Beechcraft Pressurized Baron 58PA Quick start guide

ATP
INDEX
COPYRIGHT 2002
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ATP
GRID INDEX TO
MANUFACTURER’S PUBLICATION:
BEECH
AIRCRAFT CORP.
58P,58PA,58TC,58TCA
WIRING
MANUAL
SECTION
TOPIC
GENERAL
INFORMATION
TITLE PAGE
MANUFACTURER’S
INTRODUCTION
RECORD OF
REVISIONS
RECORD OF
TEMPORARY REVISIONS
ALPHABETICAL
INDEX
ALPHA-NUMERIC
INDEX
AIRFRAME SYSTEMS
21.00.00 AIR CONDITIONING
21.00.00
LIST OF EFFECTIVE PAGES
21.30.00 PRESSURIZATION CONTROL
21.31.01 CABIN
21.32.01
DOOR SEAL
SYSTEM
21.32.01
TJ-l THRU
TJ-35
21.32.02 TJ-36
THRU T3-84
21.32.03
TJ-85,
TJ-87 THRU T3-97
21,32.04
TJ-86,
TJ-98 THRU TJ-122
21.32.05
’TJ-123 THRU
TJ-168
21.32.06
TJ-169 AFTER
22".33.01
CABIN ALTITUDE
WARNING T3-3 MRU
T3-119
21.33.01
T3-3 MRU TJ-119
21.33.02
TJ-120
THRU T3-168
21.33.03
TJ-169
AFTER
21.40.00
HEATING
21.40.01
TJ-3 THRU
TJ-228 EXCEPT TJ-210
21.40.02
TK-1 THRU TK-56
21.40.03
TJ-210,
TJ-229 AFTER
03/13/98
Copyrigh’e
(c)1998
Ai:rcraf~t;
Technical Publishers
PAGE:
1
(RCR2102)
(BC
0442
WD)

SECTION
TOPIC
21.50.00
COOLING
21.50.01
TJ-3
THRU
T3-105
21.50,03
TJ-106
THRU
TJ-168
21.50.04
T3-169
AFTER
21.51.01
TJ-3
THRU
TJ-7
(OPTIONAL)
21.51.03
T3-8
THRU
TJ-105
(OPTIONAL)
21.51.05
TJ´•106
MRU
TJ-132
(OPTIONAL)
21.51.06
TJ-133
AFTER
(OPTIONAL)
24.00.00
ELECTRICAL
POWER
24.00.00
LIST
OF
EFFECTIVE
PAGES
24.30.00
DC
GENERATION
24.30.02
LH
ALTERNATOR
AND
REGULATOR
24.30.02
TJ-3
THRU
TJ-106,
TK-1
THRU
TK-42
24,30.03
TJ-107
THRU
TJ-132,
TK-43
THRU
TK-56
24.30.04
TJ-133
MRU
TJ-138
24.30.05
T3-139
MRU
TJ-315
24.30.06
TJ-316
AFTER
24.31.02
RH
ALTERNATOR
AND
REGULATOR
24,31.02
TJ-3
THRU
TJ-138,
TK-1
MRU
TK-56
24.31.03
TJ-139
THRU
T3-315
24.31.04
TJ-316
AFTER
24.32.02
BATTERY
24.32.02
TJ-3
MRU
T3-112,
TK-1
THRU
TK-51
24.32.03
TK-1
THRU
TK-56
24.32.04
TK-52
MRU
TK-56,
TJ-113
THRU
TJ-168
24.32.05
T3-169
AFTER
24.40.00
EXTERNAL
POWER
24.41.01
EXTERNAL
POWER
(OPTIONAL)
24.50.00
ELECTRICAL
LOAD
DISTRIBUTION
24,50.01
WITHOUT
ALTERNATE
BUS
24.50.01
TK-1
THRU
TK-56,
TJ-3
THRU
TJ-168
24.50.02
TJ-169
THRU
TJ-194
EXCEPT
T3-188
24.50.03
TJ-188,
T3-195
AFTER
24.51.01
WITH
ALTERNATE
BUS
24.51.01
TK-1
MRU
TK-56,
TJ-3
MRU´•
TK-92
24.51.03
TJ-93
THRU
TJ-168
24.51.04
TJ-169
AFTER
25.00.00
EQUIPMENT/FURNISHINGS
25.00.00
LIST
OF
EFFECTIVE
PAGES
25.10.00
FLIGHT
COMPARTMEKT
25.10.01
CIGARETTE
LIGHTER
25.11.01
DIGITAL
CHRONOMETER
(OPTIONAL)
25.11.01
TJ-113
THRU
13-168
25,11.02
TK-52
THRU
TK-56
25.11,03
TJ-169
THRU
TJ-213
EXCEPT
TJ-210
TJ-212
25.11.04
T3-210,
TJ-212,
TJ-214
THRU
TJ-234
25.13..05
13-235
AFTER
25.60.00
EMERGENCY
03/13/98
Copyright
(c)1398
Aircraft
Technical
Publishers
PAGE:
2
(RCR2102)
(BC
0442
WD)

SECTION
TOPIC
25.60.01
EMERGENCY
LOCATOR
TRANSMITTER
27.00.00
FLIGHT
CONTROLS
27.00.00
LIST
OF
EFFECTIVE
PAGES
27.30.00
ELEVATOR
AND
TAB
27.31.01
STALL
WARNING
(WITH
HEATER)
27.31.01
TK-1
MRU
TK-39,
TJ-3
THR~
TJ-97
27.31.02
TK-40
THRU
TK-56,
TJ-98
T~RU
TJ-121
27.31.03
TJ-122
AFTER
27.32.01
ELEVATOR
TRIM
(OPTIONAL)
27.50.00
FLAPS
27.50.01
MOTOR
27.50.02
PERMANENT
MAGNET
MOTOR
27.50.02
TK-43
THRU
TK-56,
T3-107
THRU TJ-126
27,50.03
TJ-127
THRU
TJ-134
27.50.04
TJ-135
’THRU
TJ-186
27.50.05
TJ-187
AFTER
27.51.01
POSITION
INDICATOR
27.51.01
TJ-3
MRU
T3-186,
TK-1
THRU
TK-55
27.51.02
TJ-187
AFTER
28.00.00
FUEL
28.00.00
LIST
OF
EFFECTIVE
PAGES
28,10.00
STORAGE
28.10.01
FUEL
VENT
HEATERS
28,20.00
DISTRIBUTION
28.20.01
FUEL
BOOST
PUMP
28.20.01
TK-1
THRU
TK-56,
TJ-3
THRLI
TJ-168
28.20.02
TJ-169
THRU
T3-223
28.20.03
TJ-224
AFTER
28.40.00
INDICATING
28,40.01
FUEL
QUAKTITY
28,40.01
T3-3
THRU
TJ-27
28,40.02
TJ-28
AFTER,
TK-I
THRU
TK-56
28.40.03
T3-368
AFTER
30.00.00
ICE
AND
RAIN
PROTECTION
30.00.00
LIST
OF
EFFECTIVE
PAGES
30.10.00
AIRFOIL
30.10.01
SURFACE
DEICE
(OPTIONAL)
30.10.01
7;7-3
T3-4
30.10.03
TJ-5
THRU
TJ-97
EXCEPT
T3-86,
TK-I
THRU
TK-56
30.10,04
TJ-3,
TJ-86,
T3-98
THRU
T3-316
30.10.05
TJ-317
AFTER
30,30.00
PITOT AND
STATIC
30.30.01
HEAT
30.40.00
WINDOWS,
WINDSHIELDS,
AND
DOORS
30.40.01
WINDSHIELD
ANTI-ICE
(OPTIOM;I\L)
30.41.01
WINDSHIELD
ALCOHOL
30.42.01
WINDSHIELD
ELECTROTHERMAL
ANTI-ICE
03/13/98
Copyright
tc)1998
AircPaft
Technica~
Publishers
PAGE:
3
(RCR2102)
(8C
0442
WD)

SECTION
TOPIC
30.60.00
PROPELLERS/ROTORS
30.61..01
3
BLADE
DEICE
30.61.02
3
BLADE
ANTI-ICE
(OPTIONAL)
30.61.02
T3-l1
MRU
T3-176 EXCEPT
TJ-174,
TK-1
THRU
TK-56
30.61.03
TJ-174,
T3-177
THRU
7;1-348
30.61.04
T3-349
AT~R
31.00.00
INDICATING/RECORDING
SYSTEMS
31.00.00
LIST
OF
EFFECTIVE
PAGES
31.30.00
RECORDERS
31.30.01
FLIGHT
HOUR
METER
(OPTIONAL)
31.31.01
ENGINE
HOUR
METER
(OPTIONAL)
31.50.00
CENTRAL
WARNING
SYSTEMS
32.51.01
GWIESHIELD
ANNUNCIATOR
31.51.01
TJ-169
THRU
TJ-316
31.51.02
T3-317
AFTER
31.52.01
GLARESHIELD
ANNUNCIATOR
LIGHT
TEST
31.52.01
T3-169 MRU
TJ-316
31.52.02
TJ-317
AFTER
32.00.00
LANDING
GEAR
32.00.00
LIST
OF
EFFECTIVE
PAGES
32.30.00
EXTENSION
AND
RETRACTION
32,30.02
LANDING
GEAR
MOTOR AND
RELAY
32.30.02
TK-1
THRU
TK-56,
TJ-3 THRU
TJ-132
32.30.03
TJ-133
AFTER
32.31,01
LANDING
GEAR
POSITION
INDICA~R
32.31,01
TK-1
THRUT
TK-56,
TJ-3
THRU TJ-132
32.31.02
TJ-133
MRU
TJ-168
32.31.03
TJ-169
AFTER
32.60.00
POSITION
AND
WARNING
32.60.01
THROTTLE
32.60.01
TK-1
THRU
TK-56
TJ-3
THRU
TJ-133
32.60.02
T3-134
AND
AFTER
33.00.00
LIGHTS
33,00.00
LIST
OF
EFFECTIVE
PAGES
33.10.00
FLIGHT
COMPARTMENT
33.10.01
ANNUNCIATOR
LIGHT
TEST
33,10.01
TK-1
TO
TK-56,TJ-3
TO
-97
EXCEPT
-46,-55,-83,-86,-89
33.10.02
TK-1,
TK-9
MRU
TK-56,TJ-4~6,T3-55,TJ-83,TJ-85,TJ-89
33.10.03
TJ-86,
T3-98
THRU
TJ-119
33.10~04
TJ-120
THRU
TJ-168
33.11.01
MAP,
COMPASS,
OAT AND
WHEEL CLOCK
LIGHTS
33.11.01
TK-1
THRU
TK-56,
TJ-3
MRUIT;3-92
33.11.02
TJ-93
THRU
TJ-116
33.11.03
TJ-117
THRU
TJ-209,
T3-211,
TJ-213
33,11.04
TJ-210,TJ-212,
TJ-214 XI
AF71ER
33,12.01
ENGINE
INSTRUMENT
AND
RADIO
~BGKTS
33.12.01
TK-1
THRU
TK-56,
TJ-3
THRU!
T5-92
03/13/98
Copyright
(c)1998
Technical
Publishers
PAGE:
4
(RCR2102)
(BC
WD)

SECTION
TOPIC
33.12.02
TJ-93
THRU
TJ-134
33.12.03
TJ-135
8
AFTER
33.13.01
ENGINE
INSTRUMENT
AND
RADIO
POST
LIGHTS
33,13.02
11;3-263
AND
AFTER
33.14.01
ENGINE
INSTRUMENT
AND
RADIO´• WEDGE
LIGHTS
33.14.02
TJ-263
AND
AFTER
33,15.01
FLIGHT
INSTRUMENT
LIGHTS
33.15.01
TK-1
THRU
TK-56,
TJ-3 THRU
T3-92
33,25.02
T3-93
AFTER
33.16.01
FLIGHT
INSTRUMENT
POST
LIGHTS
33.16.02
T3-263
8
AFTER
33.17.01
FLIGHT
INSTRUMENT
WEDGE LIGHTS
33.17.02
T3-263
8
AFTER
33.18.01
FLOODLIGHTS
33.18.01
TK-1
THRU
TK-56,
TJ-3
THRU
TJ-92
33.18.02
TJ-93
THRU
TJ-129
33.18.03
TJ-130
8
AFTER
33.19.01
ELECTROLUMINESCENT
PANEL
LIGHTS
33.19.01
TK-1
THRU
TK-56,
TJ-3
MF~
TJ-92
33.19.02
TJ-93
8
AFTER
33.20.00
PASSENGER
COMPARTMENT
33.20.01
CABIN
LIGHTS
33.20.01
TK-1
THRU
TK-56,
TJ-3
THRU
TK-92
33.20.02
TJ-93
MRU
TJ-122
33.20,03
T3-123
8
AFTER
33.30.00
CARGO
AND
SERVICE
COMPARTMENTS
33.30.01
BAGGAGE
COMPARTMENT
LIGHTS
33.40.00
EXTERIOR
33.40.01
THREE
LIGHT
STROBE
33.40.01
TK-1
MRU
TK-19,
TJ-3
THRU
TJ-79
33.40.02
TK-20
MRU
TK-56,
7;3-80
THRU
TJ-132
33.40.03
T3-133
8
AFTER
33.43.01
TAXI
LIGHT
33.44.01
ROTATING
BEACON
33.44.01
TK-1,
T3-3
MRU
T3-53
33.44.02
TK-2
THRU
TK-56,
TJ-54
8
AFTER
33.45.01
NAVIGATION
LIGHTS
33.45.01
TK-1
THRU
TK-56,
T3-3
THF~´•
TJ-132
33,45.02
TJ-133
8
AFTER
33.46.01
LANDING
LIGHTS
33.46.01
TK-1
MRU
TK-28,
TJ-3
MRU TJ-93
33.46.02
TK-29
MRU
TK-56,
TJ-94
8;
AFTER
33.47.01
ICE
LIGHTS
34.00.00
NAVIGATION
34.00.00
LIST
OF
EFFECTIVE
PAGES
34.20.00
ATTITUDE
AND
DIRECTION
34.20.01
TURN
AND
SLIP
COORDINATOR
34.20.01
TK-1
THRU
TK-56,
TJ-3
THRU
TJ-92
34.20.02
TJ-93
8
AFTER
03/13/98
Copyright
(c)1998
Aircra.ft
Technical
Publishers
PAGE:
5
(RCR2102)
(BC
0’442
WD)

SECTION
TOPIC
34.21,01
GYRO
INSTRUMENTS
STRUCTURE
52.00.00
DOORS
52.00.00
LIST
OF
EFFECTIVE
PAGES
52.70.00
DOOR
WARNING
52.70.01
CABIN
AND
DOOR
COURTESY
LIGHTS
52.70.01
7;3-3
THRU
TJ-66
52.70.02
TK-1
THRU
TK-56
52.70.03
TJ-67
MRU
TJ-94
52,70.04
TJ-95
THRU
T3-122
52.70.05
TJ-123
MRU
TJ-168
52.70.06
TJ-169
AFTER
PROPELLER/ROTOR
61.00.00
PROPELLERS/PROPULSORS
61.00.00
LIST
OF
EFFECTIVE
PAGES
61.20.00
CONTROLLING
61.20.02
PROPELLER
SYNCHRONIZER
AND
GOVERNOR
61.20.02
TJ-3
THRU
TJ-105
EXCEPT
T3-46,
T3-55,
T3-83,
TJ-85,
61.20.02
TJ-89,TJ-93,
TJ-97
MRVTJ-99,
TJ-103
61.20.03
TK-1
MRU
TK-56,
TJ-46,
TJ-56,
TJ-83,
T3-85,
TJ-89,
61.20.03
TJ-93,
TJ-97
MRU
T3-99,
TJ-103,
TJ-106 AFTER
61.20.04
TJ-317
AFTER
61.21.01
PROPELLER
GOVERNOR
61.21.01
T3-85,
TJ-89
PER
MOD CO
D8´•2477
61.21.02
T3-120
THRU TJ-168
61.21.03
T3-169
AFTER
POWER
PLANT
71.00.00
POWER
PLANT
71.00.00
LIST
OF
EFFECTIVE
PAGES
71.10.00
COWLING
71,10.01
FLAPS
COWLING
71.10.01
TK-1
THRR
TK-23,
TJ-3
MRU TJ-81
71.10.02
TK-24
THRU
TK-56,
T3-82
THRM T3-132
71.10.03
TJ-133
AFTER
73.00.00
ENGINE FUEL
AND
CONTROL
73.00.00
LIST
OF
EFFECTIVE
PAGES
73.30.00
INDICATING
73.30.01
FUEL
FLOW
SYSTEM
73.30.01
TK-1
MRU
TK-50,
TK-56,
TJ-3
THRU
TJ-125
EXCEPT
73.30.01
TJ-115,
TJ-118
03/13/98
Copyright
(c)1998
Aircrsft
Technical
Publishers
PAGE:
6
(RCR2102)
(BC
WD)

SECTION
TOPIC
73.30.02
TK-51
THRU
TK-55,
TJ-115
TMRU
TJ-118,
7;3-126
AFTER
73.30.03
TJ-286
AFTER
74,00.00
IGNITION
74.00.00
LIST
OF
EFFECTIVE
PAGES
74.30.00
SWITCHING
74.30.01
IGNITION
SWITCHING
77.00.00
ENGINE
INDICATING
77.00.00
LIST
OF
EFFECTIVE
PAGES
77.10.00
POWER
77.10.01
TACHOMETER
77.20.00
TEMPERATURE
77.20.01
RIGHT
CYLINDER
HEAD
AND
OIL
77.21.01
LEFT
CYLINDER
HEAD
AND
OIL
78.00.00
EXHAUST
78.00.00
LIST
OF
EFFECTIVE
PAGES
78.40.00
SUPPLEMENTARY
AIR
78.40.01
TURBINE
INLET
TEMPERATURE,
ENGINE
INDICATING
91.00.00
CHARTS
91.00.00
LIST OF
EFFECTIVE
PAGES
91.01.01
BOX
ASSEMBLY
ANNUNCIATOR
PC
BOARD
SCHEMATIC
91.10.01
CONNECTOR
NOSE
ACCESS
91.10.01
TJ-3
THRU TJ-7
91.10.02
T3-8
THRU
TJ-228
EXCEPT
T3-u0,
TK-1
THRU
TK-56
91.10.03
TJ-21O,
TJ-229
AFTER
91.11.02
CONNECTOR
LH
WING
ACCESS
91.11.02
TK-1
THRU
TK-42,
TJ-3
THRU
T3-106
91.11.03
TK-43
THRU
TK-56,
T3-107
THRU
TJ-132
91.11.04
TJ-133
AFTER
91.12.01
TK-1
THRU
TK-56,
TJ-3
THRU
TJ-132
91.12.02
T3-133
AFTER
91.13.01
CONNECTOR
LH
ENGINE
ACCESS
91.13.01
TJ-3
MRU
T3-7
91.13.02
TJ-8
THRU
TJ-114,
TJ-119
T1RU
TJ-125,
91.13.02
TK-1
THRU
TK-50,
TK-56
91.13.03
TK-51
THRU
TK-55,
TJ-115
THRU
T3-118,
TJ-126,
TJ-132
91.13.04
T3-133
AFTER
91.14.02
TK-1
THRU
TK-56,
TJ-3
THRU
T3-132
91.15.02
CONNECTOR
RH
WING
ACCESS
91.15.02’
TK-1
THRU
TK-56,
TJ-3
THRU
13-132
91.15.03
TJ-133
AFTER
91.16.02
CONNECTOR
RH
ENGINE
ACCESS
91.16.02
TK-1
THRU
TK-56,
TJ-3
THRU
TJ-132,
TJ-119
THRU
TJ-125
91.16.03
TK-51
THRU
55
TJ´•115
M~
TJ-118
TJ-126
AFT
91.17.01
TK-1
MRU
TK-56
T3-3
T3-132
91.18.01
CONNECTOR
AFT
FUSELAGE
91.18.01
TK-1
THRU
TK-56
TJ-3
M~
T3-132
03/13/98
Copyright
(c)1998
Aircra~ft
Technical
Publishers
PAGE:
7
(RCR2102)
(BC
0’44´•2
WD)

SECTION
TOPIC
91.18.02
TK-133
AND
AFTER
91.19.01
CONNECTOR
INSTRUMENT
PANEL
GROUNDING
91.20.01
CONNECTOR
FLOATING
PANEL
DISCONNECT
91.21.01
CONNECTOR
GLARESHIELD
91.22.01
CONNECTOR
FLOATING
PANEL
DISCONNECT
91.22.01
TJ-120
MRU
TJ-166
91.22.02
TJ-169
AND
AFTER
91.23,01
CONNECTOR
GWUZSHIELD
ANNUNCIATOR
91.23.01
TJ-169
MRU
TJ-316
91.23.02
TJ-317
AND
AFTER
91.24.01
TJ-169
AND
AFTER
j’~
END
OF
INDEX
’´•it~’
03/13/98
Copyright
(c)1998
Aircraft
Technical
Publishers
PAGE:
8
(RCR2102)
(BC
t~)

NI
FG.
INTRO

Caeechaaft
PRESSURIZED
TURBOCHARGED
Ci~ron
(i~t-on
56P
58PA
S8TC
58TCA
SERIALS
TJ-3 AND
AFTER
SERIALS
TK-I
’THRU
TK-56
G:
VVIRING~ DI~AGRAM.
COPYRIGHI
BEECH
1981
PIN
102-590000-233
Reissued:
July
3,
1981

PUBLISHED
BY
COMMERCIAL
PRO~CT SUPPORT
BEECH
AIRCRAFT
CORPORATION
WICHITA,
KANSi9S
61201
U. S.
A.
M´•mb´•rofG1MA
’1~
G´•n´•rolAvio~ion
A
Raytheon
Company
~I
Manufactur´•nAlrod~tion

RECORD
OF REVISIONS
MFG REV
NO
DESCRIPTION ISSUEDATE ATPREVDA‘ INSERTED
BY
E
IReissue
7/3/81 3/23/98 ATP/IM

LIST
OF
EFFECTIVE
REVISION~
AIways destroy
superseded
pages
when
you
insert
revised
pages.
Title
Page
........................................July 3,
1981
Logo
Page´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•..............................,......
"A"
Page.
....July
3,
1981
LOG
OF
REVISIONS
Part
Number
Date
Chapters
Affected
102-590000-23
July
19,
1974
ORIGINAL ISSUE
102-590000-23B
January
30,
1976
REISSUED
102-590000-23C
Rebruary
3,
1978
REISSUED
102-590000-23D
October
28,
1979
REISSUED
102-590000-233
July
3,
1981
REISSUED
E
NOTE:
A
list
of
the
effective
pages
will
be
found
in
the
front
of
each
chapter.
basic
publications
are
assigned
a
part
number which
appears
on
the
title
page
with
the date
of the
issue.
subsequent
revisions
are
identified
by
the
adGilion
ofa
revision
code
after
the
part
number.
Al
after
a
part
number
denotes,thq
first
revision to
the
basic
publication.
A2
me
second.
etc.
Occasionally,
it is
necessary
to
completely
reissue
and
reprint
a
publication
for
the
purpose
of
a
previous
issue
and
outstanding
renuons
thereto.
As
these
replacement
reissues
are
made.
the
code will
also
change
to
the
next
successive
letter
of
tl;e
alphabet
It
each
issue.
For
example.
B
for
the
rrrstreissue.
C for the
second
reissue.
etc.
When
ordering
a
handbook.
~ve the
basic
number,
and
the
reissue
code
when
applicable,
ifa
complete
upto~ale
publication
is
desired.
Should
only
revision
pager
be
required,
give
the basic number
and
revision
code lot
the
particular
set
of
revision
pages you
desire.

RECORD
Of
TEMPO~RARY
REVISIONS
AF~
P
ATP
REV
INSERT
DATE
REV
REMOVE
Rn/
NO
DESCRIPTION
ISSUE
DATE
1I~4TE
BY
REMOVED
INCOR
BY

BEECHCRAFT
BARON
58g
ANB
BARON
58TC
WIRING
dl~iRAM
~IANUAL
IIUTRODUCTION
LIST OF
PAGE EFFECTIVIN
CHAPTER
SECTION
SUBJECT
PAGE
DATE
INTRODUCTION-EFFECIIVIP(
1
July
3,
1981
INTROOUCTION
1
July
3,
1981
thru
21
July
3,
1981
"END"
INTRODUCTION-EFFECTIVITY
Page
1
July
3,
1981

BEECHCRAFT
BARON BARON
58iC
WIRING
MANUAL
INTRODUCTION
Group
Identified
by
different
colored divider
tabs.
These
are
primary
divisions
of
the
manual
that enable
broad
separation
of
content.
Typical
of this division
is
NOTE
the
separation
between
Airframe
Systems
and the
Aircraft Power
Plant.
Service
Publications
reissues
or
revisions
are
not
automatically
provided
to
the
holders of
this
SystemlChapter
The
van’ous
groups
are
broken
down
manual.
For
information
on
how
to
obtain
a
into
major
systems
such
as
Environmental
Systems,
revision
service
applicable
to
this
manual,
refer
Electn’cal
Power,
Landing
Gear,
etc.
The
systems
are
to
the latest
revision
of
8EECHCRAFT
Service
arranged
more
or
less
alphabetically
rather
than
by
Instructions
No. 0250-010.
precedence
or
importance.
They
are
assigned
a
number,
which becomes
the
first element of
a
standardized
numben’ng
system.
Thus,
the
element
"28"
The
BEECHCRAFT
Baron
58P/Baron
58TC
Wiring
of the number 28-00-00
refers
to
the
chapter
"Fuel".
Diagram
Manual
is
prepared
in
accordance
with
the
GAMA
Everything
concerning
the
fuel
system
will
be covered
in
Spec.
No.
2
(General
Aviation
Manufacturing
Association).
this
chapter.
It
also
meets
the
intent
of the
requirements
of the
ATA
Specification
100
(Air
Transport
Association
of
Amen’ca),
Sub-SystemlSectlon
The
major
systems
of
an
with
respect
to
the
arrangement
and
content
of
the
airplane
are
broken down into
sub-systems.
These
sub-
systemlchapters
within the
designated
chapter
numbering
systems
are
identified
by
the
second element of
a
system,
standard
numben’ng
system.
The number "40"
of
the
number 28-40-00
is
for the
indicating portion
of the
fuel
This
Wiring
diagram
manual
is
supplemented
by
the
system.
following
publications:
(1)
the
BEECHCRAFT
Baron
58PIBaron
58TC
Maintenance
Manual
PIN
102-590000-5,
Unit/Subject
The
individual units
within
a
sub´•system
(2)
the
BEECHCRAFT
Manufactured
Components
may
be
identified
by
the third element
of the standard
Maintenance
Manual
PIN
102-590000-21,
(3)
numben’ng
system,
such
as
28-40-01.
This
number
is
BEECHCRAFT
Parts
Catalog
102-590000-7
and
(4)
assigned by
the
manufacturer
and
may,
or
may
not,
be
BEECHCFIAFT
Baron
58TC
Wiring
diagram
manual
PIN
used and
will
vary
in
usage.
106-590000-13.
APPLICATION
NOTICE
Any
publication
conforming
to
the
GAMA
Spec
2
or
ATA
Beech
Aircraft
Corporation
expressly
reserves
100
formats
will
use
the
same
basic
numbering
system,
the
right
to
supersede,
cancel
and/or
declare
Thus whether the
manual
be
a
BEECHCRAFT
Baron
obsolete
any
part,
part
numbers,
kits
or
58P/Baron
58TC
Component
Maintenance
Manual,
or
a
publication
that
may
be
referenced
in
this
BEECHCRAFT Baron 58P/Baron
58TC
Wiring
Diagram
manual
without
prior
notice.
Manual,
the
person
wishing
information
concerning
the
indicating 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
sub-systems
CORRESPONDENCE
covered
in
the
chapter.
If
a
question
should
arise
concerning
the
care
of
your
For
example:
airplane,
it is
important
to
include
the
airplane
sen‘al
number
in
any
correspondence.
The
serial
number
appears
28-00
General
on
the
model
designation
placard
inboard
of the
n’ght
hand
28-10
Storage
flap
on
the
fuselage.
(Tanks,
cells,
necks,
caps,
instruments,
etc.)
28-20
Distribution
ASSIGNMENT
OF
SUBJECT
MA
TERIAL
(Fuel
lines,
pumps,
valves,
controls,
etc.)
The
content
of this
publication
is
organized
at
four levels:
28-30
Dump
Group,
SystemlChapter,
Sub-SystemlSection,
and
(If
in-flight dumping
system
is
UniVSubject.
installed,
it would
appear
here.)
INTRODUCTlON
Page
1
July
3,
1981

BEECHC9atiT
BARON 58P
AND´•1~ON
58TC
WIRING
DIAGRA’MaI;IANUAL
28-40
Indicating
components
are
identified
by
a
reference
designator
and
(Quantity,
temperature,
pres-
name
adjacent
to
each item.
The
diagrams
show the
sure,
etc.,
does
not
include
en-
terminals,
wire
numbers,
switches,
etc.,
in
a
manner
which
gine
fuel
flow
or
pressure.)
will make the
operation
of
each
component
easily
understandable.
The
curcuits
are
shown
consistent
with the
Carrying
this
example
further,
by
turning
to
the
Table
of
position
of
switches and conditions
noted
on
the
diagrams.
Contents
for
Chapter
28,
the
following
information
might
be
Symbols
used in the
wiring diagrams
appear
in
the
found within
the
list.
Introduction
of
this manual.
CHAPTER
SECTION
OPTIONAL
EQUIPMENT
SUBJECT
SUBJECT
PAGE
This manual does
not
in all
cases
differentiate
between
FUEL
28
optional
and
standard
equipment.
In
order
to
facilitate the
installation
of certain
wire harnesses
used
to connect
Indicating
28-40
op~bnal
equipment,
these
harnesses
will be
installed in all
airplanes.
Wires will be dead
ended
in
airplanes
that do
Fuel
Quantity
not
require
the
equipment.
TJ-3
and
after
28-40-01
1
thru
3
The
material
is
arranged
within
the
chapter
in
ascending
EQUIPMENT
LIST
numerical
sequence.
The
Chapter-System
Subject
number
and
page
number
are
found
at
the lower
outside
corner
of
A
listing
of
the
component
parts
accompanies
each
wiring
each
page,
d~ilagram
to
aid
maintenance
personnel
in
ordering
spare
re~lacements.
An
"R"
appearing
in
the
area
between
the
r~erence
designator
and
part
number
indicates
a
revision
EFFECTIVITY
to
the
original.
The
components
are
listed
in the order
of
aleha-numen’e
sequence
of
the
reference
designators.
The
LOG
OP.EFFECTIVE
REVISIONS
’’OWITS
PER
ASSY"
column
gives
the
quantity
of
that
co"mponent
which is
used in that
assembly.
The
letters
The
Log
of Effective Revisions
following
the title
page
of
"AR"
appearing
in
the
"UNITS
PER
ASSY" column
mean
the manual
lists
the revisions
currently
effective
for the
as
required
and
are
used in
cases
where
the
quantity
may
manual,
differ
according
to
optional
equipment.
The letters
"NP"
appean’ng
in the
"UNTTS PER
ASSY"
column
mean non
LIST
OF
PAGES
AND
TABLE OF
CONTENTS
procurable.
The
List of
Pages
and
fable
of
Contents
following
each The
components
are
listed
in the order
of
alpha-numeric
Chapter
Divider-Tab,
lists the
issue date
of each
page
that
sequence
of
the
reference
designators.
Further the
aircraft
is effective
for
that
chapter,
the titles
and,
if
applicable,
the
zone
in which
each
component
is
installed
is
provided
in
effectivity
of
the
circuits
covered
in
that
chapter.
the
listing.
Reference
to
the
zone
diagram
Figure
3
in
the
Introduction
will
enable
location
of
the
component
in
the
SERIALIZATION
airplane.
The
effectivity
of
each
wiring
diagram
and
el~ctrical
component
part,
unless
otherwise
specified,
is the
same
as
ALPHABFTICAL
INDEX
the
effectivity
of
the
manual,
as
given
on
the title
page.
If
the
effectivity
of
a
circuit
is
limited,
the
airplane
sen~als
for
An
alphabetical
index,
which
may
be
found in the
which the
circuit
is
effective
will be
given
in the
Chapter
liitroduction,
is also
provided
as
an
assistance in
locating
Index
Guide In
the
Introduction
and
the List
of
Pages
and
the
desired
circuit.
The
Alphabetical
index
provides
the
Table
of
Contents
for the
chapter
containing
the
circuit.
chapter
and
sub-chapter
in
which
a
circuit
appears.
WIRING
DIAGRAMS
ALPHA-NUMERIC
INDEX
To
facilitate
locating components
and
tracing
the
circuitry
All
parts
listed
in the
Win’ng
Diagram
Manual
are
arranged
of
individual
diagrams,
each.wire
is identified
by
the
wire
alliha-numer’cally
in the
Alpha-Numeric
Index. The
circuit
code
it
bears
in the
airplane.
The individual
circuit
in
which the
component
is found
is
listed
and the
reference
INTRODUCTION
Page
2
July
3,
1981

SiEQHCRAFT
BARON
581) AND BARON
58TC
WIRING
dlA"GRAIU~
MANUAL
designator assigned
to
the
component
in the
circuit
shown within
the
outline of
an
assembly
than
are
actually
accompanies
each
part
number in the
Alpha-Numeric
part
of
the
assembly.
Assemblies should be ordered
Index.
according
to
the
equipment
list since
it will
be
more
accurate
in
showing
the
components
of
the
assemblies,
Normally
only
electrical
components
are
shown
in the
MICROFICHE
AEROFICHE
win’ng
diagram
manual
so
there
may
be
fasteners and
other
non-electrical
components
within
an
assembly
which
The
General
Aviation
Manufacturers
Association
has
are
not
shown herein.
developed
a
specification
for
microfiche
and
registered
the
name
Aerofiche for
use
by
all
GAMA Members.
This
manual
may
be obtained in Aerofiche
form
from
your
local
WIRE
CODES
BEECHCRAFT
Aero
or
Aviation Centers
and International
Distributors
and Dealers.
The
wire codes used in the
BEECHCRAFT
BARON
58P/BARON
58TC
closely
follow
the
military
numbering
system.
Each wire
and cable is identified
by
a
combination
REFERENCE
DESIGNA~ORS
of
numbers and
letters
imprinted
on
the wire and cable
as
illustrated
in
Figure
i.
Each wire
or
cable is
identified
A
reference
designator
is
a
combination of
letters
and
within
3
inches of each
junction.
No code is
required
for
numbers
which
identify
a
particular
component
in this
short
wires
or
cables
less
than
3
inches in
length.
A
Wiring
Diagram
Manual.
A
reference
designator
is
nonmetallic sleeve
carrying
identification
will
appear
on
assigned
to
each
component
shown
on
the
wiring
wires where
imprinted
codes
cannot
be
affixed.
schematics.
Any
component
found
in
the
schematic
can
be
Identified
in
the
accompanying
equipment
list
by
its
Circuit
function
letters
indicate
a
relationship
to
a
particular
reference
designator.
An
example
of
a
reference
system
(noted
in
the list
of circuit function
designations.)
designator
follows:
Wire
numbers
are
provided
to
differentiate
between
wires
in
a
circuit.
CB101
CB
Identifies this
component
as a
circuit
A
wire
segment
is
a
conductor between
two
terminals
or
breaker,
connections.
Alphabetical
sequence
is
usually
followed,
Wife
segment
A
indicates
the
power
source,
B
next
CB101
Identifies it
as a
specific
circuit breaker.
segment,
etc.
ASSEMBLIES
SUBASSEMBLIES
The
wire
site number is used
to
identify
the
size
of
the
wire
or
cable.
Assemblies
are
identified
on
the schematic
by
name
and
by appearing
inside
the box which bears the
na~ne.
The
A
suffix
to
the
wire identification
code
(N)
identifies
any
equipment
list
identifies assemblies
by
name.
The
wire
or
cable
thatcompletes
the
circuit
to
ground
network.
nomenclature
of the
component
parts
of the
assembly
is
indented two
spaces.
The
part
number of
a
subassembly
Phase
letter
"A",
"B",
or
"C"
used
as a
suffix
identifies
will
be
listed and the nomenclature
indented
two
spaces,
three-phase win’ng
in
ac
systems.
component parts
of the
subassembly
will be
indented four
spaces.
The reference
designator
of
a
component
which
The
phase
letter
"V"
is
used
as a
suffix
identifying
an
belongs
to
an
assembly
begins
with
the reference
ungrounded
wire
or
cable
in
a
single phase
system.
designator
of
the
assembly.
A
typical
example
follows:
For
thermocouple
wire,
the
following
suffixes
are
A151
OtERHEAD
METER PANEL
ASSEMBLY
applicable.
A151A1
EMERGENCY LIGHT
CONTROL
ASSEMBLY
CHROM
Chromel
CONST Constantan
A1S1A1S1
EMERGENCY LIGHT CONTROL
ALML
Alumel
COP
Copper
SWITCH
IRON
Iron
ALUM
Aluminum
Assemblies
can
be
purchased complete
and
ready
for
A
Armaments
installation
or
they
can
be
purchased by
individual
B
Photographic
components.
In
some
cases
there
are more
components
C
Control
surfaces:
automatic
pilot
INTRODUCTION
Page
3
July
3,
1981

BEECMCRAFT
BARON
58P
AND
BAR,ON
58TC
WIRING
DIAGRARM
kiANUAL
D
Instruments
other than
flight
or
engine
instrument:
V
DC
power
for
AC
systems
ammeter,
landing
gear
position,
free air
temperature,
W
Warning
and
emergency
cabin
pressure,
etc.
X
AC
power
E
Engine
instrument:
fuel
now,
fuel
quantity,
tachometer,
Y
Armaments
special
systems
synchroscope,
etc.
F
Flight
instrument
G
Landing
gear:
actuator,
retraction,
warning,
downlock,
etc,
~P
52
A
4
N
H
Heating,
ventilating, deicing
CIRCUIT
FUNCTION
LETTERS
J
Ignition
K
Engine
control:
starter,
prop
pitch,
prop
synchronizer,
W1RE
NUMBER
etc,
WIRE
SEGMENT
LETTER
L
Lighting
WIRE
SIZE
(A.W.G.)
M
Miscellaneous
electric: windshield
wiper,
etc.
P
DC
power
SUFFIX
Q
Fuel
and
oil:
fuel
valves,
fuel
pump
motors,
throttle
sTo~scza
control,
oil
pumps,
etc.
R
Radio:
RC-radio
command,
RM-marker
beacon,
etc.
S
Radar:
SA-altimeter,
SS-search,
etc.
T
Special
electronics:
TK-telemetry,
TR-receivers,
etc.
Wire
Codes
U
Miscellaneous
electronics
(other
than
R,
S
or
T)
Figure
1.
INTRODUCTION
Page
4
Jury
3,
1981