
Service
Instructions
No.
0581-194,
the
intake
filters
are
located
on
the
fonn~ard
side
of
each
engine
rear
baffle.
The
foam
type
filter
shouM
be
removed
each
100
hours,
washed
in
solvent
and
blown
dry
with
low
pressure
shop
air.
For
TC-2003
and
After;
TE-937
and
After;
TH-373
and
After
and
earlier
airplanes
that
have
complied
with
Service
Instructions
No.
0581-194,
the
intake
filter
should
be
replaced
in
accordance
with
the
OVERHAUL
AND
REPLACEMENT
SCHEDULE
in
Section
15
(Ref.
Figure
3).
This
filter
element
must
not
be
subjected
to
sdvent
and
must
be
replaced
if
this
occurs.
Always
install
the
filter
cover
with
the
opening
facing
down.
Tli7ER
CII~RIDCI
(FOI
REPLACEMENT
OIDEI
P/N
D9-ll-1)
~I
NA543003-14
lPACEI
*H31~´•3t
IIUr
NUT
I
iii
~1
iiTER
f!
~1
AN936
LOCI(
YrAlnER
AN970-3
WAIHER
960PDlf16
WASHER
Tlltill
RETAINER
NVT
ANb
W*SWtl!
IIO-IPO´•IQ
Air
Filter
Replacement
Figure
3
E23
SECTION
2
Dec
31~eege
27

Table of Contents

Related product manuals