Raytheon BEECH BARON 58P User manual

Raytheon
Aircraft
BEECH
BARON,
Pressu
rized
58P 58PA
(TJ-3
and
After)
Tu
rbocharged
58TC
58TCA
(TK-1
and
After)
Maintenance
Manual
NOTE: This
manual
was
formerly
called
the
Beechcraft
Baron
58P
58PA/Barcn
58TC
58TCA
Maintenance
Manual.
Copyright
0
Raytheon
Aircraft
Company
2002
P/N:
102-590000-5
P/N:
102-590000-5A25
Issued:
April
1,
1975
Revised:
June
28,
2002
Courtesy of Bomar Flying Service
www.bomar.biz

Published
By
RAYTHEON
AIRCRAFT
COMPANY
P.O.
Box 85
Wichita,
Kansas
67201
U.S.A
NOTE
Where
seech
Aircraft
Corporation
is
referred
to
in
this
publication,
it
will
be taken
to
read
Raytheon
Aircraft
Company.
EXPORT
STATEMENT
Exported
under
the
authority
of license
exception:
TSU.
’7hese
commodities,
technology
or
software
were
exported
from
the
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States
in accordance
with
Export
Administration
Regulations.
Diversion
contrary
to
U.S.
law
prohibited."
Member
of GAIIIIA
Raytheon
Raythecn
Aircraft
General
Aviation
Company
GAA1A Manufacturers
Assoclatlon

Ray~heon
Aircraft
BEECH
BARON 58P
AND
58TC
MAINTENANCE MANUAL
Record
of
Revisions
Rev.
Rev.
Rev.
Date Inserted
By
Date
Inserted
By
Date
Inserted
By
No.
No.
No.
A23
11/17/97
A24
1/9/02
A25
8/21/02
ATP
When
a
revision
is
inserted,
the
revision
number,
the
date the
revision
is
inserted
into the
manual,
and
the
initials
of
the
person(s) inserting
the
revision
should
be
recorded
on
this
page.

Raytheon
Aircraft
BEECH
BARON
58P
AND
58TC
MAINTENANCE
MANUAL
LIST
OF
EFFECTIVE
REVISIONS
Always destroy
superseded
pages
when
you
insert
revised
pages.
Title
Page
June
28,
2002
"Logo"
Page
"A"
Page............................................................................................................................-´•´•..........-´•´•´•
A25
"B"
Page......................................................................................................................-´•´•´•´•´•´•´•´•..........´•´•´•´•
A25
PART NUMBER
DATE
CHAPTERS
AFFECTED
102-590000-5
April
1,
1975
Original
102-590000-5A1
October
3,
1975
Introduction, 7,
12,
20,
21,
24,
27,28,32,33,36,39,52,53,57,
61,
71,
77,
91
102-590000-5A2
January
9,
1976
Introduction,
5, 6,
12,
20,
21,24,
27,
28,
30,
32, 33, 34, 35, 36, 39,
51,52,53,55,56,57,71,74,80,
81,
91,
Insp
102-590000-5A3
September
24,
1976
25
102-590000-5A4
November
30,
1976
Introduction,
5,
6, 10,
12, 21, 24,
27, 28, 32,
33,
34,
36,
52,
54, 61,
102-590000-5A5
November
11,
1977
5,
27
102-590000-5A6
January
6,
1978
Introduction,
12,
21,
25,
27, 30,
32,
91
102-590000-5A7
November
30,
1978
Introduction, 5, 7, 11,
12,
20, 21,
22,24,25,27,28,32,33,35,36,
51,
61,
71,74,
77,
91
102-590000-5A8
March
23,
1979
Introduction, 21,28, 61,
71,
81
102-590000-5A9
May
25,
1979
28,
61
NOTE:
A
List
of
Effective
pages
will
be in
the
front
of each
chapter.
ic
publications
are
assigned
a
part
number
which
appears
on
the
title
page
with the
date
of the
issue.
Subsequent
revisions
are
identified
by
the addition
of
a
ision
code
after
the
part
number.
Al
after
a
part
number denotes
the
first
revision
to
the
basic
publication,
A2 the
second,
etc.
Occasionally,
it is
necessary
to
reissue
and
reprint
a
publication
for
the
purpose
of
obsoleting
a
previous
issue
and
outstanding
revisions
thereto.
As these
replacement
reissues
are
thecode
will also
change
to
the
next
successiveletter
of
the
alphabet
at
each
issues.
For
example,
B
for the
first
reissue,
C for
the
second,
etc.
ordering
a
handbook,
give
the
basic
number,
and the reissue
code when
applicable,
I
a
complete up-to-date
publication
is desired.
Should
only
revision
be
required, give
the basic
number
and
revision
code for
the
particular
set
of revision
pages
you
desire.
A25

Raytheon
Aircraft
BEECH BARON
58P
AND
58TC
MAINTENANCE MANUAL
LIST OF
EFFECTIVE
REVISIONS
(Continued)
Always
destroy superseded
pages
when
you
insert revised
pages.
PART NUMBER
DATE
CHAPTERS AFFECTED
102-590000-5A10
October
26,
1979
Introduction,
5,
11, 12,
20,
27,
35
102-590000-5A11
March
21,
1980
Introduction,
5,
12, 21, 25, 33,
56,
91
102-590000-5Ptl
2
August
1,
1980
Introduction, 11,
12,
25,73,
91
102-590000-5A13
November
12,
1980
Introduction,
24,
61
102-590000-5A14
March
31,
1981
5,
11,
57,
91
102-590000-5A15
June
18,
1981 23,
32
102-590000-5A16
March
31,
1982
5,
25
102-590000-5A17 June
21,
1982
5,
30
102-590000-5A18
October
6,
1983
Introduction,
5,
12,
27,
28,
32,
33, 51, 52,
56,
57, 73,
91
102-590000-5A19
Auguste4
1984 30
102-590000-5A20
November
9,
1984 30
102-590000-5A21
June
14,
1985
Introduction,
27
102-590000-5A22
May
22,
1987
Introduction,
5,
7,
9,
12, 25,
30,
36,61,
91
102-590000-5A23
February28,1989
5
102-590000-5A24
September
3,
2001
5,
20,
25, 27,
32
102-590000-5A25
June
28,
2002
Introduction,
5
A25

Raytheon
Aircraft
BEECH BARON 53P
AND
58TC
MAINTENANCE
MANUAL
LOG
OF
TEMPORARY REVISIONS
Revision
Revision
Revision
No.
Date
Subject
Incorporated
5-1
Oct
31/97
Revised
landing
gear
and
actuator
ovemaul
and
replacement
A24
schedule in
Chapter
5-10-00.
27-2
Nov
15/93
Revised
FLAP
DRIVE CABLE
CONNECTION in
Chapter
A24
27-50-00.
32-1
Jul
16/99
Add
LANDING GEAR
WARNING TEST to
Chapter
32-60-00. A24
Page
1
Sep
3/01
NOTE:
Insert
this
Log
of
Temporary
Revisions
after
the
Record
of
Revisions
page.
Previous
Log
of
Temporary
Revisions
may
be discarded.

Raytheon
Aircraft
BEECH
BARON
58P
AND
58TC
MAINTENANCE
MANUAL
P/N
102-590000-5A,
REVISION
A25,
JUNE
28/02
HIGHLIGHTS
The
chapters
which have
been
revised
are
listed
below
with
the
Highlights
of each
change.
Remove
the affected
pages
and
insert
the
A25
revision
in
accordance
with
the
attached
Instruction
Page.
Enter the
revision
number
and
the
date
inserted
on
the
Record
of
Revisions
page
of
this manual.
The
Highlight Page
may
be
retained
with
the
manual
for future
reference.
Chapter/Section
Description
of
Change
Introduction
Added
new
chapter
5-50-00
to
Index Guide.
Added
additional
data
and
revised
supplier
publications
data.
5-10-00
Propeller
overhaul
data
now
refers
to
supplier
data.
Added
data
on
engine
baffle
seals
and instrument
air
manifold
check
valve,
5-20-00
Changed
FAA
references
to
Title
14
Code
of
Federal
Regulations
(14
CFR)
references.
Added
requirement
to
check
instrument
air.
Added
requirement
to
check
cylinder
baffles
and
seals.
Added
reference
to
Service
Instruction
during
fuel
cell
inspection.
Added
Flapper
Valve
Inspection.
Added
reference
to
Service
Bulletin
for
window
inspection.
Added
inspection
of
control column
U-joint
roll
pins.
Added
inspection
of
nose
and
main
gear
torque
knees.
Lightning
strike
inspection
moved
to
new
Chapter
5-50-00.
5-50-00
Added
new
chapterfor
Unscheduled
Maintenace
Inspections.
Pagel
Jun
28/02
A25

Rsal~heon
Aircraft
REVISION
102-590000-5A25
to
the
BEECH
BARON
58P
AND
58TC
MAINTENANCE
MANUAL
P/N
102-590000-5
(ISSUED:
APRIL
1,
1975)
REMOVE
INSERT
PAGE
CHAPTER
PAGE
CHAPTER
DATED
Title
Page
Title
Page
Jun
28/02
Logo
Page
Logo
Page
"A"
Page
"A"
Page
A25
"B"
Page
"B"
Page
A25
All
INTRO-EFF
1
INTRO-EFF
Jun
28/02
All
INTRODUCTION
1
thru
14
INTRODUCTION
Jun
28/02
All
5-EFF
1
and
2
5-EFF
Jun
28/02
All
5-TOC
1
5-TOC
Jun
28/02
All
5-10-00
201
thru
206
5-10-00
Jun 28/02
All
5-20-00
201
thru 218
5-20-00
Jun
28/02
201
thru 211
5-50-00
Jun
28/02
NOTE
These
instruction
pages
may
be
discarded after
the
above
revision
has
been
properly
incorporated
into
the Maintenance
Manual.
Page
1
of
1

Raytheon
Aircraft
BEECH
BARON 58P
AND
BARON 58TC MAINTENANCE
MANUAL
INTRODUCTION
LIST OF
PA
GE EFFECTIVIP/
CHAPTE
R-S ECTI
ON
-S U BJ
ECT
PAGE
DATE
Introduction-Effectivity
1
Jun
28/02
Introduction
1
Jun
28/02
2
Jun
28/02
3
Jun 28/02
4
Jun 28/02
5
Jun
28/02
6
Jun
28/02
7
Jun
28/02
8
Jun
28/02
9
Jun 28/02
10
Jun
28/02
11
Jun
28/02
12
Jun
28/02
13
Jun
28/02
14
Jun
28/02
A25
INTRODUCTION-EFFECTIVITY
Jun
28/02Pagel

Ray~heon
Aircraft
BEECH
BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
INTRODUCTION
NOTE
Neither
reissues
nor
revisions
are
automatically
provided
to
the
holder
of
this manual.
For
informa-
tion
on
how
to
obtain
reissues
or
revisions
applicable
to
this
manual,
refer
to
the
latest
revision of
the
Raytheon
Aircraft
Company
Service
Bulletin
No. 2001.
The
Beech
Baron
58PIBaron
58TC
Maintenance
Manual
is
prepared
in
accordance
with the
GAMA
(General
Avia-
tion
Manufacturers
Association)
Specification
No.
2
format.
It also
meets
the
intent
of the
requirements
of
the
ATA
Specification
100
(Air
Transport
Association
of
America)
with
respect
to
the
arrangement
and
content
of the
System/
Chapters
within
the
designated
chapter-numbering
system.
This
maintenance
manual
is
supplemented
by
the
fol-
lowing
publications:
NOTE
It shall
be
the
responsibility
of
the
owner/operator
to
ensure
that
the
latest
revision
of
publications
referenced
in
this
handbook
are
utilized
during
operation,
servicing,
and
maintenance
of
the
air-
plane.
The
Beech
Baron
58P/Baron
58TC
Wiring
Diagram
Manual
P/N
102-590000-23
The
Beech
Baron
58TC
Wiring
Diagram
Manual
P/N 106-590000-13
or
106-590000-23
The
Beech
Baron
58P
Wiring
Diagram
Manual
P/N
102-590000-59
The
Beech
Baron
58P
and
Baron
58TC
Beech
Manufactured
Components
Maintenance
Manual
P/N
102-
590000-21
The
Beech
Baron
58P and
Baron
58TC
Parts
Catalog
P/N
102-590000-7
NOTE
This
manual
provides
maintenance
coverage
for the
Baron
58P
(airplane
serials
TJ-3
and
After)
and
the
Baron
58TC
(airplane
serials
TK-1
and
After).
Subjects
which
refer
to
only
the
Baron
58P
or
Baron
58TC
airplanes
will be
designated
by
the
airplane
serials.
Subjects
which
refer
to
both
the
Baron
58P
and
Baron
58TC
airplanes
will
not
be
serialized.
NOTE
Raytheon
Aircraft
Company
expressly
reserves
the
right
to
supersede,
cancel
and/or
declare
obso-
lete
any
parts,
part
numbers,
kits
or
publications
that
may
be
referenced
in
this
manual
without
prior
notice.
IWI\RNINO)
WARNING
Use
only
parts
obtained
from
sources
approved
by
Raytheon
Aircraft
Company,
in
connec-
tion with
the
maintenance
and
repair
of
Raytheon
Aircraft
Company
airplanes.
Genuine
Raytheon
Aircraft
Company
parts
are
produced
and
inspected
under
rigorous pro-
cedures
to
insure
airworthiness
and
suitability
for
use
in
Raytheon
Aircraft
Company
air-
n25
INTRODUCTION
Page
1
Jun
28/02

Raytheon
Aircraft
BEECH
BARON
58P AND
BARON
58TC MAINTENANCE MANUAL
plane
applications.
Parts
purchased
from
sources
other than
those
approved by Raytheon
Aircraft
Company,
even
though
outwardly
identical
in
appearance, may
not
have had
the
re-
quired
tests
and
inspections
performed,
may
be
different in fabrication
techniques
and
ma-
terials,
and
may
be
dangerous
when
installed in
an
airplane.
Salvaged
airplane
parts,
reworked
parts
obtained from
sources
not
approved
by
the
Raytheon
Aircraft
Company
or
parts,
components
or
structural
assemblies,
the
service his-
tory
of which is unknown
or
cannot
be
authenticated,
may
have been
subjected
to
unaccept-
able
stresses
or
temperatures
or
have
other hidden
damage,
not
discernible
through
routine
visual
or
usual
nondestructive
testing techniques.
This
may
render
the
part,
component
or
structural
assembly,
even
though
originally
manufactured
by
the
Raytheon
Aircraft Com-
pany,
unsuitable
and
unsafe
for
airplane
use.
Raytheon
Aircraft
Company expressly
disclaims
any
responsibility
for
malfunctions,
fail-
ures,
damage
or
injury
caused
by
use
of
parts
not
approved
by
the
Raytheon
Aircraft
Com-
pany.
CORRESPONDENCE
If
a
question
should
arise
concerning
the
care
of
your
airplane,
it
is
important
to
include
the
airplane
serial
number
in
any
correspondence.
The
serial
number
appears
on
the
model
designation
placard.
Refer
to
Chapter
11
for
placard
location.
ASSIGNMENT
OF
SUBJECT
MA
TERIAL
The
content
of
this
publication
is
organized
into
four levels.
The four
levels
are:
GROUP-
Identified
by
different
colored
divider tabs.
These
are
the
primary
divisions
of
the
manual
that
enable
broad
separa-
tion
of
content.
Typical
of this
division
is
the
separation
between
Airframe
Systems
and the
Power Plant.
SYSTEM/CHAPTER
The
various
groups
are
broken
down
into
major
systems
such
as
Environmental
Systems,
Electrical
Power,
Landing
Gear,
etc.
The
systems
are
arranged
more
or
less
alphabetically
rather than
by
precedence
or
importance.
They
are
assigned
a
number,
which
becomes
the
first
element
of the
standardized
numbering
system.
Thus,
the
element
"28"
of
the
number
28-40-01
refers
to
the
chapter
"FUEL".
Everything
concerning
the
fuel
system
will
be
covered
in
this
chapter.
SUBSYSTEM/SECTION
The
major
systems/chapters
of
an
airplane
are
broken
down
into
sub-systems.
These
subsystems
are
identified
by
the
second
element
of the
standard
numbering
system.
The
element
"40"
of
the
number
28-40-01
concems
itself
with the
indicating
section
of the
fuel
system.
UNIT/SUBJECT
The
individual
units within
a
subsystem/section
may
be
identified
by
the
third
element
of
the stan-
dard
numbering
system.
The
element
"01"
of the
number
28-40-01
is
a
subject
designator.
This element
is
assigned
at
the
option
of
the
manufacturer
and
may
or
may
not
be
used.
APPLICATION
Any
publication
conforming
to
the
GAMA
or
ATA
format
will
use
the
same
basic
numbering
system.
Thus,
whether
the
manual
is
Beech
Baron
58P/Baron
58TC Maintenance
Manual,
a
Beech
King
Air 90
Ovemaul
Manual,
or a
Wiring Diagram
Manual
for
a
Beech
Baron
58P/Baron
58TC,
the
person
wishing
information
concerning
the
indica-
Jun
28/02Page
2
INTRODUCTION
,5

Raytheon
Aircraft
BEECH BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
tion
portion
of
the
fuel
system,
would
refer
to
the
SystemlChapter
Tab
"28-FUEL". The
table of
contents
in the
front
of
this
chapter
will
provide
a
list
of
subsystems
covered
in
this
chapter.
For
example,
the fuel
system
chapter
with
a
full
index
would contain:
28-00
General
28-10
Storage
(Tanks,
cells,
necks,
caps,
instruments,
etc.)
28-20
Distribution
(Fuel
lines,
pumps,
valves,
controls,
etc.)
28-30
Dump
(If
in-flight dumping
system
is
installed,
it
would
appear
here.)
28-40
Indicating (Quantity,
temperature,
pressure,
etc.,
does
not
include
engine
fuel
flow
or
pressure.)
The material is
arranged
within the
chapter
in
ascending
numerical
sequence.
The
Chapter-Section-Subject
number
and
page
number
are
found
at
the lower
outside
corner
of each
page.
TITLE PAGE
A Title
page
is located
at
the
beginning
of
each
volume
and
provides
the
part
number of
the
manual,
the
chapters
contained in each
volume
and
lists
all
aircraft
models
pertaining
to
this manual and their
respective
serial numbers.
Information
throughout
this manual is
applicable
to
all serial numbers listed
on
the title
page
except
where
specifi-
cally
stated.
LIST
OF EFFECTIVE
REVISIONS
The List
of Effective Revisions
("A")
page
following
the title
page
of the manual
lists
the revisions
currently
effective
for
the manual.
RECORD OF
REVISIGNS
PAGE
A Record of
Revisions
page
is
provided following
the List of Effective Revisions
("A")
page.
When
a
revision
is in-
serted,
the revision
number,
the
date
the
revision
is inserted
into
the
manual,
and
the
initials
of
the
person(s)
in-
serting
the revision
should be recorded
on
this
page.
LOG
OF
TEMPORARY
REVISIONS
PAGE
A
Log
of
Temporary
Revisions
page
is
provided following
the Record
of
Revisions
page.
The
Log
of
Temporary
Re-
visions
page
provides
a
history
of
each
temporary
revision,
including
the revision
number which
incorporated
the
temporary
revision
into
the
manual.
RECORD OF
TEMPORARY
REVISIONS
PAGE
A Record of
Temporary
Revisions
page
is
provided
following
the
Record
of
Revisions
Page.
When
a
temporary
re-
vision
is
inserted
or
removed from
this
manual,
the
appropriate
information
should be recorded
on
this
page.
LIST OF
EFFECTIVE PAGES
that
chapter.The
list
of
effective
pages
following
each
Chapter-Divider-Tab
lists
the
issue
date of each
page
that
is
effective
for
I
a25
INTRODUCTION
3

Ray~heon
Aircraft
BEECH
BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
TEMPORARY
REVISIONS
Temporary
revisions
are
issued
to
provide
maintenance
information
in
the
interim
between
revisions.
Each
tempo-
rary
revision
is
issued
by
the
chapter
number
to
which
it
applies
followed
by
a
sequential
number in
the
order
of
publication
CTempora~y
Revisions
12-1,
12-2,
etc.).
Tempora~y
revisions
am
printed
on
yellow
paper
and
are
to
be
placed
in
the
maintenance
manual
in
accordance
with the
instructions
provided
on
each
page
included
in
the
revi-
sion.
The
information
in
the
temporary
revision
will
be
included
in the
next
revision
of the
manual.
REVISED
TEXT
That
portion
of
text
which
has
been
revised
by
the
addition
of,
or a
change
in,
information
is
denoted
by
a
solid
re-
vision
bar
adjacent
to
the
textual
column as
shown
in the
margin
of
this
paragraph.
Each
page
may
or
may
not
have
revision
bars.
The
revision
number
and
date
printed
on
the
bottom
of
each
page
indicates
when
and
by
what
revision
the
text
on
that
page
was
changed.
Each
page
will
ONLY
show
revision
bars
for
text
changed
by
the
current
revision.
There
will
not
be
a
revision
bar
if
text
was
deleted
from
the
page.
REVISED
ILLUSTRATIONS
Revised
art
may
be
identified
by
a
revision
bar
printed
on
the
side
of
the
page
for
major
changes
or
by
the
following
pointing
hand
symbol
for
minor
changes.
Ilr
WARNINGS,
CAUTIONS
AND
NOTES
WARNING
Brings
attention
to
an
operating
procedure,
inspection,
repair
or
maintenance
practices,
which
if
not
correctly
followed,
could
result
in
personal
injury
or
loss
of
life.
CAUTION
Brings
attention
to
an
operating
procedure,
inspection,
repair
or
maintenance
condition,
which
if
not
strictly
observed,
could
result
in
damage
or
destruction
of
equipment.
NOTE
Brings
attention
to
an
operating
procedure,
inspection,
repair
or
maintenance
condition,
which
is essen-
tial to
highlight.
SCHEMATIC
DIAGRAMS
Schematic
diagrams
are
illustrated
with
the
following
conditions:
Airplane
is
on
the
ground.
All
doors
are
closed
and
locked.
Electrical
power
is
not
applied
to
the
airplane.
A
note
will be
shown
on
the
schematic
diagram
if the
above
conditions
are
not
present.
An
example
would
be:
NOTE
Airplane
shown
with
power
applied
and
entrance
door
open.
Contacts
on
connectors
that
are
identified
with
lower
case
letters
will
be shown
by
an
underlined
letter
or
a
letter
with
an
asterisk
(A*).
Jun
28/02Page
4
INTRODUCTION
,5

Raylheon
Aircraft
BEECH
BARON
58P
AND
BARON 58TC MAINTENANCE
MANUAL
SUPPLEMENTARY
PUBLICA
TIONS
Additional
publications
are
listed
in
the
current
Publications Price List
CD
Rom
(P/N 994-32808).
For
infomnation
on
these
publications
contact
the Technical Manual
Distribution
Center
(TMDC)
at
1-800-796-2665,
fax
(316)
676-4824
or
E-mail TMDC@
Raytheon.com.
Since
a
wide
variety
of avionic
components
and
equipment
is
available and
because
avionics manufacturers
nor-
mally
supply
parts
and
servicing
manuals
with
each
set/component,
the avionic
publications
are
not
included
in
the
Publications
Price
List. The manufacturer of the
equipment
should
be
contacted
when additional
parts
or
servicing
information
is
required.
Following
is
a
list
of
publications providing
servicing
and maintenance
information
on
components
of
the Baron
58P/
Baron
58TC.
SUPPLIER
PUBLICATIONS
ENGINE
NOTE
The
following engine
manuals
are
not
available
through
Raytheon
Aircraft
Company.
Please
order
all
publications
for the
engine
from
Teledyne
Continental
Motors,
Aircraft
Products,
Mobile,
Ala-
bama.
Overhaul
Manual
Form
X-30042
Continental
TS10520
Series
Aircraft
Engines,
Teledyne
Continental
Motors,
Air-
craft
Products,
Mobile,
Alabama.
Parts
Catalog
Form
X-30043A,
Continental
TSIO-520
Series Aircraft
Engines,
Teledyne
Continental
Motors,
Aircraft
Products,
Mobile,
Alabama.
Operator’s
Handbook
Form
X-30505,
Continental
TSIO-520L
Aircraft
Engines,
Teledyne
Continental
Motors,
Air-
craft
Products,
Mobile,
Alabama.
Tips
On
Engine
Care,
Teledyne
Continental
Motors,
Aircraft
Products,
Mobile,
Alabama.
ALTERNATORS
Overhaul
Manual
Form
X30531
Continental-Crittenden
100
Ampere
Altemator,
Teledyne
Continental
Motors,
Air-
craft
Products,
Mobile,
Alabama.
PROPELLER
Overhaul
Instructions
117D
for Hartzell
Propellers,
Hartzell
Propeller,
Inc.,
Piqua,
Ohio.
Owner’s
Manual
115F for
Hartzell
Propellers,
Hartzell
Propeller,
Inc.,
Piqua,
Ohio.
Maintenance
Handbook
for
Constant
Speed
Hydraulic
Propeller
Govemor
Type
CSSA,
Number
33092,
Woodward
Governor
Company,
RocMord,
Illinois.
Test
Specifications
for
Small
Airplane
Governors
and
Accumulators,
Number
TSP-197,
Woodward
Governor
Com-
pany,
RocMord,
Illinois.
Spinner
Assembly
Maintenance
Instruction
Guide,
Dated
June,
1974,
Hartzell
Propeller,
Inc,
Piqua,
Ohio.
Propeller
Synchronizer
for
Light
Twin
Engine
Aircraft,
Number
33117,
Woodward
Governor
Company,
Rockford,
II-
linois.
INTRODUCTION
J.~Page
5

Raytheon
Aircraft
BEECH
BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
Woodward
Type
11
Engine
Synchrophaser
Installation
Manual
Bulletin
33171,
Woodward
Governor
Company,
RocMord,
Illinois.
FUEL
INJECTION
Operation
and
Service
Manual
for RSA-7DA1
Fuel
Injection
System,
Form
15-596,
Bendix
Corporation,
South
Bend,
Indiana.
MAGNETOS
Overhaul
Instructions
for Bendix
S-1200
Series
Magnetos
Form
L-609X,
Scintilla
Division,
Bendix
Aviation
Corpo-
ration,
Sidney,
New
York.
Service
Parts
List for
Bendix
S-1200
Magnetos,
Form
L608,
Scintilla
Division,
Bendix
Aviation
Corporation,
Sidney,
New
York.
AIR
CONDITIONER
COMPRESSOR
Service
Manual,
I.D.
160717,
Abacus
Air
Conditioning
Compressor
Models
506-503,
Abacus
International,
Dallas,
Texas.
Service
Manual,
I.D.
SD-5,
Sankyo
Air
Conditioning
Compressor
Models SD-505
thru
SD-510,
Sankyo
international
Inc.,
Dallas,
Texas.
FUEL
CELLS
Uniroyal
Handbook,
Recommended
Handling
and
Storage
Procedures
for Bladder
Type
Fuel
and
Oil
Cells,
P/N
FC1473-73,
Uniroyal
Inc.,
Mishawaka,
Indiana.
Goodyear
Manual,
Fuel
Cell
Repair,
P/N
AP
368,
Goodyear
Aerospace
Corporation,
Engineered
Fabrics
Division,
Rockmart, Georgia
30153.
AUTOPILOT
Automatic
Flight
Systems
AK424
and
AK424/FD,
FAA
Approved
Bulletin No.
547,
Edo-Aire
Mitchell,
Mineral
Wells,
Texas.
PROPELLER
DNCING
I
Installation
Manual,
Electrothermal
Propeller
Deicing
System,
Report
No.
70-04-700C,
8.
F.
Goodrich
Company,
Akron,
Ohio.
Installation
Manual,
Electrically
Heated
Propeller
Deicers,
Report
No
59-728J,
B.
F.
Goodrich
Company,
Akron,Ohio.
I
Maintenance
Manual,
Elactrothermal
Propeller
Deicing
Systems,
Report
No.
68-04-712C.
B. F.
Goodrich
Company,
Akron,
Ohio.
I
Overhaul
Manual.
BNSh
Block
Assemblies
for
Electrothermal
Propeller
Deicing
Systems,
Report
No
68-04-7141,
B.
F.
Goodrich
Company,
Akron,
Ohio.
PRESSURIZA
TION
(TJ-3
AND
AFTER)
Operation
and
Maintenance Instructions,
Report
No.
4-267,
AiResearch
Manufacturing
Division,
Los
Angeles,
Cal-
ifornia.
Jun
28/02Page
6
INTRODUCTION

Raytheon
Aircraft
BEECH
BARON
58P
AND
BARON 58TC MAINTENANCE
MANUAL
HEATER
(TJ-3
AND
AFTER)
Maintenance
Manual
for the
87D24-2
Igniter
Assembly,
Manual
No.
93D00-1 Janitrol Division
of
Midland-Ross Cor-
poration,
Columbus,
Ohio.
Operation
and
Maintenance
Instructions,
Report
No.
4-267,
Dated:
Dec
15,
1975,
AiResearch
Manufacturing
Divi-
sion,
Los
Angeles,
California.
Maintenance
Manual
for
82D20
and
07E02-1
Heater
Assembly,
Manual
No.
94D84-1,
Janitrol Division of Midland-
Ross
Corporation,
Columbus,
Ohio.
Maintenance
Manual for the
C241-500BD
Blower,
Dynamic
Air
Engineering,
Santa
Ana,
California.
Maintenance
Manual
for
the EM605-1
Centrifugal
Blower,
Eiectro
Mech,
Inc, Wichita,
Kansas.
HEATER
(TK-
I
AND
AFTER)
Maintenance
Manual
for the
82D18 Combustion
Air
Blower,
Manual No.
94D85-1,
Janitrol Division of Midland-Ross
Corporation,
Columbus,
Ohio.
EMERGENCY
LOCA TOR
TRANSM17TER
Operating
Instructions
for
Model
CIR-10(
Emergency
Locator
Transmitter
System,
Transmitter P/N
TR70-17,
Collins/Communications
Components
Corporation,
Costa
Mesa,
California.
Operating
Instructions
for
Model
CIR-11(
Emergency
Locator
Transmitter
System,
Transmitter P/N
TR70-13,
Collins/Communications
Components
Corporation,
Costa
Mesa,
California.
Owners
Manual,
Installation
and
Pilot’s
Guide
P/N
03716-0602
for the
Narco
ELT
10
Emergency
Locator
Trans-
mitter,
Narco
Avionics,
Division
of Narco
Scientific
Industries,
Fort
Washington,
Pennsylvania.
SUPPLEMENTARY
BEECH
PUBLICATIONS
98-34998
Maintenance
Instructions
for
Goodrich
Wheel,
Brake and
Tire
Assembly.
98-35061
Servicing
and
Maintenance
Instructions
for
the
Nose Wheel
Assembly.
98-35798A Maintenance
Information
and
Illustrated
Parts Breakdown
for
Landing
Gear
Motor
Part
No. 96-380022.
32-31-24
Component
Maintenance
Manual
with
Illustrated Parts
List for
Landing
Gear Motor
Part No.
96-380022-5.
98-37515D
Safety
Information
Booklet
SYSTEM/CHAPTER
INDEX
GUIDE
The
following
System/Chapter,
Subsystem/Section
Index
Guide
is
prepared
in
accordance
with both
GAMA
Speci-
fication
No.
2
and
ATA
Specification
No.
100
for
use
with
maintenance
manuals,
parts
catalogs
and
wiring
diagram
manuals.
The
following
chapters
are
not
applicable
to
this
maintenance
manual:
23,
26,
29, 31,
37,
38,
49, 60, 70,
75, 76,
78
and
83.
INTRODUCTION
7

Ray~heon
Aircraft
BEECH
BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
CHAPTER/SYSTEM
INDEX
GUIDE
SYSTEM/CHAPTER
SUBSYSTEM/SECTION
TITLE
5
TIME
LIMITS/MAINTENANCE
CHECKS
10
Time
Limits
20
Scheduled
Maintenance
Checks
50
Unscheduled
Maintenance
Checks
6
DIMENSIONS
AND
AREAS
00
General
7
LIFTING
AND
SHORING
00
General
8
LEVELING
AND
WEIGHING
00
General
9
TOWING
AND
TAXIING
00
General
10
PARKING
AND
MOORING
00
General
10
Parking/Storage
11
PLACARDS
AND
MARKINGS
00
General
20
Exterior
Placards
and
Markings
12
SERVICING
00
General
Jun
28/02Page
8
INTRODUCTION
A25

Ral~heon
Aircraft
BEECH
BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
CHAPTEWSYSTEM
INDEX
GUIDE
(CONTINUED)
SYSTEMICHAPTER
SUBSYSTEM/SECTION
TITLE
10
Replenishing
20
Scheduled
Servicing
30
Unscheduled
Servicing
20
STANDARD
PRACTICES
AIRFRAME
00
General
21
AIR
CONDITIONING
00
General
10
Compression
(TJ-3
and
After)
20
Distribution
30
Pressurization
Control
(TJ-3
and
After)
31
Door
Seal
Pressurization
(TJ-3
and
After)
40
Heating
50
Cooling
22
AUTO
FLIGHT
24
ELECTRICAL
POWER
00
General
20
AC
Generation
30
DC
Generation
31
Voltage
Regulation
32
Battery
33
Low
Voltage
Detector
40
External
Power
50
Electrical
Load
Distribution
51
Alternate
Battery
Bus
Distribution
A25
INTRODUCTION
Page
9
Jun
28/02

Raylheon
Aircraft
BEECH
BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
CHAPTER/SYSTEM
INDEX
GUIDE
(CONTINUED)
SYSTEMICHAPTER
SUBSYSTEM/SECTION
TITLE
25
EQUIPMENT/FURNISHINGS
0
General
60
Emergency
27
FLIGHT
CONTROLS
00
General
10
Aileron
and
Tab
20
Rudder
and
Tab
30
Elevator
and
Tab
31
Stall
Warning
50
Flaps
70
Gust
Lock
and
Damper
28
FUEL
00
General
10
Storage
20
Distribution
40
Indicating
30
ICE
AND
RAIN
PROTECTION
00
General
10
Airfoil
20
Airlntakes
30
Pitot
and
Static
40
Windows
and
Windshields
60
Propellers
Jun
28/02PagelO INTRODUCTION
A25

Raytheon
Aircraft
BEECH
BARON
58P
AND
BARON
58TC
MAINTENANCE
MANUAL
CHAPTEWSYSTEM
INDEX
GUIDE
(CONTINUED)
SYSTEM/CHAPTER
SUBSYSTEM/SECTION
TITLE
32
LANDING
GEAR
00
General
10
Main
Gear and
Doors
20
Nose
Gear
and Doors
30
Extension
and
Retraction
40
Wheels
and
Brakes
50
Steering
60
Position
and
Warning
33
LIGHTS
00
General
40
Exterior
34
NAVIGATION
00
General
10
Flight
Environment
Data
35
OXYGEN
00
General
36
PNEUMATIC
00
General
39
ELECTRICAL
PANELS
AND
COMPONENTS
00
General
10
Instrument
and
Control
Panels
20
Electrical
and
Electronic
Equipment
Racks
A25
INTRODUCTION
Page
11
Jun
28/02