19/23/24 ILLUSTRATED PARTS CATALOG P/N 169

Transcription

BEECHCRAFT
19, 23, 24 AND 24R SERIES AERO CENTER AIRPLANES
ILLUSTRATED PARTS CATALOG
INTRODUCTION
The purpose of this catalog is to provide
a method for i dent i fyi ng and ordering
spare parts for your BEECHCRAFT 819, C23,
C24R Aero Center Airplanes See the following paragraphs for detailed information. To order replacement parts for
electrical components refer to the applicab 1e BEECHCRAFT Wiring Diagram Manua 1,
or Shop Manual.
characters are effective for different
airplane serials.
FIGURE NUMBER INDEX GUIDE
The Figure Number Index Guide is a listing of figures by title and figure
number, in figure number order, of figures applicable to this catalog. This
Index is located in the Introduction and
starts on page 6.
ALAPHABETICAL INDEX
LIST OF
PAGES
EFFECTIVE REVISIONS AND
The List of Effective Revisions and Pages
fo 11 owing the Logo Page of the manua 1
lists the revisions currently effective
for the manual and a list of all effective pages with date. The list of pages
is in numerical order by figure number.
The Alphabetical Index is a listing of
component i terns or systems arranged . in
alphabetical order and referenced by figure number to. their location in the
Illustrated Parts List. This index is a
part of the Introduction and follows the
Figure Number Index Guide.
ALPHA-NUMERIC INDEX
NOTE
Neither Service Publications,
Reissues, nor Revisions are
automatically provided to the
ho 1ders of this manua 1 . For
information on how to obtain 11 ReV1Slon Service" applicable to
this manual, consult a BEECH..,
CRAFT Aero or Aviation Center or
International
Distributor or
Dea 1er, or refer to the 1a test
revision of BEECHCRAFT Service
Bulletin No. 2001.
This section of the catalog is an
Alpha-Numerical listing in tabular. form
of part numbers listed in the Illustrated
Parts List. All part numbers in the
Illustrated Parts List, except those coded as attaching parts, will appear in
this index.
Parts common to more than one figure or
assembly may be listed once for each time
it appears, in order to reflect the different figures.
The Alpha-Numeric
Introduction.
Index
follows
the
FIGURE NUMBERING SYSTEM
This BEECH CRAFT Parts Cata 1og uses the
figure number system. Some figure numbers are skipped because certain figure
numbers do not apply to this parts catalog and are therefore omitted. Other
numbers
are
reserved
for
future
additions.
This catalog contains figure numbers fol1owed by the 1etter 11 A'', "B", etc. This
indicates that the particular assembly or
in sta 11 at ion has been changed and that
the original figure number is effective
only on certain airplane serials and the
figure numbers containing alphabetical
ILLUSTRATED PARTS LIST
The Illustrated Parts List consists of
installations broken down into assemb1i es, sub-assenb 1i es, deta i 1 parts and
attaching parts. A separation symbol
(---*---) follows the listing of attaching parts to distinguish them from assembly breakdown.
If two assemblies are made up of a majority of identical parts, or the assembiles
are opposite,i.e., left and right hand,
the assembiles are listed together with
their detail parts listed as common for
INTRODUCTION
Page 1
May 11, 1984
BEECHCRAFT
both assemblies. In this case, only the
left or right hand part, but not both, is
indexed and illustrated, with the difference between 1eft and right hand parts
noted in the description co 1umn. The
Units Per Assembly column indicates the
number of detail parts required per
assembly, 11 NP 11 indicates the part or
assembly is Non-Procurable as a spare,
whi 1e 11 AR 11 indicates use As Required
rather than a specific quantity. The
notation 11 (see Figure) 11 indicates that
this assembly and its detail parts are
i 11 ustrated and broken down in another
figure.
When a number is shown in the Usable On
Code Column, refer to the Codes of Effectivity at the end of the listing of parts
for that particular figure to determine
airplane serial effectivity. Each figure
has its own distinct coding, i.e., the
code number denoting airplane serial
effectivity for one figure may not be the
same for another figure.
For convenience, each page of the Illustrated Parts List contains the figure
number in a lower corner.
HOW TO USE THIS CATALOG
I
INDENTURE COLUMN
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The example above shows the indenture system used to indicate parts in any given
assembly. By this indenture system, parts shown in column 2 are component parts of the
immediately preceding assembly, column 1; parts shown in column 3 are component parts
of the immediately preceding assembly in column 2, etc., through column 7. For example, the HG-83TN3/Tl0173E8 propeller assembly includes all parts listed starting after
index 3. Note that items 1 and 3 (attaching parts) are not part of the propeller
assembly. If part number 840-60 PROPELLER HUB SPIDER UNIT were ordered, it would
include item 4 and item 5. There may be times a part number consists of more than 16
characters; in that case, an asterisk (*) will appear'at the end of the part number
column and the remainder of the number will be in the description field. See above
example.
INTRODUCTION
Page 2
May 11, 1984
BEECH CRAFT
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HOW TO LOCATE A PART WHEN THE DESCRIPTION IS KNOWN
Consult the Alphabetical Index, for the figure in which the part is listed. Immediately preceding the listing of parts is an illustration for each figure; locate the
necessary part in the illustration (see step 1 in the example shown above). The index
number adjacent to the illustrated part will appear in the listing of parts in the column entitled 11 Figure and Index Number" (see step 2 above). Immediately to the right of
the index number will be found the required part number.
INTRODUCTION
Page 3
May 11, 1984
BEECHCRAFT
SUPERSEDED PART NUMBERS
Superseded Part Numbers will appear in
the Alpha-Numeric Index with the letter
"S 11 just to the 1eft of the number. They
should also appear in the description
field of the parts list, for example" ..
. BOLT/ supersedes AN3-7/". In this
instance, AN3-7 would be the superseded
number.
Delays in filling spare parts orders
often occur as a result of i ncomp 1ete
information being furnished with the original order,· i.e. lack of model designation and airplane serial number~ The
original order should always contain the
information indicated by check marks on
on the placard shown below, in addition
to
the
correct part
number
and
description or any pertinent information
which might further define the parts
required.
REVISED LINES
Revised Lines in the parts list are indicated by the letter 11 R" which indicates
that the line has either been revised or
added.
MANUFACTURED BY
BEECH AIRCRAFT
CORPORATION
HOW TO LOCATE A PART WHEN THE
~ART NUMBER IS KNOWN
If the part number is known and the
illustrated parts list must be consulted
for model applicability or description,
refer to the Alpha-Numer.ic Index, for the
figure and i tern number of the required
part. Refer to the example shown below.
T.C.
-
P.C.S
The serial placard shown above is located
on the main access door frame.
NOTICE
IMPORTANT WHEN ORDERING PARTS
Always use the COMPLETE manufacturer•s
pa !"t number 1i sted in the part number
co i umn. Be sure the 11 a i rp 1ane seri a 1
number" accompanies all spares orders.
INTRODUCTION
Page 4
May 11, 1984
Beech
Aircraft
Corporation
expressly reserves the right to
supersede, cancel and/or declare
obsolete any part, part numbers,
kits or publications that may be
referenced in this manual without prior notice.
BEECH CRAFT
WARNING
This parts cata 1og has but one
function; to facilitate ordering
replacement parts for the BEECHCRAFT 19, 23, 24 and 24R Aero
Center Airplanes.
Illustrations in this catalog
are to be used only as aids in
identifying parts and should not
be used as a rna i ntenance reference for reassembly.
MICROFICE/AEROFICHE
The General Aviation Manufacturers
Association has developed a specification for Mi crofi ce and registered
the name Aerofi che for use by a 11
GAMA Members. This manual is availab 1e on Aerofi che or on paper, and
either form of this manual may be obtained from BEECHCRAFT Aero or Aviation Centers and International
Distributors or Dealers.
Address a 11 orders to:
Commercial Product Support
Beech Aircraft Corporation
Kansas
67201
Wichita
U.S.A.
:WARNING. Use only genuine BEECHCRAFT or BEECHCRAFT approved parts obtained from
BEECHCRAFT approved sources, in connection with the maintenance and repair of
Beech airplanes.
Genuine BEECHCRAFT parts are produced and inspected under rigorous procedures to
insure airworthiness and suitability for use in Beech airplane applications.
Parts purchased from sources other than BEECHCRAFT, even though outwardly identical in appearance may not have had the required tests and inspections performed,
may be different in fabrication techniques and materials, and may be dangerous
when installed in an airplane.
Salvaged airplane ·parts, reworked parts obtained from non-BEECHCRAFT approved
sources, or parts, components, or structural assemblies, the service history of
which is unknown or cannot be authenticated, may have been subjected to unacceptable 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
BEECHCRAFT, unsuitable and unsafe for airplane use.
BEECHCRAFT expressly disclaims any responsibility for malfunctions, failures,
damage or injury caused by use of non-BEECHCRAFT approved parts. : EWARNING.
INTRODUCTION
Page 5
May 11, 1984
8 E E CHC R AF T
19, 23, 24, & 24R SERIES AERO CENTER AIRPLANES
I L L US T R AT E 0 P A R T S C AT AL 0 G
FUNCTIONAL GROUPS
=================
10
30
60
90
130
150
180
190
200
230
240
GENERAL
WING
CENTER SECTION
FUSELAGE
EMPENNAGE
FLIGHT CONTROLS
AUTOPILOT
VACUUM OR PRESSURE SYSTEMS
LANDING GEAR
HYDRAULIC POWER
POWER PLANT
280
310
340
350
390
410
450
470
480
490
FUEL SYSTEM
CABIN FURNISHINGS
OXYGEN SYSTEM
ELECTRICAL
INSTRUMENTS
CONDITIONED AIR
PRESSURIZATION
ALCOHOL ANTI-ICER SYSTEMS
FIRE EXTINGUISHER & FIRE
DETECTION SYSTEMS
AVIONICS
FUNCTIONAL GROUP INDEX GUIDE
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
10
TITLE
GENERAL
011
STATIONS DIAGRAM.
012
WING SKINS. • • • • • • • • • • • •
M-1 THRU M-1979 EXCEPT ~-1971,
MA•1 THRU MA-368,MB-1 THRU MB-865
012A
WING SKINS •• • • • • • • • • • • •
MC-2 THRU MC-536 EXCEPT MC-533
013
FUSELAGE SKINS •• • • • • • • • • •
M-1 THRU M-1284;MA-1 THRU MA-363;
MB-1 THRU MB-480
013A
FUSELAGE SKINS. • • • • • •
M-1285 THRU M-1979 EXCEPT M-1971
0138
013C
. .....
..........
FUSELAGE SKINS • • • •
. .. . .. .. . .....
MA-364 THRU MA-368
FUSELAGE SKINS. • • • . . . . . . . . . . . . . . . . .
MB-481 THRU MB-865
0130
FUSELAGE SKINS. • • •
• • ••
MC-2 THRU MC-536 EXCEPT MC-5~3
015
EXTERIOR MARKINGS • • • •
016
INTERIOR PLACARDS • • • • • • • • •
MB-1 THRU MB-480
016A
INTERIOR PLACARDS • • • • • • • • • • •
MB-481 THRU MB-865,MA-364 THRU MA-368
017
LOOSE TOOLS AND ACCESSORIES
019
AEROBATIC EQUIPMENT • • • •
M-1136 THRU M-1284;M8-331 THRU MB-480
019A
AEROBATIC EQUIPMENT • • • • • • • •
MB-481 THR.U MB-865
INTRODUCTION
PAGE 6
MAY 11, 1984
~
. . ......
. . . . .. . .
........
8 E E C HC R A F T
I L L U S T R A T E 0 P A R T S C A T A L 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
30
TITLE
WING
032
WINGS • • • • • • • • • • • • • • •
MB-1 THRU MB-865,MA-l THRU MA-368
032A
WINGS • • • • • • • • • •
032B
WHEEL WELL FAIRING. • • • •
• •••••••
MC-3llo~C-449,MC-452 THRU MC-536 EXCEPT MC-533
039
WING TIP • • • • • •
040
FLAP STRUCTURE • • •
041
AILERON AND TAB •
90
FUSELAGE
097
CANOPY STRUCTURE • • • • • • • • • •
M-1 THRU M-1284;MA-1 THRU MA-363
097A
CANOPY STRUCTURE • •
MB-1 THRU MB-4BO
097B
CANOPY STRUCTURE • • • • • • • • • • • • • • • • • • • •
MA-364 THRU MA-368oMB-48l THRU MB-865
MC-2 THRU MC-536oEXCEPT MC-533
098
LOWER CABIN STRUCTURE • •
103
AFT FUSELAGE STRUCTURE • • • • • • • • • • • • • •
M-1 THRU M~1979 EXCEPT M-1971 0 MC-2 THRU HC-190
MA-l THRU MA-3b8,MB-l THRU MB-B65
103A
AFT FUSELAGE STRUCTURE • • • • • • • • • • • • • • • • •
MC-191 THRU MC-536 EXCEPT HC-533
104
CABIN DOOR • • • • • • • • • • • • • • • • • • • • • • •
o
••••••
MB-1 THRU MB-480,MA-l THRU HA-363
M-1 THRU M-1284
104A
CABIN DOOR • • • • • • • • • • • • • • • • • • • • • • •
MB-481 THRU MB-865
MC-2 THRU HC-536 EXCEPT MC-533
MA-364 THRU MA-368
106
BAGGAGE DOOR.
106A
LARGE BAGGAGE DOOR. •
• • • •
HC-151 THRU MC-536 EXCEPT MC-533
llO
WINDSHIELD AND WINDOWS • • • • • • •
M-1 THRU M-1284;HA-1 THRU MA-363;
MB-1 THRU MB-480
llOA
WINDSHIELD AND WINDOWS. • • • • • •
..........
INTRODUCTION
PAGE 7
HAY llo 1984
8 E E C HC R AF T
I L L U S T R AT E D P AR T S C AT A L 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
TITLE
FUSELAGE ICDNTI
90
llOA
WINDSHIELD AND WINDOWS (CONTI
111
FIREWALL.
. ..... . .. . . .. . . . ... ..
EMPENNAGE
130
..
.......
&
......
132
HORIZONTAL STABILATDR
134
VERTICAL STABILIZER
135
RUDDER. • • • •
..
DORSAL FIN • •
FLIGHT CONTROLS
150
151
AILERON CONTROLS.
152
STA8ILATOR AND TAB CONTROLS
153
RUDDER CONTROLS •
154
RUDDER PEDALS • • •
M-1 THRU M-554
154A
RUDDER PEDALS • • • • • • • • • • •
MB-1 THRU M8-865,MA-1 THRU MA-368
MC-Z THRU MC-536 EXCEPT MC-533
155
CONTROL COLUJIW.
156
CONTROL WHEEL •
158
STABILATDR TAB CONTROL CONSOLE • •
159
ENGINE CONTROLS • • • • • • • • • •
M8-1 THRU MB-557tMA-1 THRU MA-368
MC-2 THRU MC-150,M-1 THRU M-1412,M-1415
M-1419,M-14Z3,M-1439 AND M-1447
159A
ENGINE CONTROLS • • • • • •
MB-558 THRU MB-865
Mt-151 THRU MC-536 EXCEPT MC-533
M-1413 THRU M-1979 EXCEPT M-1415,M-1419wM-1423t
M-1439,M-1447 AND M-1971
160
FLAP GEARBOX AND MOTOR.
161
FLAP CONTROL MECHANISM. • •
16U
FLAP MECHANISM~LECTRIC,. • • • •
• ••• • •
M-1236wM-1278 THRU M-1284;MA-362wMA-363;
MB-452 THRU MB-464
161B
FLAP MECHANISMtELECTRlC~PTIONAL' • • • • • • • • • • •
MB-465 THRU MB-865 wMA-364 THRU MA-368
INTRODUCTION
PAGE 8
MAY 11• 1984
........
......
. .. .. .. ..
..
... ... . .. . .. ..
. . . . . . .. • ..
..
8 E E C H C R A F T
I L l U S T R A T E D P A R T S C A T A L 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMSER
180
TITLE
AUTOPILOT
182
NEW-MATIC AUTOPILOT •
182A
3 AXIS AUTOPILOT/8-4/ •
190
VACUUM OR PRESSURE SYSTEMS
194
VACUUM SYSTEM • • • • • • • • • • •
M8-1 THRU MB-480
194A
VACUUM SYSTEM • • • • • • • • • • • • •
200
........
LANDING GEAR
202
MAIN LANDING GEAR • • • • • • • • •
MB-1 THRU M8-865,MA-1 THRU MA-366
202A
MAIN LANDING GEAR • • • •
203
MAIN GEAR WHEEL • • • • • •
• • • • • • • • • • •
MB-1 THRU MB-480
203A
MAIN GEAR WHEEL • • • • • • • • • •
M-1285 THRU M-1361;MA-364 THRU MA-368;
MB-481 THRU MB-521;MC-2 THRU MC-97
• ••••••
'2036
MAIN GEAR WHEEL • • • • • • • • • • • • • • • • • • • •
M8-522 THRU MB-865
204
MAIN GEAR DOORS • • • • • • • • • • • • • • • • • • • •
206
NOSE GEAR • • • • • • • • • • • • • • • • • • • • • • •
206A
~OSE
GEAR • • • • • • • •
• • • • • • • • • • • •
207
NOSE GEAR WHEEL • • • • • • • • • •
MB-1 THRU MB-541;MC-2 THRU MC-115
207A
NOSE GEAR WHEEL • • • • • •
MB-542 THRU M8-865
209
NOSE GEAR SHIMMY DAMPER • •
..........
..........
INTRODUCTION
PAGE 9
MAY 11, 1984
B E E C HC R AF T
19, 23, Zit, & 21tR SERIES AERO CENTER AIRPLANES
I L L U S T R AT E D P A R T S C AT A L 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
zoo
TITLE
LANDING GEAR CCDNT)
209
NOSE GEAR SHIMMY DAMPER ICONT)
210
NOSE GEAR STEERING. • • • • • • • •
MB-1 THRU MB-865eMA-1 THRU MA-368
210A
NOSE GEAR STEERING AND SHIMMY DAMPER.
211
LANDING GEAR RETRACT SYSTEM • • •
212
NOSE GEAR RETRACT LOCK MECHANISM.
·MC-2 THRU MC-536 EXCEPT MC-533
218
BRAKE • • • • • • • • • • • • • • •
M-1 THRU M-1361,MA-1 THRU MA-368,
MB-1 THRU MB-52lrMC-2 THRU MC-97
218A
BRAKE •
219
BRAKE PLUMBING. • • • • • • • • • •
M-1 THRU M-1Z81t;MA-1 THRU MA-363;
MB-1 THRU M8-lt80
219A
BRAKE PLUMBING. • • • • • • • • • •
MB-481 THRU MB-865,MA-361t THRU MA-368
220
MASTER CYLINDER •
M-1 THRU M-493
220A
MASTER CYLINDER • • • • • • • • • • •
M-it91t THRU M-1031t;MA-1 THRU MA-233 1
MB-1 THRU MB-261t
220B
MASTER CYLINDER • • • • • • • • • • • • •
M-1035 THRU M-1281t;MA-231t THRU MA-363;
MB-265 THRU MB-480
220C
MASTER CYLINDER • • • • • • • • • • • •
MB-481 THRU MB-865 ,MA~61t THRU MA-368
220D
MASTER CYLINDER • • • • • • • • • • • • • • • •
M-1035 THRU M-1979 EXCEPT M-1971 1 MA-231t THRU
MA-368rMB-273 THRU MB-865tMC-2 THRU MC-536
EXCEPT MC-533
.
221
BRAKE SHUTTLE VALVE
222
PARKING BRAKE VALVE •
223
LANDING GEAR SAFETY SYSTEM.
INTRODUCTION
PAGE 10
MAY 11, 198ft
•
•
•
•
•
•
•
•
•
•
•
•
•
MB-522 THRU MB-865
MC-9.8 THRU MC-536 EXCEPT MC-533
.. ........
. .. .. . ....
•
~
.. ....... .
......... .
....... .
.... . . . . . . . . . . . .. ......
.......
.. ......
• •
. ...
..
..
......... .
.....
B E E C H C R A F T
19, 23, 24, t 24R SERIES AERO CENTER AIRPLANES
I L L U S T R A T E 0 P A R T S C A T A l 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
230
TITLE
HYDRAULIC POWER
234
240
HYDRAULIC PUMP AND MOTOR • • • • •
POWER PLANT
241
POWER PLANT • • •
M-1 THRU M-554
241A
POWER PLANT • • • •
M-555 THRU M-1094
241B
MB-1 THRU MB-865
241C
MA-l THRU MA-368
2410
POWER PLANT •
• • • • • • • •
241E
POWER PLANT • • • • • • • •
243
COWLING • • • • • • • • • • • • • •
...................
M-1 "fHRU M-1284;MA-l THRU MA-363;
MB-1 THRU MB-480
243A
COWLING • • •
• ••••••••• • • • • • • • •
MB-481 THRU M8-B65,MA-364 THRU MA-368
244
BAFFLES • •
• • • • • • • • • • • • • • • • • • •
M-1 THRU M-554
244A
BAFFLES • • • • • • • • • • • • • • • • • • • • • • • •
M-555 THRU M-1094
244B
BAFFLES
•• • • • • • • • • • • • • • • • • • • • •
MB-1 THRU MB-480
244C
BAFFLES • • • • • • • • • • • • • • • • • • • • • • • •
MA-l THRU MA-363
2440
BAFFLES • • • • • • • • • • • • • • • • • • • • • • •. •
M-1095 THRU M-1284
244E
BAFFLES • • • • • • •
MA-364 THRU MA-368
244F
BAFFLES • • • • • • • • • -• • • • • • • • • • • • • • •
MB-481 THRU MB-865
245
EXHAUST SYSTEM • • • •
• • • • • • • • • • • • • •
M-1 THRU M-554;MB-l THRU MB-480
Z45A
EXHAUST SYSTEM. • • •
........ ...
INTRODUCTION
PAGE 11
MAY 11., 1984
8 E ECHC R AF T
19. 23• 24, & 24R SERIES AERO CENTER AIRPLANES
I L L U S T R A T E D
P A R T S
C A T A L 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
TITLE
POWER PLANT CCONT)
240
245A
EXHAUST SYSTEM ICONT)
M-555 THRU M-11»94
245B
EXHAUST SYSTEM. • • •
MA-l THRU MA-31t0 & MA-344
245C
EXHAUST SYSTEM. • • • • • • • • • • • • • •
M-1095 THRU M-1234 EXCEPT M-1143 & M-1155
2450
EXHAUST SYSTEM. • • • • • • • • • • • • • •
MB-481 THRU MB-865
M-1143.M-ll55,M-1235 THRU M-1979 EXCEPT M-1971
245E
EXHAUST SYSTEM. • • • • • • • • • •
MA-341 THRU MA-368 EXCEPT MA-344
248
PROPELLERS • • • • • • • •
..... ...... ....
FUEL SYSTEM
280
281
FUEL SYSTEM • • • • • • • • • • •
M-1 THRU M-554.M8-l THRU MB-865
28U
FUEL SYSTEM • • • •
M-555 THRU M-1094
Z81B
FUEL SYSTEM • • • • • • • • • • •
MA-l THRU MA-368
281C
FUEL SYSTEM • • • • • • • • • • • • • • • • • • • • • •
M-11)95 THRU M-1979 EXCEPT M-1971
283
ENGINE DRIVEN FUEL PUMP
M-555 THRU M-1094
285
FUEL BOOST PUMP • • • • • • • • •
M-1 THRU M-554;M8-1 THRU MB-320
285A
FUEL BOOST PUMP • • •
MA-l THRU MA-368
285B
FUEL BOOST PUMP • • • • • • • • • • • • • • • •
MB-321 THRU MB-B12.M-1095 THRU M-1604wM-1606
THRU M-1836•M-1838 THRU M-184l.M-1843.M-1844•
M-1846 THRU M-1852•M-1855•M-1857 THRU M-1859•
M-1864.M-1867•M-1868•M-1870
285C
FUEL BOOST PUMP • • • • • • • • • • • • • • • • • • • •
MB-813 THRU M8-B65.M-1605•M-1837.M-1842•M-1845
M-1853,M-1854.M-1856•M-1860 THRU M-1862•M-1865
M-1866•M-1869.M-1871 THRU M-1979 EXCEPT M-1971
287
FUEL TANK CAP • • • • • • • • • • • • • • • • • •
MB-1 THRU MB-865.MA-1 THRU MA-368
288
FUEL STRAINER • • • • • • • • • • • • • • • • • • • • •
INTRODUCTION
PAGE 12
MAY 11• 1984
.......
...........
...... .. ..... .
. ..........
.......... .
B E E C H C R A F T
19, 23t 24, & 24R SERIES AERO CENTER AIRPLANES
I L L U S T R A T E D P A R T S C A T A L 0 G
============================
FU~CT.
GROUP
SUB GROUP
NUMBER
TITLE
FUEL SYSTEM ICONT)
280
293
FUEL INJECTOR • • •
• • • •
MA-l THRU HA-368
294
fUEL FLOW DIVIDER AND NOZZLE • • •
MA-l THRU MA-368
310
... ........
CABIN FURNISHINGS
-..................
311
CABIN UPHOLSTERY.
M-1 THRU M-554
311A
CABIN UPHOLSTERY • • • • • • • • • • •
M-555 THRU M-1284;MA-l THRU HA-363;
MS-1 THRU MB-480
3118
CABIN UPHOLSTERY • • • • • • • • • • • •
M-1285 THRU M-1490oMA-364 THRU HA-368
MS-481 THRU MB-621oMC-2 THRU HC-190
311C
CABIN UPHOLSTERY • • • • • •
MB-622 THRU MB-865
MC-191 THRU MC-536 EXCEPT HC-533
312
CARPETS t FLOORBOARDS • • • • • • •
M-1 THRU M-1284;MA-l THRU MA-363;
MS-1 THRU MB-480
312A
CARPETS t FLOORBOARDS • • • • • • • • •
MB-481 THRU MS-865,MA-364 THRU HA-368
M-1285 THRU M-1979 EXCEPT H-1971
313
PILOT & COPILOT SEATS • •
314
PASSENGER SEATS • •
314A
PASSENGER SEATS • •
3148
FAMILY SEAT
MB-1 THRU MB-865
317
SIXTH SEAT • • • • • •
MA-124 THRU MA-368
MC-2 THRU HC-536
324
;ASIN FURNISHINGS/MISt/
324A
CABIN FURNISHINGS/WINDOW MOLDINGS/ • • •
. .. .
ELECTRICAL
350
354
FUSELAGE ELECTRICAL •
355
WING ELECTRICAL • •
....
INTRODUCTION
PAGE 13
MAY llw 1984
BE E C H C R AF T
I L L U S T R AT E 0 P AR T S C AT AL 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
TITLE
ELECTRICAL CCONTJ
350
356
BATTERY •
357
STARTER •
M-1 THRU M-1068
357A
STARTER •
358
GENERATOR •
M-1 THRU M-544
359
ALTERNATOR •• • • • • • • • • • • • • •
M-1095 THRU M-1283;MA-1 THRU MA-363;
MB-1 THRU M8-480
359A
ALTERNATOR. • • • • • • • • • • • • • •
MB-481 THRU MB-865 ,MA-364 THRU MA-368
359B
ALTERNATOR. • • • • • • • • • • •
M-555 THRU M-1094
360
TAXI LIGHT. • • •
361
ROTATING BEACON • •
364
ELECTRIC TRIM •
•
•
•
•
•
•
•
•
•
•
•
•
•
MB-1 THRU MB-865,MA-l THRU MA-368
.. .. . . . ...
.. ... ...... .... ....
.... .
INSTRUMENTS
390
.. . . . . . . . .
. .. . . ..... ...... ..
.........
..... ...
.... ....
...
........
391
FLOATING INSTRUMENT PANEL • • • ••
MB-1 THRU MB-480wM-1 THRU M-1284
MA-l THRU MA-363
392
INSTRUMENT PANEL. •
M-1 THRU M-554
392A
INSTRUMENT PANEL. • • • • • • • • • •
M-555 THRU M-1284,MA-l THRU MA-363
MB-1 THRU MB-480
3928
INSTRUMENT PANEL. • • • • • • • • • ••
M-1285 THRU M-1375,MA-364 THRU MA-368
MB-481 THR.U MB-530,MC-2 THRU MC-102
392C
INSTRUMENT PANEL. • • • • • • • • •• •
M-1376 THRU M-1454,MB-531 THRU MB-557
3920
INSTRUMENT PANEL. • •
MC-103 THR.U MC-154
392E
INSTRUMENT PANEL. • • • • • • • • • • • • • • • • • • •
MB-558 THRU M8-865;M-1413 THRU M-1979 EXCEPT
M-1415,M-1419wM-14Z3wM-1439,M-1447,M-1971
INTRODUCTION
PAGE 14
MAY llw 1984
B E E C H CR AF T
1 L l U S T R A T E 0 P A R T S C A T A L 0 G
============================
FUNCT.
GROUP
SUB GROUP
NUMBER
390
TITLE
INSTRUMENTS lCONT)
392E
INSTRUMENT PANEL lCONT)
394
PilOT AND STATIC PLUMBING •
410
CONDITIONED AIR
..
.
411
HEAT AND VENT • • • • • • • • • • • •
M-1 THRU M-554
4llA
HEAT AND VENT • • • • • • • • • • • • • • • • • • • • •
M-555 THRU M-900
411B
FRESH AIR SYSTEM • • • • • • • • • • • • • • • • • • • •
lo\A-1 THRU lo\A-363
lo\B-1 THRU MB-480
M-901 THRU M-1284
411C
CABIN FRESH AIR AND HEAT • • • • • • • • • • • • • • • •
MA-364 THRU MA-368
M-1285 THRU M-1879 EXCEPT 14-1875
MB-481 THRU MB-816 EXCEPT MB-814
MC-Z THRU MC-451 EXCEPT MC-311 & MC-449
4llD
CABIN HEAT DISTRIBUTION • •
M8-716tMB-731 THRU MB-865
M-1586,M-1600 THRU M-1979 EXCEPT M-1971
MC-Z93,MC-305 THRU MC-536 EXCEPT MC-533
411E
FRESH AIR SYSTEM. • • • • • • • • • • • • • • • •
MB-814,MB-817 THRU MB-865
M-1875ol8BO THRU H-1979 EXCEPT M-1971
MC-311tMC-449,MC-452 THRU MC-536 EXCEPT MC-533
415
FRESH AIR BLOWER • • • • • • • • • • • • • • • • •
MB-B14tMB-817 THRU MB-865
M-1875,M-1880 THRU H-1979 EXCEPT H-1971
HC-31l,MC-449,MC-451 THRU MC-536 EXCEPT HC-533
490
AVIONICS
490
EMERGENCY LOCATOR TRANSMITTER • • • • • • • • • • • • •
INTRODUCTION
PAGE 15
MAY llt 1984
.& E E
~ H ~ R A F T
& 2~ SERIES AERO CENTER AIRPLANES
19, 23,
z~,
ALPHA BE TICAL INDEX
COMPONENT ITEM
OR SYSTEM NAME
FIGURE
NO.
A
ACCELEROMETER
ACCELEROMETER
ACCESS OJOR PLACARD
ACCESSORIES AND TOOL~
ACTUATOR COVER
ACTUATOR,ELECTRIC TAB
ACTUATOR,FLAP
ACTUATORtLANOING GEAR
ACTUATOR,NOSE GEAR
ACTUATDRtNDSE GEAR
ACTUATOReNOSE GEAR
ACTUATOR,STADILATOR TAB
ACTUATOR,THROTTLE SW
ADAPTERefUEL FILLER CAP
AOAPTER,NOSE STEERING
AEROBATIC AIRPLANE
AFT ACCESS DOOR
AFT FUS~LAGE ~TRUCTURE
AILEkON CONTROL CABLE
AILERON PUSH ROO
AILERON ~K.IN
AILERON STRUCTURE
AIR BLEEu NOZZLE
AIR BLEED NOZZLE SHIELD
AIR BOX,CARBURETOR
AIR &OX,CARBURETOR
AIR DOX,INDUCTION
AIR DUCTeCARBURETOR
AIR TEMP INDICATOR
AIR TEMP INDICATOR
AIR VENT SCOOP
AIRPLANE LIFTING SLING
AIRPLANE LOG BOOK.
AIRSPEED INDICATOR
ALTERNATOR
ALTERNATOR DRIVE BELT
ALTERNATOR RECTIFIER
ALTIMETER INDICATOR
ALTITUDE HOLD
AMMETER
AMPLIFIERtAUTOPILDT
ARMeRUDDER CONTROL
ARMREST
ARMREST
ARMRI:ST,CABIN
ASHTRAY
ASSIST HANDLE
AUTOPILOT
DAR., TOW
BATTERY
BATTERY
BOX
INTRODUCTION
PAGE 16
MAY
lle198~
ITEM
FIGURE
NO.
B
19
392D
312A
17
100
3~
161A
2.11
2.11
2.12
206A
152
392.
2.81
210
19
13
103
151
151
12
~1
29~
294
2~1A
2~1
2.41C
2~1
392A
llOA
138
17
11
391
241A
2~18
359
391
182A
392.B
182A
us
312A
32~
311A
324
97
182
B
BAFFLESeENGINE
BAGeFLIGHT
BAGGAGE C.OMPARTNENT CARPET
B.AGGAGE DOOR
BAGGAGE ODOR
BAGGAGE DOOR CHAIN
BAGGAGE DOOR HMDLE
BAGGAGE DOOR LATCH
BAGGAGE DOOR L~
BALANCE AND ~EIGHT DATA
COMP~ENT
OR SYSTEM NAME
21t4
17
312
13A
lOb
lOb
lOb
106
lOb
17
17
356
350
BATTERY GROUND CABLE
BATTERY HOLD DOWN
BATTERY S~ITCH
&EACON LIGHT,ROTATING
BEARING,NOSE GEAR
BEECHCRAFT EMBLEM
8ELLCRA~,RUDDER PEDAL
&ELTeALTERNATOR DRIVE
8ELT,GENERATOR DRIVE
BELTeSEAT .
BLEEDER SCRE~tDRAKE
BLOIIIER.FRESH AIR
BONDING ~UMPEReENGINE
BOOST PUMP,Fua
BOX,tlATTERY
BOX,INDUCTION AIR
BRAKE ASSatBL Y
BRAKE HWSING
BRAKE MANUAL,GOODYEAR
8RAK.E MASTER CYLINDER
8RAK.E MASTER C:YLINDER
8RAitE PLUMBING
BRAKE SHUTTLE VALVE
BRAK.EeDISC
BRUSH,FUEL BOOST PUMP
BRUSH, GENERATOR
BRUSH,STARTER
BUTTON,FLAP RELEASE
BUZZER,STALL ~ARMING
356
356
356
361
206
15
154A
2418
241
31~
218
415
z•1a
281
356
2~1C
21BA
218
17
151t
220
219
219
218
285A
358
357'
161
97
c
CABIN AIR COHlRQL.
CABIN AIR DEFLECTOR
CABl... AIR VENT
CABIN AlRtHEAT AND DEFROST
CABIN ARMREST
CABIN COAT HOOK
CABIN CONSOLE COVER
CABIN DOOR
CABIN DOOR SEAL
CABIN ODOR SKIN
CABIN DOOR UPHOLSTERY
CABIN ENTRANCE STEP COVER
CABIN FURNISHINGS
CABIN HEAT CONTROL
CABIN HEAT DISTRIBUTION
CABIN HEAT VALVE
CABIN SKIN
CABIN STORII ~INDO~
CABIN UPHOLSTERY
CABIN VENT SCREEN
CABIN ~INDO~
CABLE ASSYeAILERON
CABLE ASSY,RUDDER
CABLE ASSY,STABILATOR
CABLE,BATTERY GROUND
CABLE,CARB HEAT CONTROL
CABLE,CONTROL COLUMN
CABLE,STABILAlOR TAB C:ONTROL
CANOPY STRUCT..aE
C:AP,FUEL
CAP,MASTER 8RAK.E tYL RESERVOIR
CARB AIR DUCT
392
111
13
241A
311A
3114
311A
104
104
13
311A
98
324
159A
4llD
41lC
13
104A
311
311A
97
151
153
152
356
l59A
155
1.58
97
281
220
241A
S E E C H C R A F T
& 2~ SERIES AERO CENTER AIRPLANES
ll.LU~TRATED
PARTS CATALOb
19, 23,
2~,
ALPHABETICAL INDEX
FIGuRE
NO.
C.UMPONt:Nl ITE~
01< SVSTi::M NAME
~ARo HEAT CONTROL
CARS HEAr CONTROL CA~Lc
CARd Hi::AT SH~O~O
(.ARo ricAT VALVE:
C.AitiSUR H :JR
C.ARoURET~~ AIR SOX
CARSURETUk HEAT CONTROL
CARO,OW~~R NOTIFICATION
CA~~i::TtO PANEL 1 CONTROL C.OLUMh
C.AK?~TS AND F~OORdOAKuS
C.e~TE:R s:CTION S~IN
CMAlNwbAbGAbt DOOR
C.riAlNtPA~~lNG
dRA~E
C.riAl~tPA~lN&
SRA~E
CHARTwHO~EPOWER SET
CHECK Ll~T,PILOTS
C.IGARETT~ LIGHTEK
CIKCUIT SREA~ER,FLAP
~IRCUIT ~REA~ER,FLAP
INDICATOR
MOTOR
CIRCUIT oREA~ER,GENERATO~
CIRCUIT BREA~ER 1 TAXI LlbHT
~OAT HOQ,..,CA61N
COMPASS
COMPASS,WINOSHIELO
COMPRESSOR,MAIN GtAK
COMPRESSuR,MAIN SHOC~ ASSOKbEK
COMPRESSUR,NOSE GEAR
CONE,TAIL
~PEED
PR~P
CONT«.OL c.lLUMN
~OLUMN CADL~
~OLUMN CARPEtED
CONTROL
PANEL
CONTROL COLUMN COVER
CONTROL IIIHEEL
CONTROL WHEEL MlC SWITCH
C.ONTKOI..tCABIN AIR
CONTROL,CA8IN Alit
CONTkO~tvASlN HEAT
CONTROL,CABIN HEAT
C.ONTkOL,CARSURETOR HtAT
CONTROL 1 LIEFROST
C.ONTROL,uEFRCJST
CONTKOL,FLAP
CONTROL,FLIGHT
CONTROL,FLIGHT LOC~
CONTROL 1 fRESH AIR
CONlROL,HIXTURE
C.ONTROL,PAR~
l.!)9A
1!)9A
COVC:R,PEDESTAL
COWLING, ENGINE
312
2 ..1
CYLINO~R.,8RA~E
218A
2 ..1
2..1
CYLINDERw8RAKE MASTER
CYLINDER,riYDRAULIC RETRACT
CYLINDER.,NOSc GEAR
CYLlNOER,NOSE GEAR
15..
2~1A
392
l7
312
312
8R~E
CONTROL,PROPELLE~
CO.'IIl K.OL, ~\UDDER
AND lAS
CONTROL,STABlLATOR TAB
CONTROL,IHROTTLE
CONTROLL:R,AUIOPlLOT
CONTROL,~TA61LATOK
2~3
202A
212
20C.A
0
l2A
lOo
15.. A
151.
313
CHAIR WitAPP ER
~ONTROL
FIGURE
NO.
c
c
C~~STANT
COMPONENT ITeM
OR SYSTeM NAME
17
17
392
lolA
lolA
392
3o0
3llA
392
392c
202A
202
ZOo A
10~
2.a
lSS
lSS
312
98
lSS
lSo
lS9A
392
OAMPER,SHIMMY
OECAL-lSEE PLACARD)
OECALtFUEL SELECTER
OECALtRAillO
DEFLECTOK,CABIN AIR
DEFROST CONTROL
DETECTOR 1 STALL WARNING
DIAGAAM,STATIONS
DIAPHRAGM 1 FUEL IN~ECTOR
DIRECTIONAL GYRO
DIRECTIONAL GYRO
DOOR,AFT AC.CESS
DOOil 1 8AGGAGt:
OODR.,8AbGAGE
OOOR 1 CABIN
OOOR,C.A8IN/A~R08ATIC
OOOR,COWLlNG
DOOR 1 FRESH AIR
OOOR..FU~L BOOST PUMP ACCESS
0001!. ,LANDIN~ GEAR
OOOR,LANOIN~ GeAR
DOORtLARGE BAGGAGE
DOOR,WlNG ACCESS
DOOR,WING ACCESS
OOkSAL FIN
DORSAL SKIN
DRAINoFUEL TA.NK.
DUMP VALVE CARPETED DOOR
209
15
281
1o
111
l59A
3~
11
293
39ZC.
19~A
l3
UA
106
10~
19A
2~3
~11
98
2~
32A
106A
32A
32
13..
13
281
312A
392
l!)'iiA
159
159A
392
lo1
1!)1
l1
..u
392
392
159
153
152
158
159
182A
CO.lL~R,O!L
2~1
COPILOT RUDDER PEDAL
COlfE:R,ACTUATOR
COlfeR,CA~lH CONSOLE
COVEKwCAolN ENTRANCE STEP
C.OVER 1 CONTROL COLUMN
C.OVEK.,EHGlNE: CONTROLS
COVEK.,FLlGHT CONTROL
COVER,HEATEO PITOT TUBE
151.
1o0
311A
98
'il8
3920
155
E
ELEC FLAP POSITION INDICATOR
ELEC TRIM SWITCH
ELEC TRIM TAB ACTUATOR SWITCH
ELECRICAL,FUSELAGE
ELECTRIC FLAP DRIVE
ELEVATOR TAS MHEEL
EMBLEM HOLDER
EMBLEM,CONTROL ~EEL
EMERGENCY LOCATOR XMTR
ENGINE
ENGINE BAFFLE DEFLECTOR
ENGINE BAFFLES
ENGINE CONTROLS
ENGINE CONTROLS COVER
ENGINE COWLING
ENGINE ORI YEN FIJEL PUN"
ENGINE MOUNT
ENGINE STARTER
EXHAUST RISER
EXHAUST STACK
EXHAUST ,ENGINE
CXTERIOR ·MARKINGS
392E
39ZO
3011-
35..
l61A
158
3llC
155
..90
2..1
21t4
21t4
159
392D
2~3
283
2 ..1
2..1
2~50
2~5a
2~5
15
ll
INTRODUCTION
PAGE 17
MAY lltl9M
8 E E C H C k A F T
19t 23t 2~, & 2~ SERIES AfRO CENTER AIRPLANES
ALPHABETICAL INDEX
COMPONENT ITEM
OR SYSTEM NAME
FIGURE
NO.
F
FAIRING,FWO DORSAL
FAIRING,NAIN GEAR
FAMILY SE.AT
FIREWALL
FLAP ACTUATOR
FLAP CONTROL
FLAP GEARBOX
FLAP INDICATOR CIRCUIT BREAKER
FLAP MOTOR
FLAP MOTOR CIRCUIT BREAKER
FLAP POSITION INDICATOR
FLAP SKIN
FLAP'STRUCTURE
FLAP SWITCH
FLAP WALKWAY SKIN
FLAPtELECTRIC DRIVE
FLIGHT CONTROL COVER
FLIGHT HOUR METER
FLOATING INSTRUKENT PANEL
FLDOR,CABIN
FLOORBOARD
FDOT,CHAIR
FORK AND AXLEtMAIN GEAR
FORK AND AXLE,NDSE GEAR
FRAME,BAGGAGE DOOR
FRESH AIR DOOR
FRESH AIR SYSTEM,CABIN
FRESH AIR VALVE
FUEL BOOST PUMP ACCESS QOOR
FUEL BOO$T PUMP BRUSH
FUEL BOOST PUMP PLUNGER·
FUEL BOOST PUMP,ELECTRlC
FUEL CAP
FUEL CAP ADAPTER
F.UEL CAP ADAPTER
FUEL FILLER CAP
FUEL FLOW DIVIDER
FUEL GUARD
.FUEL lNJCCTOR
FUEL l~ECTOR DIAPHRAGM
FUEL INJECTOR STRAINER
FUEL PRESSUaE GAGE
FUEL PRIMER
FUEL PUMP,ENGINE DRIVEN
FUEL QTY TRANSMITTER
FUEL QTY TRANSMITTER
FUEL SELECTOR DECAL
FUEL SELECTOR STOP
FUEL SELECTOR VALVE
FUEL SELECTOR VALVE STOP
FUEL STRAINER
FUEL STRAINER
FUEL STRAINER DRAIN VALVE
FUEL STRAINER PLUG
FUEL SYSTEM
FUEL TANK.
FUEL TANK
FUEL TANK DRAIN
FUEL TANK PLUG
FURNISHINGS,CABIN
FUSELAGE ELECTRICAL
FUSELAGE SKINS
FUSELAGE STRUCTURE,AFT
INTRODUCTION
PAGE 18
KAY llt1984
COMPONENT ITEM
SYSTEM NAME
DR
FIGURE
NO.
G
13~
202
31~8
111
160
161
160
161A
160
l61A
161A
12
~
161A
~
lolA
155
3928
391
GAGE,FUEL PRESSURE
GAGE,FUEL QUANTITY
GAGE,DIL TEMP
GAGEtVACUUM
GAGE, VACUUM
GEAR,ACTUATDR LANDING
GEARtMAIN LANDING
GEAR,NDSE LANDING
GEARBOX,FLAP
GEARED STARTER MOTOR
GENERATOR
GENERATOR BELT
GLARESHIELD
GYRO THROTTLE AND FILTER
GYRO,DIRECTIONAL
GYRO, DIRECTIONAL
GYRDtNlRIZDN
GYRO,NlRIZON
GYRO,VACUUN SYSTEM
391
392
391
194A
19~
211
202
206
160
357A
358
2~1
392
182
194
392C
392C
19~
194
98
312
313
202
206
97
~11
~11
~11
98
285A
285
285
281
·281
32
287
291.
281
293
293
293
391
281
283
281
355
281
2818
281
281
281
288
H
HANDBOOK,PILOTS OPERATING
HANDLEtBAGGAGE DOOR
HANDLE,STDRM WINDOW
HARNESS,SnDULDER
HATSHELF
HEADREST
HeAT AND.DEFROST,CABIN AIR
HEAT SHROUD.CARBURETOR
HEATED PITOT
HEATER MUFFLER
H£4TER SHROUD
HDLDER,EM8LEM
NlRIZON GYRO
HORIZON GYRO
HORIZONTAL Sl"ABIUTDR
HDRN.STABIUTOR TAB
HDRN.STALL IIIARNING
HOURMETER.FLIGHT
HOUSING.BRAKE
HDUSINGeMAIN GEAR
HDUSINGtNOSE LANDING GEAR
HUB,PRDPELLEk
HYDRAULIC MANIFOLD
HYDRAULIC PReSSURE SWITCH
HYDRAULIC PUMP
HYDRAULIC RETRACT CYLINDER
HYDRAULIC SHUT OFF VALVE
HYDRAULIC SHUTTLE VALVE
HYDRAULIC SYSTEM
17
1D6
110
31~
32~A
324
241A
245
324
2~5D
2458
311C
392C
194
132
132
97A
392B
218
202A
206
2~8
211
211
211
202A
211
211
211
281
2818
281
32
l2A
281
2818
32~
3~
13
103
IGNITION KEY
IGNITION SWITCH
INDICATOR,AlR TERP
INDICATOR,ELEC FLAP POSITION
INOICATDR.FLAP POSITION
INDICATOR.MIXTURE CONTROL
INDICATOR,RATE OF CLIMB
INDICATOR,SUCTIDN
INDICATOR t TURN COORD INA TOR
INSTRUMENT LIGHT LENS
17
392
392A
392E
lolA
3928
3928
3928
391
97A
8 E E C H C R A F T
& ~~ SERIES AERO CENTER AIRPLANES
I L L US TR A T E 0 P AR T S C AT A L 0 G
19, 23,
2~,
ALPHABETICAL INDEX
COMPONENT ITat
OR SYSTEM NAME
FIGUKE
NO.
COMPONeNT lTE:M
SYSTEM NAME
OR
fiGURE
NO.
M
INSTRUMENT PANEL
INSTRUMENT PANEL,AEROSATIC
INTERIOR PLACARDS
392
19A
1o
L
L,G CIRCUIT BREAKER SWITCH
LANDING ~EAR ACTUATOR
LANDING GEAR eRAKE,MAIN
LANUING ocAR OOOR,MAIN
LANDING bfAR DOWNLOCK,NOS~
LANDING GEAR RETRACT
LANDING GEAR SAFETY SYSTEM
LANDING GEAR SWITCh
LANDING GEAR SWITCH ACTUATOR
LANDING ~EAR UPLOCK,MAIN
LANDING GfAR,MAIN
LANDING GEAR 1 MAIN
LANDING LIGHT
LANDING LIGHT SWITCH
LARGE BAGGAGE DOOR LATC~
LARGE BAGGAGE DQOR WINDOW
LATCH,BAGGAGE DOOR
LATCH,CABIN DOOR
LATCH,LARGE BAGGAGE DOOR
LENS,ROTATING BEACON
LICENSe CHARACTERS
LIGHT,LANillNG
LIGHT,POST
LIGHT,ROTATING BEACON
LIGHT ,RUOOER
LIGHT,STo(()BE
LIGHT,~ING NAVIGATION
LIGHT,iUNG TIP
LIGHTER,CIGARETTE
LOCK,BAGGAGE DOOR
LOCK,CABIN DOOR
LOCK,FLIGHT CONTROL
LOCKwNOS~ GEAR RETRACT
LOCK,STORH WINDOW
LOCK,STORM WINDOW
LOG BOOK,AIRPLANE
LOOSE TOOLS
LOWER CA3IN STRUCTURE
2.2~
211
2.11;
zo•
ZOo A
Zll
2.23
2.23
4!2.3
211
2.02
~ZA
32
392.
lOt:> A
lOoA
10o
:&.o-.
lCioA
3o1
15
32
392&
1..34
135
39
39
32
392
lOo
lOit
:nus
15
220
uo
392.£s
15o
l92
2~1A
159
3928
15
32.. A
2.3...
l~l
z...s
H
NAVIGATION Ll~T ~WITCH
NAVIGATION LIGHTS
NOSE GEAR ACTUATQR
NOSE GEAR A~TUATOR
NOSE bfAR afAKlNG
NOSE GEAR CDMP~cSSOR
NOSE GEAR CYLINDER
NOSE GEAR ~fLINDER
NO~E GEAK fORK ANO AXLE
NOSE ~cAR RETRACT LOCK
NOSE ~cAR STEERING
NOSE GEAR wHEEL
NOSE ~G OOWNLOCK
NOSE ~- Ll,.IT SWITCH
NOSE LANDING GEAR
NOSE UNUING GEAR HOUSING
NOSE WHEEL AND TIRE
NOSE WHEEL STEERING
NOZZLE,AIR BLEED
392A
39
2.11
212
201:>
ZOI:>A
luoA
212
2.01:>
2ll
2.0/:>A
2.07
lOb A
20oA
2.01:>
201:>
zoo
210
2.9<'1-
11
212.
110
97
l7
l7
98
M
MAGNETO
KAIN GEAR COMPRESSOR
MAIN GEAR FORK AND AXLE
MAIN GEAR ~DUSING
MAIN GEAR LIMIT SWITCH
MAIN GEA~ RET~ACT ARM
MAIN GEAR UPLDCK
MAIN GEAR WHEEL
MAIN LANDING GEAR
MAIN SHOCK ABSORBER COMPRESSOR
MANIFDLD,HYORAULIC
MANUAL 1 CONTINENTAL ENGINE
MANUAL,GUODYEAR BRAKE
KANUAL,LYCOMING ENGINE
MANUAL,NAVATEER MODEL
MANUAL,SERVICE INSTRUCTIONS
MAP BOX
MAP POCKET
"ARKINGS 1 EXTERIOR
MAST~R dRAKE CYL RESE:RVOIR CAP
MASTeR CYLINO~,BRAKE
"ECHANlCAL TACI1Qio\ETER
"IC ~~lTCH,CONTROL WHEEL
NICROPHONE,kAOIO
•UXTURE: CONTROL
MIXTURE C.ONTkOL.
"IXTURf CONTROL INulCATOR
"ODEL DE~IGNATION PLATE
MOL&liNGS, WINDOW
"OT0k 1 RETRAC.T PU~P
I'IOUNT 1 ENGINE
"UFFLER,ENGINE
0
OIL COOLER
OIL PRESSURe GAGE
OIL TEMP ~ULB
OIL TEMP GAGE
OVERHEAD LIGnT S~ITOH
OVEattEAD PANEL
OWNERS MANUAL
z•1
391
2.~1
391
97
91
17
2~1
202A
202
202A
202A
202A
211
203
32A
202
Zll
17
17
17
l7
11
392
p
PANEL,FLOATING INSTRUMENT
PARKING BRAKE Ct1AIN
PARKING BKA~ VALVE
PARKING BRAKE VALVE LEVER
PARTS CATALOG
PASSENGER SEATS
PEDAL.RUDOER
PEDESTAL COYER
PEDESTAL SKIRT
PILOT AND COPILOT SEATS
PILOTS OPERATING HANDBOOK
PITOT AND STATIC PLMB
PITOT HEAT SWITCH
PITOT MAST
391
154
2.22
22.2
17
314
154
312.
312
313
17
39~
392A
394
INTROOUCTION
PAGE 19
NAY 11,1984
19,
2~,
B E f C H C R A F T
2•• & 2~ SERIES AERO CENTER AIRPLANES
ILLUSTRATED
PARTS
CATALOG
ALPHABETICAL INDEX
COMPONENT ITEM
OR SYSTEM NAME
FIGURE
NO.
312A
15
1o
15
2818
2818
3118
3928
2•1
281
2~
2•1
159
248
17
211
23'tl9't-
R
RADIO DECAL
RATE OF CLIMB INDICATOR
REFLECTOR,NAVIGATlON LIGHT
REGULATOR, VOLTAGE
RESERVOIR,BRAKE FLUID
RETRACT ARM,MAIN GEAR
ROO,SEAT ADJUST
ROTATING BEACON
RUDDER
RUDDER CONTROL ARM
RUDDER CONTROLS
RUDDER PEDALtCOPILDT
RUDDER PEDAL,PILOT
RUDDER SERVO
RUDDER SKIN
RUDDER TIP
RUDDER TIP SKIN
RUDDER TRIM TAB
lo
39ZS
~9
241A
2l9
202A
313
1~
us
135
153
lS'tlS't18ZA
13
135
13A
13
s
SAFETY SYSTEM,LANDING GEAR
SCOOP,.UR VENT
SEAL,CABlN DOOR
SEAT AD.IUST ROO
SEAT BACK STOP
SEAT BELT
SEAT COVER,PROTECTIVE
SEAT TRACK
SEAT ,FAIULY
SEAT,SIXTH
SEATS, PASSENGER
SEATSePILOT AND COPILOT
SERVO,AILERON
SERYOeRUODER
SHAFTeTACHOMETER
SHlELD,AIR BLEED NOZZLE
SHIMMY DAMPER
SHOCK ABSORBER,MAlN
SHOCK ABSORBER tHOSE
SHOULDER HARNESS
SHROUD t C.ARB HEAT
SHUTTLE VALYEeBRAKE
INTRODUCTION
PAGE 20
MAY llel984
FIGURE
NO.
s
p
PLACARD,ACCESS DOOR
PLACAROS,EXTcRIOk
PLACARDS, INTERIOR
PLATE,MOOEL DESIGNATION
PLUG,FUEL STRAINER
PLUG,FUEL TANK
POCKET,MAP
POST LIGHT
POWER PLANT
PRIKC:R,FUcL
~ROP,CONSTANT SPEED
PROPELLEi<.
PROPELLER CONTROL
PROPELLEK HUB
PROTECTI~t: SEAT COVER
PUMP ,HYDRAULIC
PUMP,HYDRA\JLIC
PUMP,VACUUM
COMPONENT ITEM
OR SYSTEM NAME
223
138
lOit
313
313
31't11
98
3148
3l7
31.
313
l82A
l8ZA
2't-1A
SIXTH SEAT
SKIN, AILERON
SKIN, CABIN
SKIN,CABIN DOOR
SKIN, FLAP
SKIN,RUDOER
SKIN,RUDOER TIP
SKIN,STABILATOR
SKIN,VERTlCAL STAB
SKINSeFUSELAGE
SKINS,WING
SKIRT,PEDESTAL
SPARK PLUG
SPEAKER,OVERHEAD
SPINNERtPROPELLER
STABlLATOR
STABILATOR CONTROL
STABIUTOR SKIN
STABILATOR TAB
STABIUTOR TAB CA&LE ASSY
STABIUTOR TAB CONTROL
STABIUTOR TAB CONTROL CABLE
STABILATOR TAB HORN
STABILATOR TAB TIP
STAIULATOR TIP
STA&ILIZER.VERTICAL
STALL ~ARNIMG &UZZER
STALL WARNING DETECTOR
STALL WARNING HORN
STARTER
STARTER
STARTER MOTDR.GEARED
STARTER SOLENOID
STATION DIAGRAM
STEERING,NOSE GEAR
STEP.ENTRANCE
STOP • CABIN DOOR
STOPeSEAT SACK
STOP,SEAT BACK
STORH Ill INDOIII
STRAINER, FUEL
STRAINERwFUEL
STRAINEReFUEL IN.IECTOR
STROBE LIGHT
STRUCTURE,AFT FUSELAGE
STRUCTURE,FLAP
STRUCTURE.LDWER CABIN
STRUCTURE,STABILATOR
STRUCTURE.UPPER CABIN
STRUCTURE eWING
SUCTION INDICATOR
SUN VISOR
~ITCH,ELEC TRIM
SWITCH• ELEC TRIM TAB ACTUATOR
~ITCHeFLAP
~lTCH,trtDRAUUC
PRESSURE
317
12
13
13
12
13
13A
l3
13
13
12
312
241
97
241
132
152
l3
132
152
158
158
132
132
l3Z
134
97
355
97A
357
24lA
357A
241
ll
200A
98
104
314A
313
97
288
281
Z93
39
103
•o
98
132
97
32
3928
32.
3920
304
lolA
211
SWITCH. IGNITION
SWITCH,VG CIRCUIT BREAKER
392
Z9lt
209
~ITCH,LANDING
202
SWITCHeLANOING LIGHT
~ITCH,KAIN GEAR LIMIT
SWITCH,NAVIGAnON LIGHT
~ITCH,NOSE VG LIMIT
SWITCH,OYERHEAD LIGHT
Z23
392
Z02A
39ZA
206A
206
314
z•1
221
GEAR
223
97
B
c
f
C H C K A F T
!9, 23, 24r ~ 24R SERIES AERO CENTER AIRPLANES
I L L U S T R A T f u P A R T S C A T A L 0 G
ALPHABeTICAL INDEX
CJMPONC:NT ITclt
SYSTEM NAMe
0.-<.
FIGURE
NO.
FIGURE
NO.
v
s
SWITCHrPlTOT HEAT
SwiTCHrTAXI LlbrlT
.>oiiTCHc!>rMASTER
392A
3ou
.:.92
T
lAB
fAd
CIJMPONCN T ITEM
SYSTEM NAME
OR
CONT~OL,STABlLATOR
WHEE~rELcVATO~
TAooAlLE~ON
158
!58
41
TABoELECTRlC ACTUATOR
TAi:i 1 STAiHL.AIL)R
TACHUME:TtK.
TACHuMcl:R SnArl
TAIL. CON;
TAlL. CONE
TANK,FUEL.
TAXI LlGHT
TAXI LlbnT CIR~UIT oREAKcK
TAXI Llb~T SRITCH
THKOTTL.E AN~ FILTERoGYR~
THkOTTLE CuNTkOL
TnKOTTLE CONTROL
TriRuTTLE CONTROL. CABLE
Tlt: DOWN LUG
TIPoRUilOt::~
TIP, STABILATOR
TIP,STABlLATOK TAB
TlPoVERTICAL STABlLllfK
TIP,WlNb
36't
132
392
2~1A
103
l3C.
.:.2
360
360
360
182
159
.2~1A
159A
32
135
132
132
13C
39
32A
Tl~oi'IING
TlREoMA1:t GEAR
Tli<.Eofi&OS<:. GEAR
TOW BAR
TRANSHITIE:R,C:McRbENCY
TRANSMITTER 1 FLAP POSITION
TRANSMITTC:R,FUEL WUANTITY
TRANSMITTcRoFUtL. ~UANTITY
TiUM TAih~UilOt:M.
TRIMoWINuSHIELu·INTERIOR
TUkN COO~INATOR INDICATOR
202
VENT,CASIN EXHAUST
VERTICAL STAB S~lN
VERTICAL STABILIZeR
VERTICAL STABILIZER TIP
VOLTAGE REGULATDk
VOLTAGE REGULATOR
97A
13
134
13C
241
241A
w
WALKWAY,FLAP
IIIALKWAY',WING
IIIHEEL WELL FAIRING
WHEE:L,CONTRDL
WHEEL,MAIN GEAR
WHEEL ,NOSE GEAR .
WINOLAC~tCASlN DOOR
WINDOW MOLDINGS
llllNDOw,tAolN ODOR
WINDOW,~A61N STORM
WIN~OIIIoLARGE 8AGGAGE DOOR
WINDOWS AND WINDSHIELD
WINDShieLD COMPASS
IIIINuSHIEL.O INTERIOR TRIM
WING ACCE~S OOOk
IIIING ELECTRICAL
WING SKINS
oUNG STRUCTURE
llllNG TIP
IIIING TIP
WING TIP LIGHT
IIIRAPPER,CHAIR
.a
12
328
155
ZCi3B
ZOo
104
llOA
104
104A
lOoA
110
392E
llOA
32
355
12
32
32A
39
32
313
ZOo
l7
49v
1~1A
2&1
3"55
13
llOA
391
u
UPrlOLSTEK.Y,CABIN
uPnOL.STE~Y,CABlN
OOOK
v
VACuUM P""'P
VACUUM R:L.IEF VALVE
VACUUM SYSH:M
VALVEoBRAKE SHUTTLE
VALVE,&RAKE SHUTTLE:
VALVEoCABlN HEAT
VAL.VEoCA:(.B HEAT
VA.LVE,DEFROST
VALVEoFkt:SH AIR
VALVEoFUEL STRAINER ORAlN
VALVEoHYuRAULIC SHUT OFF
VALVEoHYORAULIC SHUTTLE
VALVE 1 PAKKlNG BRAKE
~AL.VEoVACUUM RELIEF
VALVEoVA~UUM RELIEF
VENToCASIN AIR
1~
194A
1~
219
221
~llC
2~1
4ll
~11
281
2ll
2ll
222
191t
194A
13
INTIUJDl£TlON
PAGE iU
MAY 11,1984

19/23/24 ILLUSTRATED PARTS CATALOG P/N 169

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