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JUL 01/17INTRODUCTION-LOEP

BARON B55, E55, 58 & G58 ILLUSTRATED PARTS CATALOG

List of Effective Pages

CH-SE-UN-FIG PAGE DATE

Introduction-LOEP 1 Jul 01/17

Introduction 1 thru 12 Jul 01/17

Beechcraft CorporationBARON B55, E55, 58 & G58 ILLUSTRATED PARTS CATALOG

PAGE INTENTIONALLY LEFT BLANK

INTRODUCTION Page 1JUL 01/17


00-00-00

INTRODUCTION

1. INFORMATION

Reissues are automatically provided to the subscription holders of the manual. Additional publications arelisted on the web at http://pubs.beechcraft.com. For more information on these publications, or to checksubscription status, contact the Technical Manual Distribution Center (TMDC) at 1.800.796.2665 or316.676.8238, fax 316.671.2540, E-mail [email protected].

An Interactive Maintenance Library (IML) contains selected Manuals in a digital format. This manual, alongwith others, is available on CD-ROM and online. A PDF version is available for purchase on single CD.

Help Line phone support for IML CD and Online Users is available 8:00 AM to 4:30 PM Central Time (US andCanada). During off-hours, leave a detailed voicemail message. Calls will be returned within one businessday. Contact the Help Line at 1.800.240.2959 or 1.316.676.3053, E-mail [email protected].

Comprehensive user guides for the IML CD and Online manuals are available on the Beechcraft Corporation(BC) Technical Publications website http://pubs.beechcraft.com. Illustrated and detailed procedures for usingIML features are included in the downloadable user guides.

This document is prepared, issued and revised by BC for the exclusive use of its customers and is intendedto be used for provisioning, requisitioning, storing and issuing line replaceable airplane parts. The contentsare proprietary to BC and its customers and are subject to change. The use of any part of this document byany other person or persons, or for any other purpose without the prior consent of BC is expressly prohibited.This document is produced to support the configuration of the airplane at the time of delivery to the originalcustomer and does not necessarily reflect the current configuration of any specific airplane.

In addition to this manual and its subsequent revisions, additional maintenance information is published in theform of BC service bulletins. The information contained in these service bulletins is an integral part of, and isto be used in conjunction with, the information contained in this manual.

A. General

The Baron Illustrated Parts Catalog (IPC) is prepared in accordance with the requirements of ATA 2200(Air Transport Association of America) with respect to the arrangement and content of the System/Chapters within the designated numbering system. This manual is supplemented by the followingpublications:

• The Baron Maintenance Manual, P/N 55-590000-13

• The Baron G58 Maintenance Manual Supplement, P/N 58-590001-1

• The Baron 58 Electrical Wiring Diagram Manual, P/N 96-590011-29

• The Baron 58 Electrical Wiring Diagram Manual, P/N 96-590010-39

• The Baron E55/58 Electrical Wiring Diagram Manual, P/N 96-590010-15

• The Baron G58 Electrical Wiring Diagram Manual, P/N 58-590001-3

• The Baron G58 Avionics Wiring Diagram Manual, P/N 58-590001-5


Page 2JUL 01/17 INTRODUCTION

• The Baron 55/56/58 Long Inspection Guide, P/N 118662

• The Baron 55/56/58 Short Inspection Guide, P/N 98-39097

• The Baron 55/56/58 Continuing Care Inspection Guide, P/N 98-36712

It shall be the responsibility of the owner/operator to ensure that the latest revision of the publicationsreferenced in this manual are utilized during operation, servicing and maintenance of the airplane.

Beechcraft Corporation expressly reserves the right to supersede, cancel and/or declare obsolete anyparts, part numbers, kits or publications that may be referenced in this manual without prior notice.

WARNING: Use only parts obtained from sources approved by Beechcraft Corporation , in connection with the maintenance and repair of Beechcraft Corporation airplanes.

Genuine Beechcraft Corporation parts are produced and inspected under rigorous procedures to insure airworthiness and suitability for use in Beechcraft Corporation airplane applications. Parts purchased from sources other than those approved by Beechcraft Corporation, even though outwardly identical in appearance, may not have 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 sources not approved by the Beechcraft Corporation 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 the Beechcraft Corporation, unsuitable and unsafe for airplane use.

Beechcraft Corporation expressly disclaims any responsibility for malfunctions, failures, damage or injury caused by use of parts not approved by the Beechcraft Corporation.

B. Correspondence

If a question should arise concerning the care of your airplane, it is important to include the airplaneserial number in any correspondence. The serial number appears on the model designation placard.Refer to Chapter 11 for placard location.

C. Publications Change Request (PCR)

If an irregularity or missing information is noted, the user of this manual may access a PCR form at http://pubs.beechcraft.com. Instructions on how to submit a PCR are included on the web page.

D. Variation Numbers

Some parts on the airplane may be identified with -6xx, -7xx, -6xxx, -7xxx, -6 U, -006 U, -0006 U partnumber suffixes. These suffixes (dash numbers) are used when a part has been produced to aconfiguration different than to the Engineering. Examples of these differences can include but are not



limited to an additional trim allowance, holes undrilled, and assemblies without all the attaching parts orwith additional parts. These dash numbers may not necessarily be in the Illustrated Parts Catalog (IPC)therefore, when ordering parts, it is important to quote the part number as found in the IPC.

2. MANUAL LAYOUT

A. Front Matter

(1) Title Page

A Title page is located at the beginning of the manual and provides the part number of the manual,and lists all airplane models pertaining to this manual and their respective serial numbers.Information throughout this manual is applicable to all serial numbers listed on the title pageexcept where specifically stated.

(2) Record of Revisions

A Record of Revisions page is provided for the purpose of recording revisions inserted into thisIPC. When the revision is inserted, the revision number, the date the revision is inserted and theinitials of the person(s) inserting the revision should be recorded on this page.

IML CD and Online Parts Catalogs do not include a Record of Revisions page. Revision standardis available by a link to the catalog Title Page or accessible by clicking Help on the menu bar andselecting ‘About This IML Book...’.

(3) Introduction

This section contains general and specific information on the contents of this catalog. Also, it hasspecific explanations of the BC part-numbering system and instructions on how to use this catalog.

(4) Numerical Index

The Numerical Index is a complete alphabetical and numerical (alpha/numeric) listing of all partnumbers contained in the Parts List of this IPC. The index is divided into two sections, “NumericalIndex-Alpha” and “Numerical Index-Numeric.” The first section contains part numbers whose firstdigit is an alpha character and the second section contains part numbers whose first digit is anumeric character. Entries in these indexes refer to the Chapter, Section, Unit, Figure and ItemNumber (CSUFI) in the Parts List.

Common hardware items having more than ten locations, are listed in the Numerical Index withoutlocations and with a total quantity representing all locations unless the total quantity is greater than999, where “AR” is listed.

IML CD and Online versions of the IPC do not have the alpha/numeric list incorporated. The IMLCD and Online viewer software incorporates a search feature that will permit searches using eitherthe part number or part description. The ‘Searching an IML Parts Catalog’ section details thesearch feature.

(5) Effective Pages and Table of Contents

The Effective Pages following each chapter divider tab lists a summary of allChapter-Section-Unit-Figure and Page numbers, with the current effective date for all pagesapplicable to that chapter. An asterisk (*) preceding the entry indicates that the page has beenadded or revised by the current revision.



The Chapter Table of Contents following the Effective Pages is sequentially arranged inChapter-Section-Unit and Figure number order. The airplane effectivity is also listed.

B. Organization

This IPC is organized in accordance with the Air Transport Association (ATA) Specification No. 2200format. The contents are organized into five levels as follows:

(1) Chapter - Identified by yellow divider tabs. The various groups are broken down into majorsystems such as Environmental Systems, Electrical Power, Landing Gear, etc. Each system isassigned a chapter, which becomes the first element of the standard numbering system. Theelement "28" in chapter 28-40-10-01 refers to the chapter “Fuel.” Everything concerning the fuelsystem will be covered in this chapter.

(2) Section - The major systems of an airplane are broken down into subsections, and areidentified by the second element of the standard numbering system. The element “40” of28-40-10-01 identifies the “Indicating” portion of the fuel system.

(3) Unit - The individual units within a subsystem/section may be identified by the third element ofthe standard numbering system. The element “10” of the number 28-40-10-01 is a subjectdesignator. This element is assigned at the option of the manufacturer and will not necessarilyagree with any other manual.

(4) Figure - Figures are the final definition of the breakdown system. The element “01” of28-40-10-01 represents the figure of the parts list. Some installations or assemblies may be goodonly for certain airplane serials. These figure locations break up the installations or assemblies sothey can be listed for just the airplane serials they effect.

(5) Item - The items are the numeric value in the Fig. Item column on the text page assigned tothe part number. This number corresponds to the number in the Illustration. If however, the itemnumber has a dash (-) preceding it, that part is a non-illustrated item in the list. Example: 110would be illustrated and -110 would not.

3. DETAILED PARTS LIST

The Parts List consists of installations broken down into assemblies, sub-assemblies, detail parts andattaching parts.

A. Column Breakdown

(1) Figure and Item No. Column

This column contains the figure number, of the illustration that shows the parts and the itemnumbers that locate the parts on the illustration. Parts not illustrated will carry a (-) before the itemnumber.

(2) Part Number Column

This column contains the part number assigned to each part.

(a) Long Part Number (Overlength Part Number)

When a part number exceeds 17 characters, the part number column will have either areference/coded part number (RACREF) or ‘+#’ at the end of 17 characters and the completemanufacturer’s part number will then be shown in the nomenclature column. That is the partnumber to use when requisitioning replacement parts. Refer to Figure 1, item 7.



(b) Dash Numbers

A part number (i.e., -1) in the Illustrated Part Catalog may appear, when ordering a partthrough Hawker Beechcraft Parts & Distribution (HBP&D), as a -1, -01, -001 or -0001. Thesedash numbers are considered equivalent and identifiers of the same part.

(3) Nomenclature Column

NOTE: IML CD and Online Catalogs use Description instead of Nomenclature as the Nomenclature Column header.

(a) Indenture

For proper identification of details of assemblies, the listings employ the indention system.Each installation or assembly is broken down to the next indentation to the right. Conversely,the next higher indentation for an installation or assembly for any detail is listed above it.

1 2 3 4 5 6 7

Installation

. Detail parts for installation

. Assembly

. Attaching parts for assembly -------*-------

. . Detail parts for assembly

. . Sub-Assembly

. . Attaching parts for sub-assembly -------*-------

. . . Detail parts for sub-assembly

(b) Left and Right Handed Parts

If two assemblies are made up of a majority of identical parts, or the assemblies areopposite, (i.e., left and right hand), the assemblies are listed together with their detail partslisted as common for both assemblies. In this case only the left or right hand part, but notboth, is illustrated, with the difference between left and right hand parts noted in thedescription column.

(c) Attaching Parts

Attaching parts are listed immediately after the assembly or detail part they attach. Anopening separation symbol, ATTACHING PARTS, followed by a closing separation symbol,-------*-------, distinguishes the listing of attaching parts from a subsequent listing of parts withthe same indention. Refer to Figure 1, items 1 through 4.



(d) Nomenclature Qualifiers

The following qualifiers are used in the nomenclature column:

1 Alternate - Identifies the part number of an interchangeable part.

2 Spare - A preferred replacement part.

3 True Part Number - Indentifies the part number listed in the correct format to be usedfor ordering the part. Refer to Figure 2.

4 Pre - Indentifies those parts that were used prior to the incorporation of a kit or servicebulletin.

5 Rotable Item - Identifies to the user that the part is a candidate for procurement aseither, overhauled, repaired or new.

(4) Effectivity Column

If the Usable On Code column lists an alpha then that will indicate the effectivity. Refer to the endof the parts list of that particular figure to determine the effectivity of the alpha. Each figure has itsown distinct coding, i.e., the code number denoting airplane serial effectivity for one figure may notbe the same as it is for another. The range consists of 10 digits showing a five digit serial numberwhere the effectivity starts and a five digit serial number where the effectivity ends. If no alpha islisted in the column, then the effectivity for the figure (and all its items) will be for all airplanes. Thefollowing table shows an example of the range representation:

(5) Units Per Assembly Column

This column lists the quantity of the units required for the next higher assembly of the part. Thequantity of attaching parts is the quantity required to attach one unit (piece) of the part they attach.The notation “RF” in the “Units Per Assy” column indicates that the part number is “Reference”only. The notation “AR” indicates that part is “As Required” and indicates the parts vary in thenumber required to properly build the assembly.

“USABLE ON CODE” Column

Effectivity(at the end of figure) Airplane(s)

A C1608-C1608 TC-1608 only

B C1608-C2207 TC-1608 thru TC-2207

C E0943-E9999 TE-943 and after

DC2438-C2445 E1199-E1200H1336-H9999

TC-2438 thru TC-2445TE-1199 thru TE-1200TH-1336 and after

FE Figure Effectivity All airplanes for the figure

No alpha code listed None listed All airplanes



4. HOW TO USE THIS CATALOG

A. Graphic Examples

Figure 1 is an example that shows the indenture system used to indicate parts included in any givenassembly. These part numbers are only examples. By this indenture system, parts shown in column 2are component parts of the immediately preceding assembly in column 1. Parts shown in column 3 arecomponent parts of the immediately preceding assembly in column 2, etc., through column 7. As anexample, if the 390-524092-3 PUSH ROD ASSEMBLY is ordered, it would include items 5 through 13.Note that items 1 through 4, bolts, washers and nuts (the attaching parts) are not a part of the PUSHROD ASSEMBLY.

There may be instances when a part number consists of more than 17 characters. In that case thecomplete number will appear in the nomenclature (refer to item 7). The examples in Figures 2 and 3show how to locate a part when the part number is known and how to locate a part number when thedescription is known.



Figure 1Indenture

MU00A

055005AB.AI

FIG

ITEMPART NUMBER 1 2 3 4 5 6 7 NOMENCLATURE USABLE

ON CODE

UNITSPER

ASSY

390-524092-3

AN174-13A

AN174-11A

AN960-416L

MS21042-4

390-524093-1

390-524095-1

SSF-100-3-1.00-+#

390-524096-1

MC21245L7

AN960-716

AV316-4R

AN490HT6P

390-524092-7

390-524079-3

AN4-11A

AM960-416L

REP4M6-4

. PUSH ROD ASSY, TAB CONTROL

. BOLT

. BOLT

. WASHER

. NUT

. . CLEVIS

. . TIGHTENER

. . BUSHING

LONG PART NUMBER:

SSF-100-3-1.00-5.00-0.60

. . TIGHTENER

. . NUT

. . WASHER

. . NUT

. . ROD END

. . TUBE

. ACTUATOR ASSY, RUDDER TRIM TAB

ATTACHING PARTS

. BOLT

. WASHER

. . ROD END

ACTUATOR INST RUDDER TRIM TAB

ATTACHING PARTS

- - - - * - - - -

- - - - * - - - -

01

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

16

1

1

1

2

2

1

1

1

1

2

2

1

1

1

1

4

4

2

INDENTURE COLUMN

1 2 3 4 5 6 7



Figure 2How to Locate a Part when the Part Number is Known

UE00A

023678AB.AI

MS27039-1-38

MS28913-4C

57 60 10 1 470MS27039-1-8

MS27039-4-16 57 60 10 1 475

28 10 50 40 720

28 20 00 20 510 28 10 50 45 170

28 10 50 10 170 28 10 50 30 100

MS27039-4-20 28 10 10 1 440 28 20 00 10 170

28 20 50 20 700 28 40 00 1 740

MS27039-4-26 28 10 10 1 420 28 20 00 20 210MS27039-806 28 20 00 20 540 28 20 00 20 670MS27039C1-10 57 60 10 1 470

MS29513-020 28 20 00 1 60

MS29513-029 28 10 00 1 790MS29513-114 28 20 00 1 290

MS29513-123 28 20 00 20 620

28 20 00 1 330

MS29513-117 28 10 00 1 240 28 10 00 1 300

28 10 00 20 430 28 10 00 20 340

28 10 00 20 450 28 10 00 20 570 28 10 00 20 580 28 10 00 20 640

28 10 00 20 730 28 10 00 20 690

28 10 00 20 750 28 10 00 20 790 28 10 00 20 260

02

0202020402

0202

0201

0202

0202

02

02

RF

02

02

04

02020204020402080802040204

04

APRIL, 2007NUMERICAL INDEX ALPHA-PAGE 21

PART NUMBER CH-SECT-UNIT-FIG-ITEM

AIRLINE PART NO. TTL. REQ.

MS29513-141 28 20 00 1 260MS29513-214

MS29513-222

MS29513-327

28 10 50 1 260 28 10 50 1 760

28 10 50 20 40

28 10 10 1 480MS29526-2 28 10 50 40 240

28 10 50 30 160 28 10 50 40 200

MS29561-112 73 10 00 1 110MS29561-115 73 10 00 1 120MS296512-10 28 10 00 20 400MS3124F10-6P 35 10 10 1 140MS3341-1-9 25 10 70 1 260

MS3341-2-9 25 10 70 1 240 25 10 70 1 250MS33514-04 32 40 00 1 350

MS3364-5-9 33 20 00 30 30

29 10 20 10 40

25 10 70 1 270

MS33514-6

MS33514-8

MS33514E4

MS33514E6

MS33514G8

21 51 30 10 220 21 51 30 20 570

21 51 30 10 210 21 51 30 20 560

29 10 20 10 20 32 40 00 1 510 36 10 00 1 420

29 10 20 10 80 32 40 00 1 520

MS33656-4

MS33656-5

34 10 10 1 60 35 10 00 1 90

02

0404

040602

02

01

02

02

02

02

0301

0201

01

01

01

01

01

020402

0101

02

05

0201

PART NUMBER CH-SECT-UNIT-FIG-ITEM

AIRLINE PART NO. TTL. REQ.

PART NUMBER

TRUE PART NUMBER

CHAPTER, SECTION,

UNIT, FIGURE

& ITEM NUMBER

MS27039C1-10

MS27039C-1-1057 60 10 1 470



Figure 3How to Locate a Part Number when the Description is Known

SUBJECT

AILERON TRIM TAB CONTROLS

CHAPTER 27 - FLIGHT CONTROLS

TABLE OF CONTENTS

CHAPTERSECTIONUNIT

FIGURE EFFECT

27-10-00 30 BB002BB733BB735BB792BB794BB828BB830BB853BB871BB873BB892BB893BB912BB912BL001BL036BN001BN001BT001BT022

110

50

(REF)

40(REF)

100

(REF)160

(REF)

120

B

B

VIEW A

110

170(REF)

130(REF)

5040 140

150

180

160170

120013

27-20-10-01

80

8

2

6

6

3

2

7090

PAGE 0

SEP 30/99

P27A032A

VIEW B

27-20-01-01PAGE 0

APRIL, 2007

BB00A

023679AB.AI

Consult the table of contents in front of the appropriate chapter for the applicable section and figure in which the part is

listed. Immediately preceding the listing of parts is an illustration (refer to step 1 in the example shown above). The

item number adjacent to the illustrated part will appear in the listing of parts in the column entitled "fig item" (refer to

step 2 above). Immediately to the right of the item number will be found the required part number.

PART NUMBER 1 2 3 4 5 6 7

390-524111-0001- 1

20 MS24665-132 . PIN-COTTER

30 NAS6603D8 . BOLT. BOLT

40 NAS6604-4

50 NAS6604-2

ALTERNATE SPARE:

NAS6203-8D

60 NAS1149D0332K

70 NAS1149C0463R . WASHER

. BOLT

. WASHER

. BOLT

80 MS17825-3 . NUT

90 MS21042-4 . NUT

100

110

120

130

140

150

390-524033-0005 . PEDAL ASSY-PILOT

FOR DETAILS SEE:

27-20-10-10

390-524032-0005 . PEDAL ASSY-COPILOT

390-524298-0001 . BRACKET

390-524298-0002 . BRACKET

UBPMV05-03 . BOLT

FOR DETAILS SEE:

27-20-10-10

160 390-524162-0001 . BRACKET

170 390-524162-0002

180

4

RF

4

6

6

4

12

4

12

1

1

1

12

12

1

1

12UBPMV05-02 . BOLT

UBPMV05-04

ATTACHING PARTS

. BRACKET

ATTACHING PARTS

1 RUDDER PEDAL INSTL

PEDAL INSTL-RUDDER

FOR OTHER SYS DETAILS SEE:

32-40-05-01

NOMENCLATURE EFFECTFROM TO

FIGITEM

UNITSPER

ASSY

- - - - - - - - - - - - - -*

- - - - - - - - - - - - - -*

. BOLT

1

110 390-524032-0005 PEDAL ASSY-COPILOT

DESCRIPTION

STEP 1

LOCATE CHAPTER, SECTION, UNIT,

FIGURE & ITEM NUMBER ON

ILLUSTRATION

27-20-01-01PAGE 1

APRIL, 2007200

- ITEM NOT ILLUSTRATED

MISSING ITEM NO. NOT APPLICABLE

STEP 2

LOCATE UNIT

& ITEM NUMBER ON

PARTS LIST



5. FILTERING AN IML PARTS CATALOG

Interactive Illustrated Parts Catalogs in the Interactive Maintenance Library (IML) have the ability to "filter out"unnecessary parts and only display parts applicable to a specific airplane serial effectivity. This feature isavailable on the CD and Online Parts Catalogs and can significantly reduce the amount of data presented inthe parts list window and chapter Table of Contents.

Filtering applies only for the currently open IML parts catalog. When another IML manual is opened or uponexiting the viewer, the filter setting is lost.

NOTE: IML can only filter for one airplane at a time. Filtering for multiple airplanes or a range of airplanes is not available.

A. Filtering a DVD-based IML Parts Catalog

Open an IPC. It is not necessary to be on any particular page. When the Filter is set, it will be applied tothe entire manual.

(1) Select Aircraft Prefix as applicable and enter Serial Number.

(2) Select Filter.

NOTE: A serial number must be set when the filter is turned on or zero results will be available.

(3) When filtering is on, a notification identifying the aircraft prefix and serial number is displayed inthe top left corner of the screen. The notification remains until the filter is turned off.

(4) To turn off the filter select Turn Off Filter.

B. Filtering an Online IML Parts Catalog

Open an IPC. It is not necessary to be on a particular page. When a filter is set, it will be applied to theentire manual.

(1) Select Aircraft Prefix as applicable and enter a Serial Number.

(2) Select Turn On Filter.

NOTE: A serial number must be set when the filter is turned on or zero results will be available.

(3) When filtering is on, a red notification identifying the aircraft prefix and serial is displayed in the topright corner of the screen. Also available are Clear and Change selections.

(4) Select Clear removes the filter. Selecting Change displays a box where the serial number can bechnaged.

6. SEARCHING AN IML PARTS CATALOG

A. Single Book Search

Unless otherwise specified, selecting a search applies to the currently open manual. Multi-book searchis described in the Comprehensive User guide available online and the online help (Ref. Step 8).

(1) Select Search from the tool bar.



(2) From the drop-down menu select the type of search to perform.

(3) In the top-most text box of the Search dialog box, enter the search data. Enter the whole word orjust part of the word (part number etc.).

NOTE: Multi-word search is unavailable.

(4) Click the Search button. All occurrences of data entered in the box in step 3 are returned. Forexample, a search for "bolt" would return "bolt", "Bolts", "Jo-bolt", etc. If this returns too muchextraneous results, click the Exact Match check box and Search again. This time the search willonly return occurrences of "bolt".

(5) The search results are displayed in the Matching Text and Page areas. Click the entry in theMatching Text area to select the most closely matching result. The entries listed in the Page areaare the locations in the manual where it occurs.

(6) Click the entry in the Page area that is the closest to the desired result.

(7) Click the Go To button. The manual will open to the location selected and highlight the searchword.

To go to the next occurrence of the search criteria, click on the "…next occurrence…" icon (smallblue arrow with binoculars). If the results are not satisfactory, go back to the tool bar, select Searchagain and select another (or different) occurrence. The first search results will remain in place untilanother search is performed or the viewer is exited.

(8) The results of a search can be saved to a plain text Comma-Separated Value (.csv) file that willopen as a spreadsheet. Click the Save… button and follow the directions. The exact format andstructure of the text file is described in detail in the Online Manual.

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