MODEL C200 SERIES

PROPELLER
OVERHAUL MANUAL

Member of GAMA

COPYRIGHT © 1992
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
REVISION 2 16 MARCH 2015
1 SEPTEMBER 2005
 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
MAINTENANCE MANUAL

INTRODUCTION - LIST OF EFFECTIVE PAGES

CHAPTER-SECTION-SUBJECT PAGE DATE
00-Title
00-List of Effective Pages Page 1 Mar 16/2015
00-Record of Revisions
00-Record of Temporary Revisions
00-Contents Page 1 Mar 16/2015
LIST OF REVISIONS Page 1 Mar 16/2015
INTRODUCTION Pages 1-9 Mar 16/2015
ICA SUPPLEMENT LIST Page 1 Mar 16/2015

INTRODUCTION - LIST OF EFFECTIVE PAGES Page 1 of 1

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 McCAULEY PROPELLER SYSTEMS
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OVERHAUL MANUAL

INTRODUCTION - CONTENTS
LIST OF REVISIONS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 1
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 1
Export Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 1
INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 1
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 1
Coverage and Format . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 2
Instructions for Continued Airworthiness (ICA) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 2
Cross Reference Listing of Popular Name Verses Model Numbers. . . . . . . . . . . . . . . Page 3
Propeller Model Number . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 3
Coverage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 3
Definitions of Propeller Servicing and Life . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 4
Applicable Service Bulletins and Service Letters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 4
Using the MPC200 Overhaul Manual . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 5
List of Effectivity Pages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 5
Warnings, Cautions and Notes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 5
Revision Filing Instructions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 6
Identifying Revised Material . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 6
Incorporated Service Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 6
Service Information Incorporated (Obsolete) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 7
Service Information Active Because of Active Airworthiness Directives . . . . . . . . . . . Page 7
Applicable Service Bulletins and Service Letters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 7
How to Get Customer Assistance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 8
Customer Comments on Manual . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 9
ICA SUPPLEMENT LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 1
ICA Supplement List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Page 1

INTRODUCTION - CONTENTS Page 1 of 1

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

LIST OF REVISIONS

1. General
A. This maintenance manual includes the original issue and the revisions listed in Table 1. To ensure
information in this manual is current and the latest maintenance and inspections procedures are
available, the revisions must be incorporated in the manual as they are issued.

Table 1. Original Issue -- September 1, 2005

Revision Number Date Revision Number Date

1 Feb 25/2008 2 Mar 16/2015

B. For FAA Approved Airworthiness Limitations that affect propeller models applicable to this
maintenance manual, refer to MPC26, Owner/Operator Information Manual, Revision 2 (always use
the latest revision), Chapter 4 Airworthiness Limitations (latest revision).

2. Export Compliance
A. This publication contains technical data and is subject to U.S. export regulations. This information has
been exported from the United States in accordance with export administration regulations. Diversion
contrary to U.S. law is prohibited.
ECCN: 9E991

LIST OF REVISIONS Page 1

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 McCAULEY PROPELLER SYSTEMS
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OVERHAUL MANUAL

INTRODUCTION

1. General
A. The instructions for continued airworthiness (ICA) in this publication uses the data available at the
time of publication. This publication is updated, supplemented, and changed by service letters,
service bulletins, publication revisions, reissues, ICA supplements, and temporary revisions, which
are supplied by subscription services available from McCauley Product Support. All of these changes
become part of and are specifically included in this publication. The latest changes to this publication
are given through the McCauley Product Support subscription services and/or McCauley authorized
service facilities.

WARNING: The information in this manual has been written for McCauley
approved parts. If non-McCauley approved parts are installed or
McCauley parts are installed in an assembly not authorized by
McCauley, refer to the manufacturers and/or seller's publications
for inspection intervals, replacement time limits, methods
of inspection, life limits, etc. All of the inspection intervals,
replacement time limits, overhaul time limits, inspection methods,
life limits, cycle limits, etc., that McCauley recommends are given
when new, remanufactured, or overhauled McCauley approved
parts are installed. The inspection intervals, replacement time
limits, overhaul time limits, the methods of inspection, life limits,
cycle limits, etc., for non-McCauley parts or non-McCauley
authorized assemblies may not be the same as the approved
McCauley part or assembly.
B. Inspection, maintenance and parts requirements for Supplemental Type Certificate (STC) installations
that modify the propeller are not given in this manual. When the propeller has an STC installation,
those parts of the propeller that the installation has an effect on, must be examined in accordance with
the inspection program published by the owner of the STC. McCauley-supplied inspection criteria may
not be valid for propellers that have STC installations because they may change the systems interface,
operating characteristics and component loads or stresses on adjacent structures.

WARNING: Any inspection and/or repair requiring disassembly, reassembly or

overhaul of a McCauley propeller must be done in an FAA-approved
or international equivalent propeller repair station by qualified
personnel.
C. The inspection procedures described in this manual should be accomplished at every overhaul of the
propeller as required in McCauley MPC26 (latest revision) Owner/Operator Information Manual.

WARNING: All disassembly, overhaul, inspection, repair and reassembly

procedures on a McCauley propeller must be done in an
FAA-approved or international equivalent propeller repair station
by qualified personnel.
D. Users of this manual are presumed to have sufficient training to follow these instructions carefully and
correctly.
E. The inspection requirements are stated in a manner to establish what propeller component is to be
inspected, preferred inspection method, and criteria for airworthiness.
F. This manual contains overhaul instructions, test instructions and illustrated parts list for the Model
C200 Constant-Speed Propeller Assemblies manufactured by McCauley Propeller Systems.

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OVERHAUL MANUAL

G. Overhaul instructions are provided on a functional basis (Disassembly, Cleaning, Repair, etc.). To
the maximum extent possible, the instructions are general and apples to all C200 propellers. When
propellers differ from the general or typical propeller, different instructions as required will be identified
with the particular propeller model or subassembly part number as the case may be.
H. Additional model C200 series propellers will be incorporated in this manual by the addition of pertinent
data and the addition of the model number and detail parts to the Illustrated Parts List. Different
instructions specific for the added models will be given in the appropriate chapters.
I. McCauley Standard Practices Manual (SPM100), Tools List Section 60-00-09, lists the tools by
propeller type required to perform the overhaul operations.
J. Tables of Propeller Application are not given in this manual. The user is directed to consult the FAA
Aircraft Type Certificate Data Sheet (TCDS) for pertinent data for propellers (blade angles, certificated
diameter ranges, particularly). For convenience, the McCauley Propeller Systems Application Guide
(MAG) may be used for propeller application information. The TCDS supersedes any information
published in the MAG.

2. Coverage and Format

A. The MPC200 Propeller Overhaul Manual has been prepared to assist in servicing, overhauling,
and inspecting McCauley C200 model series propeller assemblies, blades/blade assemblies, and
associated parts. In conjunction with the SPM100, Standard Practices Manual, BOM100, Blade
Overhaul Manual, MPC26 Owner/Operator Information Manual, and all subsequent necessary
and required service bulletins and service letters, and ICA Supplements, this manual provides the
necessary information required to enable the certified propeller repair technician to service, inspect,
overhaul, and repair a McCauley C200 model series propeller assembly.
B. The information in this publication is based on data available at the time of publication and is updated,
supplemented, and automatically amended by all information issued in Service Bulletins, Service
Letters, Revisions, Reissues, Temporary Revisions, and ICA Supplements. All such amendments
become part of and are specifically incorporated within this publication. Users are urged to keep
abreast of the latest amendments to this publication through information available through the
McCauley subscription services.
C. Information in this manual is applicable to all U.S. and Foreign Certified propellers.
D. All supplemental service information concerning this manual is supplied to all appropriate McCauley
Service Stations so that they have the latest authoritative recommendations for servicing McCauley
propellers. Therefore, it is recommended that McCauley owners and operators utilize the knowledge
and experience of the McCauley Service Centers.
E. This manual has been prepared in accordance with the Air Transport Association (ATA) Specification
Number 2200 for Manufacturer’s Technical Data.
F. Information beyond the scope of this manual may be found in the SPM100, Standard Practices
Manual, BOM100, Blade Overhaul Manual, and the MPC26, Owner/Operator Information Manual.
G. This manual is available on paper and CD-ROM.

3. Instructions for Continued Airworthiness (ICA)

A. Owner/Operator Information Manual
(1) MPC26, Owner/Operator Information Manual is the principal manual for maintenance personnel
to service, examine, troubleshoot, remove and install C200 model series propellers.
(2) Refer to the MPC26 Owner/Operator Information Manual for all C200 model series propeller
airworthiness limitation inspection time limits and airworthiness limitation replacement time limits.
B. MPC200 Propeller Overhaul Manual
(1) The instructions provided in this manual may be revised to add changes to an existing ICA or
to add an additional ICA when changes to an affected propeller type design require changes
to these instructions. When a revision to this manual is not possible within the time constraints
for these ICAs, the instructions may be transmitted with a temporary revision or with an ICA

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supplement. Temporary revisions will be incorporated in the next revision to this manual and
ICA supplements will also be incorporated in the next revision unless these instructions require
restricted distribution.
C. Temporary Revisions
(1) Temporary revisions may be produced to transmit supplemental instructions for continued
airworthiness when a revision to this manual is not possible within the time constraints for the
ICA. The Temporary Revision will consist of complete page blocks which replace the existing
paper and will temporally supersede the CD-ROM data. Temporary revisions will be included on
the CD-ROM on the next CD-ROM release. Temporary revisions are numbered consecutively
in the ATA chapter assignment. Page numbering uses the three-element number, which
matches the affected manual.
(2) Paper version of the temporary revision
(a) Paper temporary revisions will be distributed on yellow paper. File the temporary revision
cover sheet after the title page of the chapter to which it applies and substitute or add the
remaining pages in the paper manual.
(3) Electronic (CD-ROM) Version of the Maintenance Manual.
(a) The cover sheet will be located in the overhaul manual at the beginning of the chapter to
which it applies and the changed or added pageblocks will be located in the appropriate
location by ATA.
D. ICA Supplements
(1) ICA supplements may be produced to transmit supplemental instructions for continued
airworthiness when a revision to the owner/operator information manual is not possible within
the time constraints for these ICAs. ICA supplements will provide supplemental instructions
for one or more affected manuals and is to be used in conjunction with the affected manuals
(maintenance manual, wiring diagram manual, etc.) until those instructions are incorporated
into the manuals. ICA supplements are numbered consecutively by model in the ATA chapter
assignment. Page numbering uses the three-element number, which matches the affected
manual.
(2) Refer to the ICA Supplement List to determine the incorporation status for each manual affected.

4. Cross Reference Listing of Popular Name Verses Model Numbers

A. All propellers are certified under model number designations. However, in this manual, reference to
specific propellers is almost always by the shortened propeller model number unless the full model
number is necessary to differentiate between versions of the same basic model.

EXAMPLE: Example: E2A37C233-X/X-90REB-8 propeller assembly is shortened to the Hub

model designation E2A37C233 which can also be shortened to C233.

5. Propeller Model Number

A. Refer to Figure 3 in the Propellers - Description and Operation section of this manual for an explanation
of the propeller model number.

6. Coverage
A. The information in this Propeller Overhaul Manual is applicable to the following model propellers:

Table 1. Table 1: Propeller Models

Propeller Models

2A34C201 B2D34C202 2A34C203 C2A34C204 B2A34C205 B2D34C206 B2D34C207

B2D34C208 2A34C209 2A34C210 B2D34C211 B2D34C212 B2D34C213 B2D34C214

2D34C215 2A34C216 B2D34C217 B2D34C218 B2D34C219 B2D34C220 2A34C221

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Table 1. Table 1: Propeller Models (continued)

Propeller Models

2A37C223 B2D37C224 B2A34C225 2A34C227 B2A37C228 B2D37C229 D2A37C230

D2A37C231 E2A37C233 E2A37C234 B2D34C235 C2D37C236 B2A37C238 2A34C239
2A34C240 2A34C241

B. This manual gives the necessary information required to help maintenance personnel to overhaul,
service, examine, and troubleshoot McCauley C200 model series propellers.
C. Information in this manual is applicable to all U.S. and Foreign Certified propellers.

7. Definitions of Propeller Servicing and Life

A. Overhaul - The periodic disassembly, inspection, reconditioning, and reassembly. The overhaul period
is generally based on hours of service (operating time) or calendar time. At such specified times, the
propeller is completely disassembled; inspected for wear, cracks, corrosion or any other unusual or
abnormal condition; parts are refinished; certain parts are replaced; and the propeller is reassembled
and balanced. At overhaul, the instructions contained in this manual, SPM100, BOM100, and all
subsequent necessary and required service bulletins and service letters must be followed.
B. Reconditioning - The rework of major or minor blade damage caused by erosion or striking small
objects during normal operation. Rebalancing of the propeller may be required. Reconditioning is
accomplished on an irregular basis as necessary and required.
C. Repair - The correction, on an irregular basis as necessary and required, of minor or major damage
caused by a physical mishap or failure. Minor repair may be accomplished without overhaul. The
amount, degree and extent of damage determines whether or not a propeller can be repaired without
overhaul. If there is any question, and whenever possible, overhaul should be accomplished. If
propeller blade(s) are bent or twisted, the repair is major and overhaul must be accomplished.
D. Propeller Life - This is expressed in terms of the total hours of service (TT or Total Time) and the hours
of service since overhaul (TSO or Time Since Overhaul). Both references are necessary to define the
life of the propeller. Overhaul does not return the propeller to zero hours total time (TT), only to zero
hours since overhaul (TSO). Reconditioning or repair without overhaul has no effect on total time (TT)
or time since overhaul (TSO).

8. Applicable Service Bulletins and Service Letters

A. Alert Service Bulletin
(1) Alert Service Bulletins are technical documents that provide instructions and, if applicable, part
information for the incorporation of an installation, modification, or repair to a specific propeller
or propeller component. Alert Service Bulletins are used to announce mandatory special
product inspection criteria and modifications, revised maintenance information and/or revised
operational information which has been determined to be critical for the continued safe and
reliable performance of the propeller, or propeller component.
B. Service Bulletin
(1) Service Bulletins are technical documents that provide instructions and, if applicable, part
information for the incorporation of an installation, modification, or repair to a specific propeller or
propeller component. Service Bulletins are used to announce special product inspection criteria
and modifications, revised maintenance information and/or revised operational information
which has been determined to be critical for the continued safe and reliable performance of the
propeller, or propeller component.
C. Service Letter
(1) Service Letters are used to announce support and service information.
D. Special Service Project

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(1) Special Service Projects (SSP's) are similar to service bulletins and are used to announce
special product inspection criteria and modifications, revised maintenance information and/or
revised operational information which is intended to assist in improving propeller safety,
reliability, durability and/or performance. SSP's typically contain similar information and/or
headings as service bulletins, but are often tailored for special situations and/or conditions
or logistical requirements that may affect only a limited number of propellers. One additional
heading that can be found on a SSP is the heading titled "Duration". The Duration heading
provides an expiration date for the SSP when used.

9. Using the MPC200 Overhaul Manual

A. Division of Subject Matter.
(1) The information in the MPC200 Propeller Overhaul Manual content organization is covered by
Air Transport Association Chapter 61.
B. Page Numbering System.
(1) The page numbering system of this Overhaul Manual consists of the Air Transport Association
Specification 2200 three-element numbers separated by dashes, next to which the page number
and date are printed.
(2) The page number to the right of the three-element number complies with Air Transport
Association Specification 2200 for subdividing an Overhaul Manual. Blocks of sequential
numbers are used to identify:

Page 1 through 99 Description and Operation

Page 101 through 199 Troubleshooting
Page 301 through 399 Disassembly
Page 401 through 499 Cleaning
Page 501 through 599 Inspection/Check
Page 601 through 699 Repair and Replacement
Page 701 through 799 Assembly
Page 801 through 899 Testing and Balance
Page 1001 through 1099 Illustrated Parts List
(3) The date which appears below the page number signifies when the page was issued. If no
revisions to that page have occurred, the date signifies original date.
(4) Illustrations use the same figure numbering as the page block in which they appear. For example:
Figure 602 would be the second figure in a repair section.

10. List of Effectivity Pages

A. A list of effective pages is provided at the beginning of each chapter. All pages in the specific chapter
are listed in numerical sequence on the Effectivity Page(s) with the date of issue for each page.

11. Warnings, Cautions and Notes

A. Throughout the text in this manual, warnings, cautions and notes pertaining to the procedures being
accomplished are included. These adjuncts to the text are used to highlight or emphasize important
points. Warnings and Cautions precede the text they pertain to, and Notes follow the text they pertain
to.
(1) WARNING - Calls attention to use of materials, processes, methods, procedures or limits which
must be followed precisely to avoid injury or death to persons.
(2) CAUTION - Calls attention to methods and procedures which must be followed to avoid damage
to equipment.
(3) NOTE - Calls attention to methods which will make the job easier.

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12. Revision Filing Instructions

A. Regular Revision
(1) Pages to be removed or inserted in the manual are determined by the effectivity page. Pages are
listed by the three-element number (chapter/section/subject) and then by page number. When
two pages display the same three-element number and page number, the page with the most
recent Date of Page Issue shall be inserted in the maintenance manual. The date column on
the corresponding chapter effectivity page shall verify the active page.
B. Temporary Revision
(1) File temporary revisions in the applicable chapter(s) in accordance with filing instructions
appearing on the first page of the temporary revision.
(2) The rescission of a temporary revision is accomplished by incorporation into the manual or by a
superseding temporary revision. A Record of Temporary Revisions is furnished in the Temporary
Revision List located previous to the Introduction. A Manual Incorporation Date column on the
Temporary Revision List page will indicate the date the Temporary Revision was incorporated,
thus authorizing the rescission of the temporary revision.

13. Identifying Revised Material

A. Additions or revisions to text in an existing section will be identified by a revision bar in the left margin
of the page and adjacent to the change.
B. When technical changes cause unchanged text to appear on a different page(s), a revision bar will be
placed in the left margin opposite the chapter/section/subject, page number and date of all affected
pages, providing no other revision bar appears on the page. These pages will display the current
revision date in the Date of Page Issue location.
C. When extensive technical changes are made to text in an existing section that requires extensive
revision, revision bars will appear the full length of text.
D. Revisions to illustrations will be shown by a revision bar along the entire vertical length of the left
margin of the illustration.

14. Incorporated Service Information

A. The following service information has been incorporated into this manual. This service information
remains active due to applicability to other models.

Service Bulletin Service Bulletin Date Manual Incorporation Status

Number
119A March 1, 1999 Original Active

Service Letter Number Service Letter Date Manual Incorporation Status

1979-5 July 25, 1979 Original Active
1989-2C February 15, 2002 Original Active
1991-5A January 5, 2004 Original Active
1991-11A November 22, 1993 Original Active
1998-3A September 21, 1998 Original Active
1998-5 January 23, 1998 Original Active
1998-8B March 15, 2001 Original Active

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Service Letter Number Service Letter Date Manual Incorporation Status

1998-24 September 21, 1998 Original Active
1999-6 June 21, 1999 Original Active
2000-5A August 1, 2000 Original Active
2000-19 November 20, 2000 Original Active
2000-20 November 20, 2000 Original Active

15. Service Information Incorporated (Obsolete)

A. The following service information has been incorporated into this manual.

Service Bulletin Number Service Bulletin Date Manual Incorporation

198 December 21, 1992 Original

Service Letter Number Service Letter Date Manual Incorporation

1979-7 September 18, 1979 Original

16. Service Information Active Because of Active Airworthiness Directives

A. The following service information has been incorporated into this manual. Due to the relationship of
the service information to active Airworthiness Directives, the service information also remains active.

Service Bulletin Service Bulletin Date Manual Incorporation Airworthiness Directive

Number Number
146 December 3, 1982 Original AD 82-27-02 R1

Service Letter Number Service Letter Date Manual Incorporation Airworthiness Directive
Number
1993-13 September 15, 1993 Original AD 95-09-08

17. Applicable Service Bulletins and Service Letters

A. Service Bulletins are issued to advise of propeller design changes that must be incorporated,
to provide procedures for correction of problems that have developed in the field, and for other
appropriate reasons.
B. Service Letters are issued for minor modifications to be performed in the field and for recommended
action at overhaul.
C. The following list of Service Bulletins and Service Letters supplement or replace information contained
in this manual and are to be reviewed prior to servicing or overhaul of a propeller assembly.

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Service Bulletins Service Letters

Number Date Number Date
176E March 3, 2003 1989-2C February 15, 2002
177B June 30, 1992 1989-4D July 20, 2001
227B August 28, 2001 1991-11A November 22, 1993
237C February 15, 2003 1995-4B June 6, 2005
1995-21B August 5, 1997
1995-5A December 5, 2007
1998-23 September 21, 1998
1998-24 September 21, 1998
2004-1 January 26, 2004
2000-5A August 1, 2000
2004-1 January 26, 2004
2005-5 August 8, 2005
2006-5 June 15, 2006
2007-13 December 7, 2007

18. How to Get Customer Assistance

A. REVISIONS, REISSUES and TEMPORARY REVISIONS can be purchased directly from Cessna:,
Attention: Customer Care, e-mail: Customercare@cessna.textron.com, Telephone 316-517-5800,
Telefax 316-517-5802.
B. Product Support

McCauley Product Support

McCauley Propeller Systems
P.O. Box 7704
Mailing Address Wichita, KS 67277-7704

(1) If you need assistance with a general support question, publication information, subscriptions,
or maintenance programs visit our website at www.mccauley.textron.com or contact:

McCauley Product Support

Wichita, Kansas
Phone Numbers
1-800-621-7767 or 316-831-4021
Fax 316-206-9948
Email Address productsupport@mccauley.textron.com

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19. Customer Comments on Manual

A. McCauley Propeller Systems has endeavored to furnish you with an accurate, useful, and up-to-
date manual. This manual can be improved with your help. Please return the registration card to
receive revisions to this manual. Please contact McCauley Product Support to report any errors,
discrepancies, and omissions in this manual as well as any general comments you wish to make.

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ICA SUPPLEMENT LIST

1. ICA Supplement List

ICA Supplement Title ICA Manual

Number Supplement Incorporation
Date Date

NOTE: No ICA Supplements have been issued that affect this manual.

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CHAPTER

61
PROPELLERS
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61 - LIST OF EFFECTIVE PAGES

CHAPTER-SECTION-SUBJECT PAGE DATE
61-Title
61-List of Effective Pages Page 1 Mar 16/2015
61-Record of Temporary Revisions
61-Contents Page 1 Mar 16/2015
61-10-01 Pages 1-11 Mar 16/2015
61-10-01 Pages 301-306 Sep 1/2005
61-10-01 Page 401 Sep 1/2005
61-10-01 Pages 501-511 Mar 16/2015
61-10-01 Pages 601-617 Mar 16/2015
61-10-01 Pages 701-717 Feb 25/2008
61-10-01 Page 801 Mar 16/2015
61-10-01 Pages 1001-1031 Feb 25/2008

61 - LIST OF EFFECTIVE PAGES Page 1 of 1

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

61 - CONTENTS
PROPELLERS - DESCRIPTION AND OPERATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 1
Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 1
Definitions of Propeller Servicing and Life . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 1
Introduction. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 4
Oil filled Models . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 9
DISASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 301
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 301
Disassembly of Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 301
Disassembly of Components . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 305
CLEANING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 401
Cleaning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 401
INSPECTION/CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 501
Detailed Part Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 501
Bores and Diameters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 501
Nondestructive Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 501
Spring Testing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 504
Blade Actuating Pin Assembly Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 504
Spinner Dimension Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 506
REPAIR AND REPLACEMENT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 601
Repair . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 601
Change Letter Stamping . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 601
Modification of Propeller to Oil Filled . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 611
Replacement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 613
Replacement of C-3411 Bearing Races With C-5270 Bearing Races . . . . . . . . . . . . . 61-10-01 Page 617
Refinishing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 617
ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 701
Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 701
Hub Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 701
Piston Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 702
Propeller Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 702
Blade Shimming . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 708
Blade Shake Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 710
Blade Rotation Friction Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 710
Install Actuating Pin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 711
Pitch Control Parts Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 711
Pitch Stop Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 712
Decal Installation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 713
TESTING AND BALANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 801
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 801
Leakage Check for Oil Fill Propellers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 801
Static Balance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 801
Oil Filling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 801
Placing Attaching Parts on Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 801
ILLUSTRATED PARTS LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 1001
Illustrated Parts List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61-10-01 Page 1001

61 - CONTENTS Page 1 of 1
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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

PROPELLERS - DESCRIPTION AND OPERATION

1. Description
A. The C200 series propellers are of the constant speed type. They are a single-acting unit in which
hydraulic pressure works against the forces of springs and the natural centrifugal moment of the
rotating blade to provide the correct pitch for engine load. Hydraulic pressure causes the blades to
move toward high pitch (decreasing rpm). The springs and centrifugal moments urge blades toward
low pitch (increasing rpm) (refer to Figure 1, C200 Series Propeller). An engine-mounted governor
of the McCauley Model C290 Series or equivalent is required for operation. No other external
components are required.
B. The source of hydraulic pressure for operation is oil from the engine lubricating system, controlled by
the engine driven governor. Pressure is supplied to the forward side of the propeller piston through
the engine shaft flange. Increasing the engine speed will cause oil to be forced into the cylinder to
move the piston with a corresponding increase in pitch. Conversely a decrease of engine speed will
result in oil leaving the cylinder, with a decrease in pitch. Flow of oil through governor and propeller
does not interfere with engine lubrication.
C. Cockpit procedure for normal constant speed operation, starting, stopping, and ground run-up is
consistent with standard practice for this type propeller.
D. A complete reduction of hydraulic pressure in flight, either by a failure in the system causing loss of
oil, or by manipulation of controls to require maximum RPM, will cause springs to automatically move
the blades to the low or minimum pitch position.

2. Definitions of Propeller Servicing and Life

NOTE: Terms used in this manual are defined as follows for propeller assembly servicing and life:
A. Overhaul
(1) The interval between overhauls of the propeller must not exceed limitations stated in the latest
revision of MPC26, Owner/Operator Information Manual.
(2) Overhaul is the periodic disassembly, inspection, reconditioning and reassembly of a propeller
assembly which is constructed of a number of moveable, detachable parts.
(a) The period between overhauls is based either on hours of service (operating time) or on
calender time.
(3) At specified overhaul periods:
(a) Completely disassemble propeller assembly.
(b) Inspect all parts for cracks, wear, corrosion and other unusual or abnormal conditions.

NOTE: Refer to the Standard Practices Manual, Section 60-00-02, Inspection Criteria.

(c) Refinish or replace certain parts as specified.

(d) Balance blade and propeller assembly per Section 60-00-07 of the Standard Practices
Manual, Blade Track and Blade to Blade Balance
(4) At overhaul, follow all applicable instructions in this manual and in later service bulletins and
letters.
B. Reconditioning
(1) Reconditioning is the rework of either minor or major damage of certain propeller components,
such as blade damage caused when small objects strike the blade during normal operation.
(a) Recondition parts as needed or required in accordance with procedures in this manual.
C. Repair
(1) Repair is the correction of either minor or major blade assembly damage.

61-10-01 Page 1
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McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

C200 Series Propeller

Figure 1 (Sheet 1)

61-10-01 Page 2
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McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

C200 Series Propeller

Figure 1 (Sheet 2)

61-10-01 Page 3
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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

CAUTION: Always refer to Section 61-10-22, Special Instructions, Blade

Overhaul Manual (BOM100) before you do any repairs.
(a) Repair propeller assembly as needed or required in accordance with procedures in this
manual.
D. Blade Model Designation
(1) Blade model designation .

3. Introduction
A. The propeller model number is the basic propeller assembly i.e. B2A34C201, refer to Figure3.
Variations to the assembly are specified by the "part number" for example, P2017294-XX. The part
number identifies a variation of the propeller assembly by the angles, blade diameter, paint scheme,
oil-fill configuration, and deice equipment. Part numbers which end in "-5X" designate propeller
whose configuration was modified to or designed as oil-filled.

NOTE: The C201, C203, C204, C205, C209, C223, C227, and C228 were not originally oil-filled.
These models must be modified to the oil-fill configuration at the next overhaul or major
disassembly. Currently produced propellers of those models are oil filled.

EXAMPLE: Part number P2017294-51 has a low blade angle of 13.0 degrees, high blade angle of
24.5 degrees, 90DA-8 blades, uses the D-6286 paint scheme. Part number P2017294-
52 has a low blade angle of 10.5°, high blade angle of 24.5°, 90DA-2 blades, and uses
the D-6286 paint scheme. Figure 2 illustrates a part number explanation.
B. The Illustrated Parts List is for all part numbers of a propeller assembly.
C. Table 1 specifies blade model, installation decal, paint scheme, hub assembly, and angles for each
part number propeller.
(1) Blade model is specified in maximum diameter for a specific propeller part number application.
(2) Refer to the SPM100 Standard Practices Manual, Section 60-00-07, Paint Instruction, for paint
scheme details.
(3) Angles are specific for the propeller part number.
(4) Some model numbers will have two hub assemblies listed. Either assembly may be used when
assembling the propeller, however only the current production model is available from McCauley.
Careful attention must be made to Notes for correct installation of parts.

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Part Number Explanation

Figure 2 (Sheet 1)
D. Tables of propeller part numbers with a coresponding airplane application are not given in this
manual. The user is directed to consult the FAA Aircraft Type Certificate Data Sheet (TCDS)
for pertinent data for propellers (blade angles, certificated diameter ranges, particularly). For
convenience, the McCauley Propeller Systems Application Guide (MAG) may be used for propeller
application information. The TCDS supersedes any information published in the MAG.

Table 1. Propeller Part Number, Blade Model, Installation Decal, Paint Scheme, Angles, and Hub Assembly

HIGH
BLADE
PART LOW BLADE ANGLE
NUMBER ANGLE (degrees
PART BLADE DECAL PAINT HUB (degrees +0.5 or SPINNER
NUMBER MODEL B-4862 SCHEME ASSEMBLY +0.2 or -0.2)* -0.5)* ASSEMBLY
* Angle tolerance unless otherwise stated.
P2017294-51 90DA-8 -491 D-6286 D-7292 13.0 24.5 D-7569
P2017294-52 90DA-2 -492 D-6286 D-7292 10.5 24.5 D-7569
P2024135 82PA-X -- D-4819 D-7292 12.1 26.0
P2033909-51 90DCA-8 -541 D-4819 D-7292 12.5 25.0
P2033909-52 90DCA-2 -542 D-4819 D-7292 10.0 24.5
P2033909-53 90DCA-14 -543 D-4819 D-7292 12.0 25.1
P2033909-54 90DCA-10 -544 D-4819 D-7292 11.3 24.8
P2033909-55 90DCA-8 -545 D-4819 D-7292 12.5 29.0
P2033909-56 90DCA-8 -546 D-6286 D-7292 12.5 25.0 D-7519,
D-7520
P2033909-57 90DCA-2 -547 D-6286 D-7292 10.0 24.5 D-7519
P2043909-51 90DCB-0 -548 D-4819 D-4801 12.9 26.0
P2043909-52 90DCB-8 -549 D-4819 D-4801 15.0 29.4
P2043909-53 90DCB-2 -550 D-4819 D-4801 13.3 26.0
P2043909-54 90DCB-8 -551 D-6286 D-4801 15.0 29.4

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1. Propeller Part Number, Blade Model, Installation Decal, Paint Scheme, Angles, and Hub Assembly
(continued)
HIGH
BLADE
PART LOW BLADE ANGLE
NUMBER ANGLE (degrees
PART BLADE DECAL PAINT HUB (degrees +0.5 or SPINNER
NUMBER MODEL B-4862 SCHEME ASSEMBLY +0.2 or -0.2)* -0.5)* ASSEMBLY
* Angle tolerance unless otherwise stated.
P2043909-55 90DCB-8 -630 D-4819 D-4801 14.5 31.0
P2056588-51 90DHA-4 -330 D-4819 D-6608 9.7 28.5 (+1.0
or -0.5)
P2064327-01 78TA-0 -- D-4819 D-4326 11.6 27.5
P2064327-02 78TA-0 -- D-4819 D-4326 12.9 27.5
P2074392-01 78TCA-0 -130 D-4819 D-4326 12.9 27.5 (+1.0
or -1.0)
P2074392-02 78TCA-0 -624 D-4819 D-4326 11.9 27.5 (+1.0
or -1.0)
P2084392-01 82PA-6 -- D-4819 D-4326 12.1 26.0 (+1.0
or -1.0)
P2094447-51 78CCA-2 -553 D-4819 D-7292 11.3 22.0
P2094447-52 78CCA-4E -646 D-4819 D-7292 12.5 23.0
P2104532-01 78CCA-2 -132 D-4819 D-4531 11.3 22.0
P2104532-02 78CCA-6 -133 D-4819 D-4531 12.5 22.0
P2114392-21 82PCA-6 -134 D-4819 D-4326 12.1 26.0 (+1.0
or -1.0)
P2124392-31 78CDA-4 -135 D-4819 D-4326 14.0 29.5
P2124392-32 78CDA-4E -162 D-4819 D-4326 14.0 29.5
P2134392-41 90DHA-16 -148 D-4958 D-4326 12.5 27.5
P2144392-61 90DHB-8 -158 D-4819 D-4326 15.8 29.4
P2144392-62 90DHB- -163 D-4819 D-4326 13.9 33.0
16E
P2144392-63 90DHB- -237 D-5616 D-4326 13.9 33.0
16EP
P2155092-01 90DJA-14E -183 D-4958 D-5098 12.5 27.5
P2164532-10 90DHB- -173 D-4819 D-4531 14.7 33.0
16E
P2164532-11 90DHB- -238 D-5616 D-4531 14.7 33.0
16EP
P2164532-12 90DHB- -453 D-6286 D-4531 12.6 33.0
16E
P2174990-01 90DHB-8 -175 D-4819 D-4326 15.8 31.9
P2185053-01 90DHB-8 -179 D-4819 D-5045 15.8 29.4

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1. Propeller Part Number, Blade Model, Installation Decal, Paint Scheme, Angles, and Hub Assembly
(continued)
HIGH
BLADE
PART LOW BLADE ANGLE
NUMBER ANGLE (degrees
PART BLADE DECAL PAINT HUB (degrees +0.5 or SPINNER
NUMBER MODEL B-4862 SCHEME ASSEMBLY +0.2 or -0.2)* -0.5)* ASSEMBLY
* Angle tolerance unless otherwise stated.
P2195054-01 90DHB-8 -180 D-4819 D-5045 15.8 31.9
P2205060-01 80VHA-3.5 -181 D-4819 D-5078 12.1 26.4
P2214532-12 90DHC- -241 D-4819 D-4531 14.7 38.0
16E
P2214532-13 90DHC- -244 D-5616 D-4531 14.7 38.0
16EP
P2235197-51 90RB-6 -429 D-6286 D-7108 12.0 29.7 D-7587
P2235197-52 90RB-6 -430 D-6286 D-7108 12.7 29.7
P2235197-53 90RB-6 -431 D-6286 D-7108 13.0 29.7
P2235197-54 90RB-6 -432 D-6286 D-7108 13.3 29.7
P2246262-01 90RA-9 -253 D-6286 D-5045 14.7 24.6 D-6195
P2246262-02 90RA-4 -256 D-6286 D-5045 15.0 24.6
P2246262-03 90RA-9 -487 D-6286 D-5045 13.3 24.6
P2246262-04 90RA-12 -554 D-6286 D-5045 13.4 29.5 D-6195
P2246262-05 90RA-10.5 -604 D-6286 D-5045 13.1 29.5
P2246262-06 90RA-9 -605 D-6286 D-5045 12.7 24.6
P2256247-01 90DJA-22 -254 D-6286 D-6237 17.5 48.0 D-5915
P2273909-51 90DHB- -552 D-6286 D-7292 14.8 33.0
16E
P2286737-51 90RDA-4 -359 D-6286 D-6740 11.5 29.5 D-3396,
D-5255
P2296805-01 90RHC-11 -358 D-6286 D-5045 13.8 35.0
P2306949-52 90REB-4 -392 D-4819 D-6962 10.5 27.5
P2306949-53 90REB-8 -393 D-4819 D-6962 12.0 28.3
P2306949-60 90REB-8 -394 D-4819 D-6962 12.8 28.3
P2306949-61 90REB-2 -404 D-4819 D-6962 11.5 28.3
P2306949-62 90REB-2 -396 D-4819 D-6962 11.7 24.5
P2306949-63 90REB-8 -395 D-4819 D-6962 13.3 28.3
P2316949-51 90REC-8 -397 D-4819 D-6962 14.3 34.5
P2316949-52 90REC-8.5 -398 D-4819 D-6962 14.3 34.5
P2336960-51 90REB-8 -399 D-4819 D-6953 12.8 28.3
P2346960-51 90REC-8 -400 D-4819 D-6953 14.3 34.5

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1. Propeller Part Number, Blade Model, Installation Decal, Paint Scheme, Angles, and Hub Assembly
(continued)
HIGH
BLADE
PART LOW BLADE ANGLE
NUMBER ANGLE (degrees
PART BLADE DECAL PAINT HUB (degrees +0.5 or SPINNER
NUMBER MODEL B-4862 SCHEME ASSEMBLY +0.2 or -0.2)* -0.5)* ASSEMBLY
* Angle tolerance unless otherwise stated.
P2357299-02 90DKB-8E -503 D-6286 D-7301 17.0 31.8 D-7267
P2367451-01 90REA-4 -522 D-6286 D-7450 10.5 29.5
P2387543-51 90REA-2 -567 D-6286 D-7546 8.1 29.5 D-7519-1
P2387543-52 90REA-4 -568 D-6286 D-7546 8.5 29.5
P2387543-53 90REA-6 -569 D-6286 D-7546 8.9 29.5 D-7520
P2387543-54 90REA-8 -570 D-6286 D-7546 9.3 29.5
P2397580-01 90DMC-15 -591 D-6286 D-7585 19.0 37.5 (+1.0 D-7579
or -0.5)
P2407596-01 90DJA-22 -590 D-6286 D-4531 17.5 45.5
P2417580-01 82PGC-6 -597 D-6286 D-7585 20.0 37.5 (+1.0 D-7579
or -0.5)

Table 2. Propeller Type Certificate and Mounting Flange to Blade Centerline Distance

Distance From
Mounting Flange to
Model Part Number Type Certificate Blade Centerline
2A34C201 P2017294-X P3EA 3.688
B2D34C202 P2024135-X P7EA 4.500
2A34C203 P2033909-X P3EA 3.688
C2A34C204 P2043909-X P3EA 3.688
B2A34C205 P2056588-X P3EA 3.688
B2D34C206 P2064327-X P7EA 4.500
B2D34C207 P2074392-X P7EA 4.500
B2D34C208 P2084392-X P7EA 4.500
2A34C209 P2094447-X P3EA 3.688
2A34C210 P2104532-X P3EA 6.563
B2D34C211 P2114392-X P7EA 4.500
B2D34C212 P2124392-X P7EA 4.500
B2D34C213 P2134392-X P7EA 4.500
B2D34C214 P2144392-X P7EA 4.500
2D34C215 P2155092-X P7EA 4.500
2A34C216 P2164532-X P3EA 6.563

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Table 2. Propeller Type Certificate and Mounting Flange to Blade Centerline Distance (continued)
Distance From
Mounting Flange to
Model Part Number Type Certificate Blade Centerline
B2D34C217 P2174990-X P7EA 4.500
B2D34C218 P2185053-X P7EA 4.500
B2D34C219 P2195054-X P7EA 4.500
B2D34C220 P2205060-X P7EA 6.500
2A34C221 P2214532-X P3EA 6.563
2A37C223 P2235197-X P3EA 4.375
B2D37C224 P2246262-X P7EA 4.500
B2A34C225 P2256247-X P3EA 3.688
2A34C227 P2273909-X P3EA 3.688
B2A37C228 P2286737-X P3EA 4.375
B2D37C229 P2296805-X P7EA 4.500
D2A37C230 P2306949-X P3EA 3.688
D2A37C231 P2316949-X P3EA 3.688
E2A37C233 P2336960-X P3EA 6.563
E2A37C234 P2346960-X P3EA 6.563
B2D34C235 P2357299-X P7EA 6.500
C2D37C236 P2367451-X P7EA 4.500
B2A37C238 P2387543-X P3EA 3.688
2A34C239 P2397580-X P3EA 6.563
2A34C240 P2407596-X P3EA 6.563
2A34C241 P2417580-X P3EA 6.563

4. Oil filled Models

A. The C230, C231, C232, C233, C235, C236, C238, C239, and C241 propellers were originally made
in an oil filled configuration. The C201, C203, C204, C205, C209, C223, C227, and C228 models
were originally made as non-oil filled but are now made as oil filled (conversion to oil fill is mandatory).
Replacement hubs are only available in an oil filled configuration.
(1) Identification - Oil filled propellers are identified by a letter change in the model designation
(Refer to Table 601, Change Letter Stamping Requirements). They are also identifiable by a
filler plug in the hub. The filler plug is unique to the oil filled models.
(2) Interchangeability - To put oil in a propeller has no effect on the interchangeability or eligibility of
the model. For example, an oil filled propeller can be installed on any approved aircraft for the
model, if it is in the diameter and angle specifications.
(3) Repair of leaks - An indication of leakage from the propeller is red oil. It is necessary to
disassemble the propeller repair leaks. An FAA approved propeller repair station or international
equivalent must repair the leaks.

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Propeller Model Number Explanation

Figure 3 (Sheet 1)

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(4) Internal oil leak - An internal O-ring leakage between the propeller lubrication oil and the propeller
actuation oil (from the propeller governor). The increased oil pressure in the hub could cause
a sluggish response in the propeller pitch change. An FAA approved propeller repair station or
international equivalent must repair the internal oil leaks. The engine oil and propeller oil are
compatible. If the two oils mix together, no harmful effects will occur.
(5) Propeller balance - Centrifugal force on the rotating propeller will evenly distribute the oil and
not cause an unbalanced condition. However, during a start in the extreme cold, congealed oil
can cause momentary roughness. Also, you must drain the oil to prepare the propeller for a
static balance vertically (for example knife-edge). It is usually not necessary to drain the oil for
a horizontal balance (for example suspension).
(6) Weight - Two blade oil filled propellers weigh approximately 2.8 pounds (1.27 kg) more than the
non-oil filled counterpart.
(7) Disassembly - The disassembly of the threadless, two-blade oil filled propellers is the same as
the non-oil filled models except you must drain the red oil. Refer to Disassembly .
(8) Assembly - The procedures to assemble a two-blade oil filled propeller is the same as the non-oil
filled models except as referred to in the Assembly section.

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DISASSEMBLY

1. General
A. Parts for the spinner may accompany the propeller. Handle them with care to prevent damage.
B. Do disassembly and reassembly on clean surfaces. Handle and store removed parts with care so
that damage does not occur, particularly to the highly finished working surfaces, and so that dirt is not
admitted to the clearances between parts not disassembled but which must be loosened.
C. Refer to the Illustrated Parts List, Figure 1001 for C200 Series Propeller Parts.

NOTE: The numbers in parentheses show the index numbers for the parts that are referred to in
the instructions. (Refer to the Illustrated Parts List.)

2. Disassembly of Propeller
A. Disassemble Propeller
(1) On oil filled models, remove the fill plug and drain the oil into a suitable container.
(2) Apply blade wrap to cover at least six inches (15 mm) of each blade outward from the hub.
(3) Remove screws (1), tubes, (3), cylinder mounting ring (2), that secure the cylinder (8) to the hub.
(a) Discard the screws (1).
(4) On oil filled models, remove the screws (30 or 34).
(5) Pull the cylinder (8) off the hub.
(6) Remove gasket (9) and discard.
(7) By hand, rotate the blades toward low pitch. This will force the piston (14) forward.
(8) Insert the B-4092-1 roll pin tool into the hub opening.
(9) While you support the piston, drive out the roll pins (16) that secure the piston rod pins (15) to
the piston (14)
(10) Remove the piston rod pins (15) from the piston (14) and link (17).
(11) Rotate the blades toward high pitch until the links (17) are approximately half way out of the
piston slots.
(12) Grasp the piston and remove it and all attached parts from the hub.

WARNING: The spring is compressed and incorrect disassembly could

cause injury.
(13) Put the piston aside for later disassembly. Refer to Disassembly of Components
(14) Remove the lockwire from the actuating pin assembly (60) screws (59).
(15) Remove the screws (59) that secure the actuating pin assembly (60) to the blade butt.
(16) Carefully remove the actuating pin assembly (60) from the blade butt with the link still attached.
(17) Blade Removal
(a) Rotate propeller so that a blade is down. Hold and manipulate the blade while the retention
parts are loosened and the bearing is removed.

CAUTION: Make sure the blade butt is up and the blade is pointing down
when the retaining ring is removed. The butt could fall into the
hub, and be damaged or damage the other blade.
(b) Use a Snap-On PR8, or equivalent, pliers to release the retaining ring (53) from the groove
in the blade butt. (Refer to Figure 301).
(c) Make sure the blade is protected with blade wrap at least six inches (150 mm) from the
hub outward.
(d) Move carrier (49), shims (50 and 51), wire ring (52), and retaining ring (53) down and
temporarily secure along the blade shank.

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(e) Remove split retainer halves (45) through the front hub opening as follows:

NOTE: In addition to moving the blade butt within the hub, the split retainer halves must
be simultaneously rotated and manipulated for release from the blade butt and
withdrawal from the hub.

1 Raise the blade butt into hub approximately 0.5 to 1 inch (13 to 26 mm).
2 If the bearing race (46) adheres to the split retainer halves (45), tap the retainer ring
halves with a plastic rod to break them free.

NOTE: When done properly, the split retainer can be removed by hand without
using any force.

NOTE: Split retainers (45) are manufactured in matched sets and identified by
serial numbers etched on each retainer half. Keep matched sets together
when disassembling. It is important that retainers have matching serial
numbers when installed on a propeller blade. If they do not, dimensional
variations between the two retainer halves could result in stresses being
concentrated on only one retainer half instead of being evenly distributed.

CAUTION: If you feel any resistance while attempting removal, return

the ring half to its original position and start over. Any
attempt to force or pry out the ring will only wedge it in
tighter and cause damage.
3 While you hold the blade up, grasp either retainer half at the center of its arc and
rotate it upward.

NOTE: Alternately, put a small magnet on the center of the arc of the retainer half
and rotate it up and off the butt.

4 When the split retainer ends clear the blade neck, work the split retainer half up over
the end of blade butt and withdraw it from the hub.
5 Remove the other half of the split retainer in the same manner
6 Remove the blade from the hub.
(f) Position the inner race against the outer race and temporarily clamp in place with spatulas
and rubber bands as shown in Figure 302.
(g) Repeat the steps necessary for the other blade.
(h) Remove the shim carrier (49), shims (50, 51), and retainer (53) from the blade shank.
Remove the O-ring (44) from the blade shank or hub bore as required.
1 Discard the O-rings.
(i) Measure and record shim thicknesses on a tag attached to the carrier with which it was
used.
(j) Record the blade and hub serial numbers and the hub socket number.
(k) Protect the blade during handling and storage with blade wrap or a sack and blade butt
protector.
(l) Remove and discard balls (47) and separators (48) from bearing.
(18) Bearing Race Removal.

NOTE: The following procedure is for one set of bearing races.

CAUTION: Be extremely careful when you remove the bearing races from the
hub. If the races scratch or dent the hub at the slots, cracks will
develop from this damage.
(a) Remove the clamp used to hold the inner bearing race.

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Removal of Retaining Ring

Figure 301 (Sheet 1)

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Clamp Bearing Races

Figure 302 (Sheet 1)

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1 While it is still in the hub, tag the inner bearing races (46) to correspond to hub socket
in which it is used.
2 Remove the race through the slots in the hub front opening.
3 It will be necessary to rotate the inner race so that it can be removed through the
slots.

NOTE: Bearing races are manufactured in pairs and may or may not be identified
as pairs by serial number. Therefore, they must be identified as sets before
removal from the hub. Bearing races must be used as serialized or matched
pairs.

CAUTION: Do not attempt to pry or use any metal tool to remove the outer
race.
(b) Place shop cloths in the hub so that outer race does not fall down and damage itself or the
hub when loosened.
(c) Use a soft, wedge-shaped tool (fabricated from nylon or other plastic material) and tap
lightly around the perimeter to loosen the outer bearing race (46).
(d) Tag and remove the outer race from hub in the same manner as the inner race.
(e) Store with it's corresponding inner race.

3. Disassembly of Components
A. Piston Assembly
(1) Remove the high pitch stop spacer (28) from the rear of the assembly.
(a) Remove and discard the O-ring (13) from its groove in the piston.
(b) If the fiber washer (27), on the models in which it is installed, did not come out with the
assembly, it can be removed from the hub later.
1 Discard the fiber washer.
(2) Put the remaining parts of the assembly in an arbor press with the piston end up.
(a) Supply a plate with a hole large enough for the piston rod tube at the base of the press, so
that the assembly rests on the retaining ring (26) at the aft end.
(b) Put the assembly in position so that the press ram engages the top surface of the piston
as close as possible to the piston center, but away from the open ends of the retaining ring
(11) at the piston end.
(c) Move the arbor press ram down to slightly compress the spring (21 or 23 and 24).
(3) Remove and discard the retaining ring (11) at the piston end.
(a) Release the arbor press ram until the pitch return spring(s) (21 or 23 and 24) is (are)
completely relaxed.
(4) Remove the remaining retaining ring (26).
(a) Move the low pitch stop spacer (12), piston, spring guides (20 or 22 and 25), and spring(s)
off the tube.
(b) Remove and discard the retaining ring (26) and O-ring (18).
B. Hub Assembly
(1) Remove and discard the piston rod to hub O-ring (29) and hub to engine shaft O-ring (67).
(2) Refer to the Standard Practice Manual, 61-11-20, Hub Disassembly, for procedures.
C. Blade disassembly

NOTE: There are two different style blade plugs. One is retained by a screw that is installed into
the blade butt. The second type uses an internal retaining ring that engages a groove in
the blade butt.

NOTE: Only oil filled propellers have blade plugs installed.

(1) If a retaining ring (58) is installed, remove it.

(2) If a screw (56) and washer (57) are used to secure the blade plug (54) to the blade butt, remove
them.

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(3) Insert a bolt or slide hammer with 1/4-28 threads (B-6052 and B-7090 plug) or 1/4 -20 threads
(B-6481 plug) into the hole at the center of the plug.
(4) Remove the blade plug (54).

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CLEANING

1. Cleaning
A. Refer to the following in the Blade Overhaul Manual (BOM100):
(1) Section 61-10-22, Special Instructions.
(2) Section 61-10-02, Inspection Procedures.
B. Refer to the following in the Standard Practices Manual (SPM100):
(1) Section 60-00-01, Cleaning Procedures.
(2) Section 60-00-02, Inspection Criteria.
(3) Section 60-00-22, Special Instructions.
(4) Section 61-11-02, Hub Inspection.

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INSPECTION/CHECK

1. Detailed Part Inspection

A. Do an inspection of the parts.
(1) Inspect all the parts for damage or defects.

NOTE: The types of damage and defects are given in Table 501, Table 502, and Table 503.

2. Bores and Diameters

A. Measure the bores and diameters.
(1) Make sure that the bores and diameters are in the limits shown in Table 501.

Table 501. Diameters

Index
Number Nomenclature Diameter - Inches (mm)
Inside Outside
8 Cylinder 4.2620 to 4.2635 (108.25 to
108.29 mm)
0.750 to 0.752 (19.05 to 19.10 4.247 to 4.250 (196.77 to
14 Piston
mm) Note 1 197.25 mm)
14 Piston Pin Holes (4) 0.5015 to 0.5025 (12.74 to
12.76 mm)
15 Piston Rod Pins 0.5000 to 0.5005 (12.70 to
12.71 mm)
19 Piston Rod Tube 0.7485 to 0.7495 (19.01 to
(each end) 19.03 mm)
60 Blade Actuating Pin 0.5010 to 0.5013 (12.72 to
12.73 mm)

NOTE 1: From the large diameter end to edge of the internal O-ring groove.

3. Nondestructive Inspection
A. Do an inspection of the parts.
(1) Examine all the steel parts by the magnetic particle process. Refer to the Standard Practices
Manual, Section 60-00-03, Non-Destructive Inspection Procedures.
(2) Examine all the aluminum alloy parts by the penetrant inspection process. Refer to the Standard
Practices Manual, Section 60-00-03, Non-Destructive Inspection Procedures .
(3) Examine the parts. Refer to Table 502 and the Standard Practices Manual, Section 60-00-02,
Inspection Criteria.

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Table 502. Propeller Assembly Inspection

Inspection
Additional
Procedures
Beyond Those
Index Part name Method Specified Acceptable Defects
2 Cylinder Visual None None. Strip and replate as necessary. Note 1
mounting
ring
3 Cylinder Visual None None. Strip and replate as necessary. Note 1
mounting
tubes
4 Balancing Visual None None. Strip and replate as necessary. Note 1
Ring
7 Balance Visual None Strip and replate as necessary. Note 1
weights
8 Cylinder Visual and Examine ID None. Strip and replate as necessary. Note 1
Magnetic for scratches,
spiral marks;
measure to check
out-of-round:
Check diameters
Table 501. Check
for dents or
deformation.
10 Support- Visual : None Some defects are allowed on steel support
spacer B-6911 spacers. Cracks on the edge of the inner hole
Support (where cylinder support is mounted on piston
Spacers rod) are permitted to 0.030 inch maximum depth
(aluminum) on this surface only. A maximum of four cracks
Visual and are permitted with 0.250 inch minimum spacing
Magnetic: between cracks.
B-7093
Support
Spacers
(steel)
12 Spacer - Visual None None
low pitch
stop
14 Piston Visual and Check O-ring None
Penetrant grooves for
damage; OD
and ID surface
smooth, free from
scratches. Check
diameters Table
501. Link ears not
deformed.

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Table 502. Propeller Assembly Inspection (continued)

Inspection
Additional
Procedures
Beyond Those
Index Part name Method Specified Acceptable Defects
15 Pin, piston Visual and Examine for Polish only. No breaks in plating. Do not replate.
Magnetic concentrated
wear; check for
out-of-round.
Check diameters
per Table 501.
19 Piston rod Visual and Check that tube None. Do not replate.
tube Magnetic is straight: OD
surfaces are
smooth; ring
grooves for
damage; examine
for plating damage.
Check diameters
per Table 501.
21, 23, Spring Visual, None None
24 Magnetic,
and load
testing
28 Spacer - Visual None None
high pitch
stop
36 Hub Refer to Standard
Practices Manual,
Section 61-11-02
Hub Inspection
45 Split Visual and Make sure that No surface ptting is permitted. Removal of
retainer Magnetic the retainer halves light surface corrosion is permitted. Remove
(matched have matching corrosion with fine scotch bright pads.
halves) serial numbers.
46 Blade Visual and None Only that which can be removed by light
retention Magnetic polishing.
bearing
49 Carrier, Visual None None
shim
53 Retaining Visual and None None. Strip and replate as necessary. Note 1
ring Magnetic

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Table 502. Propeller Assembly Inspection (continued)

Inspection
Additional
Procedures
Beyond Those
Index Part name Method Specified Acceptable Defects
60 Actuating Visual and Refer to Blade None. Replace pin assembly. Do not replate.
pin Penetrant Actuating Pin
assembly Assembly
Inspection
61 Blade Visual and Refer to Blade
Penetrant Overhaul Manual,
Section 61-10-02
Inspection
Procedures
101 Spinner Penetrant No cracks None

NOTE 1: Refer to the Standard Practices Manual, Section 60-00-04 Protective Treatments.

4. Spring Testing
A. Do a test on the springs to give the performance recorded in Table 503.
(1) If the spring load is not tested, mandatory replacement is required

Table 503. Spring Loads

Solid Height
Index
Maximum Load at compressed length Load at compressed length
Number
Inches (mm)
21 3.313 (84.15) 146 to 179 pounds at 4.930 649 to 796 N at 125.22 mm
inches and
282 to 345 pounds at 3.580 1254 to 1535 N at 90.93 mm
inches
23 3.094 (78.59) 140 to 156 pounds at 4.488 to 623 to 694 N at 114.00 to
4.508 inches 114.50 mm
283 to 298 pounds at 3.130 to 1259 to 1326 N at 79.50 to
3.150 inches 80.01 mm
24 2.870 (72.90) 172 to 188 pounds at 4.270 to 765 to 836 N at 108.46 to
4.290 inches 108.97 mm
272 to 288 pounds at 2.912 to 1210 to 1281 N at 73.96 to
2.932 inches 74.47 mm

5. Blade Actuating Pin Assembly Inspection

A. Do an inspection of the Blade Actuating Pin Assembly (refer to Figure 501).
(1) Examine the plating of the actuating pin for damage.

NOTE: Breaks in the plating are not permitted.

(2) Do a check of the dimension of the locating dowels. Refer to Figure 501.
(3) Measure the diameter and straightness of the actuating pin.
(a) Make sure that the diameter is in the limits shown in Table 501.
(b) Use a surface table, V-block and dial indicator to check the straightness of the pin (0.001
inch maximum total indicator reading).

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Blade Actuating Pin Assembly

Figure 501 (Sheet 1)

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1 For part number A-2973-8 actuating pins found to have an undersized diameter, the
pins may be replaced if the installed pin passes the 500 pounds (2224 N) press fit
test. If the installed pin fails this test, then the complete actuating pin assembly must
be replaced.
(4) Measure the depth of the steel pin with relation to the bottom of the base.
(a) Make sure that the measurement is between 0.0010 and 0.0000 inch (0.025 mm).
(b) Record the measurement.
(5) Fabricate a support with a hole that will give clearance for the actuating pin.
(a) Make sure the diameter of the hole is greater than the diameter of the pin.
(b) Align the hole with the pin so the pin will move freely through the hole.
(6) Use an arbor, or locally available equivalent device, to apply a force of 500 pounds (2224 N) on
the end of the pin (500 pound press fit test).
(7) Measure again the depth of the steel pin with relation to the base.
(a) If the depth has changed from the recorded measurement, replace the actuating pin
assembly.

NOTE: No modification or repair of the actuating pin assembly is approved.

(8) Do a check of the squareness of the pin with respect to the base.
(a) Make sure the measurement is less than or equal to 0.001 inch in a 1.000 inch length.

6. Spinner Dimension Checks

A. Spinner Identification (Refer to Figure 502)
(1) The dimensions provided in Figure 502 and Table 504 are for reference to assist personnel to
identify spinners.

Table 504. Spinner Identification

Spinner Shell Diameter Standoff (Shell Edge to Shell Length (Inside)

Assembly Mounting Flange)
D-3290 13.7 inches (349 mm) 1.4 inches (35 mm) 12.0 inches (305 mm)
D-3396 13.6 inches (345 mm) 0.9 inches (22 mm) 15.4 inches (392 mm)
D-5255 13.6 inches (345 mm) 0.9 inches (22 mm) 15.4 inches (392 mm)
D-5915 13.2 inches (335 mm) 1.1 inches (27 mm) 14.5 inches (368 mm)
D-6195 12.7 inches (324 mm) 0.8 inches (21 mm) 19.9 inches (505 mm)
D-7267 13.9 inches (353 mm) 4.5 inches (115 mm) Note 1 18.1 inches (458 mm)
D-7519 12.7 inches (324 mm) minus 0.5 inches (13 mm) 20.3 inches (515 mm)
D-7520 12.1 inches (307 mm) 1.8 inches (27 mm) 15.0 inches (38 mm)
D-7569 11.0 inches (279 mm) minus 1.1 inches (79 mm) 15.7 inches (399 mm)
D-7579 13.8 inches (351 mm) 2.8 inches (79 mm) Note 1 17.5 inches (445 mm)
D-7587 13.7 inches (349 mm) 1.3 inches (33 mm) 15.7 inches (400 mm)

NOTE 1: To the aft face of the hub bulkhead flange.

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Spinner Identification
Figure 502 (Sheet 1)

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Spinner Identification
Figure 502 (Sheet 2)

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Spinner Identification
Figure 502 (Sheet 3)

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Spinner Identification
Figure 502 (Sheet 4)

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Spinner Identification
Figure 502 (Sheet 5)

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REPAIR AND REPLACEMENT

1. Repair
A. For hub repair instructions refer to the Standard Practices Manual SPM100, Section 61-11-24, Hub
Repairs.
B. For blade repair instructions refer to the Blade Overhaul Manual BOM100, Section 61-10-24, Repair
and Replacement.
C. For refinishing instructions refer to the Standard Practices Manual SPM100, Section 60-00-04,
Protective Treatments.
D. Perform repairs as specified in Inspection/Check, Table 502.

2. Change Letter Stamping

A. Change Letter Stamping
(1) Propeller change letter stamping is required after a propeller is assembled.
(2) Change letter requirements must be reviewed prior to assembly. Stamping requirements may
be affected by part usage which may be internal and would not be visible after assembly.
(3) Change letter information may indicate the following:
(a) "Not Applicable to Field"
1 Minor Engineering changes which do not affect the field. These changes will be
identified as in the description and do not require stamping on hub.
(b) "Not used"
1 Change letter was not used for any production propeller.
(c) "At manufacture date"
1 Change letter configuration was incorporated at the time of manufacture.
(4) Changes may be listed as mandatory. These changes must be accomplished at the compliance
time listed.
(5) Changes which are not mandatory are to be accomplished as needed and appropriate change
letter stamped at that time.
(6) Change letters do not affect the eligibility or interchangeability of propellers.
(7) Review the following change letter stamping requirements and the Master Parts List prior to
stamping change letter.
(8) Refer to the Section 61-11-26 Hub Reassembly, in the SPM100 for the correct hub stamping
procedure.

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Table 601. Change Letter Stamping Requirements

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C201 A Not used
C201 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 manual.
C201 C Requirement to oil fill, Modify hub to oil fill Yes Next
configuration (see Note 1). overhaul
The following parts are added/replaced: or major
A-1633-58 O-ring disassembly.
A-1633-76 O-ring
A-1633-109 blade O-ring replaces P/N A-1633-
96
A-1635-36 screw
A-1635-86 screw
A-1637-11 red dyed oil, 1000cc (1.05 qts)
A-1638-18 washer
A-1664-15 sealant
A-1750-4 seal washer
A-4714 pipe plug
B-4746 slot block
B-6480 cylinder gasket replaces P/N B-4138
B-6481 blade plug
B-6494 oil fill decal
A-6590 patch
B-6631 cylinder mounting ring
C-6549 cylinder replaces P/N C-5263 (see Note
3).
C-6560 balance ring replaces P/N C-5727 (see
Note 3)
Modify the blades per BOM100 manual (drill
weep hole and blade plug attachment hole).
C202 A Not used
C202 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
The propeller blade shank must be modified to
"G" configuration, refer to BOM100 Manual.
C203 A Not used
C203 B The following parts are added/replaced: No
C-5270 bearing races replaces P/N C-3411
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
The propeller blade shank must be modified to
"G" configuration, refer to BOM100 Manual.

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C203 C Requirement to oil fill hub, modify hub to oil fill Yes Next
configuration (see Note 1). overhaul
The following parts are added/replaced: or major
A-1633-58 O-ring disassembly.
A-1633-76 O-ring
A-1633-109 replaces P/N A-1633-96
A-1635-36 screw
A-1635-86 screw
A-1637-11 1000cc (1.05 qts) red dyed oil
A-1638-18 washer
A-1664-15 sealant
A-1750-4 seal washer
A-4714 pipe plug
A-6590 patch
B-4746 slot block
B-6480 cylinder gasket replaces P/N B-4138
B-6481 blade plug
B-6631 cylinder mounting ring
B-7367 oil fill decal
C-6549 cylinder replaces P/N C-5263 (see Note
3)
C-6560 balance ring replaces P/N C-5727 (see
Note 3)
Modify blade per BOM100 manual (blade plug
attachment hole)
C204 A Not used
C204 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C204 C Requirement to oil fill, modify hub to oil fill (see Yes Next
Note 1) overhaul
The following parts are added/replaced: or major
A-1633-58 O-ring disassembly.
A-1633-76 O-ring
A-1633-109 blade O-ring replaces P/N A-1633-
96
A-1635-36 screw
A-1635-86 screw
A-1637-11 red dyed oil, 1000cc (1.05 qts)
A-1638-18 washer
A-1664-15 sealant
A-1750-4 seal washer
A-4714 pipe plug
A-6590 patch
B-4746 slot block
B-6480 cylinder gasket replaces P/N B-4138
B-6481 blade plug
B-6631 cylinder mounting ring
B-7367 oil fill decal
C-6549 cylinder replaces P/N C-5263 (see Note
3)
C-6560 balance ring replaces P/N C-5727 (see
Note 3)
Modify blade per BOM100 Manual (blade plug
attachment hole)
C205 A Not used
C205 B The following parts are added/replaced: No
C-5270 bearing races replaces P/N C-3411
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C205 C Requirement to oil fill propeller, modify hub to Yes Immediately,
oil fill configuration (see Note 1) refer to
The following parts are added/replaced: SB191
A-1633-58 ) O-ring Compliance
A-1633-76 O-ring
A-1633-109 blade O-ring replaces P/N A-1633-
96
A-1635-36 screw
A-1635-86 screw
A-1637-11 red dyed oil, 1000cc (1.05 qts)
A-1638-18 washer
A-1664-15 sealant
A-1750-4 seal washer
A-4714 pipe plug
A-6590 patch
B-4746 slot block
B-6480 cylinder gasket replaces P/N B-4138
cylinder gasket
B-6481 blade plug
B-6631 cylinder mounting ring
B-7367 oil fill decal
C-6549 cylinder replaces P/N C-5263 (see Note
3)
C-6560 balance ring replaces P/N C-5727 (see
Note 3)
Modify blade per BOM100 manual (weep hole
and blade plug attachment hole)
C206 A Not used
C206 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual
C207 A Not Applicable to Field
C207 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual
C208 A Not Applicable to Field
C208 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C209 A Not used
C209 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual
C209 C Requirement to oil fill propeller, modify hub to Yes Next overhaul
oil fill configuration (see Note 1) or major
The following parts are added/replaced: disassembly.
A-1633-58 O-ring
A-1633-76 O-ring
A-1633-109 blade O-ring replaces P/N A-1633-
96
A-1635-36 screw
A-1635-70 cylinder screws replaces P/N
A-1635-77
A-1635-86 screw
A-1637-11 red dyed oil, 1000cc (1.05 qts)
A-1638-18 washer
A-1664-15 sealant
A-1750-4 seal washer
A-4714 pipe plug
A-6590 patch
B-4354-1 cylinder mounting tubes replaces P/N
B-4354-3
B-4746 slot block
B-6480 cylinder gasket replaces P/N B-4138
B-6481 blade plug
B-6631 cylinder mounting ring
B-7367 oil fill decal
C-6549 cylinder replaces P/N C-5263 (see Note
3)
C-6560 balance ring replaces P/N C-5727 (see
Note 3)
Modify blades per BOM100 Manual (blade plug
attachment hole)
C210 A Not Applicable to Field
C210 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual
C211 A Not Applicable to Field

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C211 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to BOM100 Manual
C212 A Not Applicable to Field No
C212 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C213 A Not Applicable to Field
C213 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C214 A Not Applicable to Field
C214 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C215 A Not used
C215 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C216 A Not used
C216 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C217 A Single spring to dual springs configuration Yes Next
The following parts are added/replaced: overhaul
A-4501 and A-4502 springs replaces P/N A- or major
3125 spring disassembly
A-4503 front spring guide and A-4989 rear
spring guide replaces P/N A-3124 spring guides
C217 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
ball
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C218 A At manufacture date No
C218 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C219 A At manufacture date
C219 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C220 A Not used
C220 B The following parts are added/replaced: No
A-1634-9 ball bearings replaces P/N A-1634-6
B-5223 ball separators replaces P/N B-4014
C-5270 bearing races replaces P/N C-3411
Blade shank must be modified to "G"
configuration, refer to the BOM100 Manual
C221 B At manufacture date
C223 B At manufacture date

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C223 C Requirement to oil fill propeller, modify hub to Yes Immediately,
oil fill configuration (see Note 1) refer to AD
The following parts are added/replaced: 95-09-08
A-1633-58 O-ring
A-1633-99 O-ring
A-1633-109 blade O-ring replaces P/N A-1633-
96
A-1635-36 screw
A-1635-86 screw
A-1637-11 red dyed oil, 940cc (0.99 qts)
A-1638-7 washer
A-1664-15 sealant
A-1750-4 seal washer
A-4714 pipe plug
A-6494 oil fill decal
A-6590 patch
B-4354-1 cylinder mounting tubes
B-4746 slot block
B-6480 cylinder gasket replaces P/N B-4138
B-6631 cylinder mounting ring
B-7090 blade plug
B-7092 actuating pin and base assembly
(B-7091 actuating pin base) replaces the
B-3905 actuating pin and base assembly
(B-3427 actuating pin base)
B-7093 spacer support replaces P/N B-6911
B-7094 piston rod tube replaces P/N B-2345
C-6549 cylinder replaces P/N C-5263 (Note 3)
C-6560 balance ring replaces P/N C-6440(-A)
Modify blade to per BOM100 manual (drill weep
hole and blade plug attachment hole)
C224 B At manufacture date
C225 None
C227 B At manufacture date

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C227 C Requirement to oil fill propeller, modify hub to Yes Next
oil fill configuration (see Note 1) overhaul
The following parts are added/replaced: or major
A-1633-58 O-ring disassembly.
A-1633-76 O-ring
A-1633-109 blade O-ring replaces P/N A-1633-
96
A-1635-36 screw
A-1635-86 screw
A-1637-11 red dyed oil, 1000cc (1.05 qts)
A-1638-18 washer
A-1664-15 sealant
A-1750-4 seal washer
A-4714 pipe plug
A-6590 patch
B-4746 slot block
B-6480 cylinder gasket replaces P/N B-4138
B-6481 blade plug
B-7367 oil fill decal
C-6549 cylinder replaces P/N C-5263 (see Note
3)
C-6560 balance ring replaces P/N C-5727 (see
Note 3)
Modify blade per BOM100 manual (blade plug
attachment hole)
C228 None
C229 B At manufacture date
C230 B At manufacture date
C231 B At manufacture date
C232 A At manufacture date
C233 A At manufacture date
C234 A At manufacture date
C235 A At manufacture date
C235 B At manufacture date
C236 None
C238 None

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Table 601. Change Letter Stamping Requirements (continued)

PROP DETAILS/
MODEL CHANGE MANDA- COMPLI-
NUMBER LETTER DESCRIPTION TORY ANCE TIME
C239 None
C240 None
C241 None

NOTE 1: Original part number propeller hub can be modified to an oil fill configuration, refer to SPM100 manual.

NOTE 2: C-5263 cylinders can be used with C-6911, C-5271 or B-4643 support spacers C-4645 cylinders can
be used with C-6911, C-5271 or B-4643 support spacers C-4129 cylinders can be used with C-6911,
C-5271, B-4643 or B-3526 support spacers.

NOTE 3: Oil fill configuration C-5263, C-4645, and C-4129 cylinders can be modified and used in place of
C-6549 per Repair section. C-5727 balance ring can be modified into C-6560 per Repair section.

3. Modification of Propeller to Oil Filled

A. Hub Pipe Plug Hole (Refer to Figure 601).
(1) Locate the hole per Figure 601.
(2) Before drilling, mark the hole location with a center punch.
(3) Secure the hub in a drill press so that the hole will be square with centerlines of blade sockets
and cylinder.
(4) Drill the hole with size Q (0.332 inch diameter) drill bit.
(5) Use a small 45-degree burring reamer to remove burrs from each end of the hole.
(6) Carefully tap hole with 1/8-27 NPTF (4 flutes) tap to a depth that will leave the top of the plug
protruding within 0.030 inches (0.76 mm) from the hub surface when tightened.
(a) The pipe plug (A-4714) can be effectively used as a depth gauge.
(b) If the hole is oversize, a slightly oversize pipe plug (part number A-4714-1) is available
and, when installed, may protrude more than 0.030 Inches.
B. Hub Breather Holes and Cylinder Thru-Holes
(1) Hubs converted must have breather holes plugged.
(a) Make sure the roll pin has been removed.
(b) Clean the breather hole with MPK.
(c) Squeeze RTV #109 into one side of each hole until it is seen exiting the opposite end of
the hole.
(d) Remove excess sealant and allow to cure for a minimum of 12 hours.
(2) Cylinder Mounting Through-Holes

NOTE: Some earlier C200 hubs have four through-drilled cylinder mounting holes. These
four holes must be sealed to prevent oil leakage.

(a) Thoroughly clean the four through-drilled holes with MPK (methyl propyl ketone) and allow
to dry.
(b) Make sure that hardware is clean and dry.
(c) Temporarily install A-1635-21 screws and A-1638-7 washers in the four affected cylinder
holes in the hub.

NOTE: These temporarily installed screws and washers only insure proper sealant
penetration of holes. They are NOT to be used for actual cylinder installation.

(d) Pack holes from inside hub with RTV #109 sealant, guarding against trapped air pockets.
(e) Mound sealant around hole inside hub to form a small "button" of excess material.
(f) Allow sealant to cure a minimum of twelve hours.
(g) After curing, remove all screws and washers.

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Hub Modification and Repair

Figure 601 (Sheet 1)

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C. C-5263 Cylinder Modification (Refer to Figure 602).

NOTE: A C-6549 cylinder may be purchased and installed instead of modifying a C-5263 cylinder.

NOTE: The additional holes are required to secure the cylinder to the slot blocks.

(1) Drill holes 0.172 to 0 182 inch (4.37 to 4.62 mm) diameter as shown.
(2) Break hole edge 0.010 inch on the face side only.
(3) Re-identify with part number C-6549.
D. C-5727 Balance Ring Modification (Refer to Figure 603).

NOTE: A C-6560 balance ring may be purchased and installed instead of modifying a C-5727
balance ring.

NOTE: The modification allows installation of screws that secure the slot blocks.

(1) Remove material in two locations as shown in Figure 603.

(2) Locate balance ring centerline.
(3) Remove 0.250 inch (6.35 mm) material on each side of centerline.
(4) The cut must continue approximately 0.250 inch into radius area as indicated.
(5) Radius corner 0.063 to 0.094 inch (1.60 to 2.39 mm).
(6) Re-identify balance ring with part number C-6560.

4. Replacement
A. Replace all parts for which the repair would have an effect on the operation or serviceability. The parts
listed in Table 602 must be replaced at each overhaul.
(1) Replace all parts that have cracks.
(2) Replace the chrome-plated parts on which the plating is broken, chipped, or peeled to expose
the base metal.
(3) Replace cadmium-plated parts on which cleaning and repair has exposed the base metal, if
replating is not possible.
(4) Replace the ball races that have extensive brinelling or other damage not readily repaired without
affecting the serviceability.
(5) Replace the parts that have dimensions outside the limits given in the Inspection/Check, Table
501.

Table 602. Mandatory Replaced Parts

Index Number Name

1 Screw, Cylinder attaching
5 Screw, balance weight
6 Nut, balance weight
9 Cylinder gasket
11, 26 External retaining ring
13 O-ring (piston)
16 Roll pin (piston)
17 Link, blade actuating
20 Spring guide
22 Spring guide, front
25 Spring guide, rear

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Table 602. Mandatory Replaced Parts (continued)

Index Number Name
18, 29 O-ring (piston to hub, tube to hub)
27 Fiber Washer
30 Screw, slot block
31 Stat-O-Seal
32 O-ring (slot block)
37 Stud
38 Washer
39 Nut
40 Roll pin (hub)
41 Dowel (hub alignment)
43 Roll pin (hub)
44 O-ring (blade to hub)
47 Ball bearing
48 Ball separator
55 O-ring (plug to blade)
56 Screw
57 Washer
59 Screw (12 point)
62 Patch
63 Decal
64 Decal, Installation
65 Decal, Part number
66 Decal, Warning
66 Decal, Notice
67 O-ring
68 Nut, mounting
105 Screw
106 Washer
111 Screw
112 Washer
113 Bolt
114 Washer
115 Nut
116 Decal, Installation

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Cylinder Modification for Oil Fill

Figure 602 (Sheet 1)

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Balance Ring Modification for Oil Fill

Figure 603 (Sheet 1)

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5. Replacement of C-3411 Bearing Races With C-5270 Bearing Races

A. General.
(1) C-3411 bearing races were installed on C201 through C220 propellers manufactured before April
1982. Those propellers that do not have a prefix letter G stamped on the butt of the blade must
be modified before you install C-5270 bearing races as a replacement.
(a) The following model propellers may be modified.

2A34C201/90DA 2D34C202/82PA 2A34C203/90DCA C2A34C204/90DCB

B2A34C205/90DHA B2D34C206/78TA B2D34C207/78TCA B2D34C208/82PA
2A34C209/78CCA 2A34C210/78CCA B2DC211/82PCA B2D34C212/78CDA
B2D32C213/90DHA B2D34214/90DHB 2D34C215/90DJA 2A34C216/90DHB
B2D34C217/90DHB B2D34C218/90DHB B2D34C219/90DHB B2D34C220/80VHB
(2) C-3411 bearing races require 40 bearings and spacers with a smaller diameter than the A-1634-
9 balls and B-5223 spacers. The replacement bearing races require 32 each balls and spacers.
(3) The blade shank must be modified as shown in the BOM.
(4) You must not use two different part number bearing races on the same propeller.

6. Refinishing
A. Refinish parts as specified in Inspection/Check, Table 502 per the Standard Practices Manual, Section
60-00-04 Protective Treatments.

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ASSEMBLY

1. Assembly
A. Refer to the Illustrated Parts List, Figure 1001.

NOTE: The numbers in the parentheses show the index numbers for the parts in the instructions.
(Refer to the Illustrated Parts List.)
B. Use Propellers - Description And Operation, Table 601, Change Letter Stamping Requirements and
the Illustrated Parts List, Table 1001, Notes, for the mandatory part changes and compliance.

CAUTION: Make sure that only permitted and correct parts are used for the propeller
assembly.
C. Use the Illustrated Parts List, Tables 1002 through 1009, for permitted part combinations and uses.
D. Perform assembly on clean surfaces.
E. All lockwiring is to be accomplished using 0.032 inch diameter corrosion resistant steel lockwire.

Table 701. Assembly Torque Values

Index Part Name Part Number Torque

Number
1 Cylinder screws A-1635-70 30 to 36 inch-pounds (3.39 to 4.06
N.m)
5 Balance weight screws A-1635-X 20 to 24 inch-pounds (2.26 to 2.71
N.m)
30 Screw, cylinder to slot A-1635-86 20 to 24 inch-pounds (2.26 to 2.71
block N.m)
34 Screw, cylinder and A-1635-207 30 to 36 inch-pounds (3.39 to 4.06
gasket N.m)
42 Pipe plug A-4714 50 to 55 inch-pounds (5.65 to 6.21
N.m)
56 Screw, blade plug A-1635-36 20 to 24 inch pounds (2.26 to 2.71
N.m)
59 Actuating pin screws A-1635-113 160 to 180 inch-pounds (18.1 to 20.3
N.m)
59 Actuating pin screws A-1635-171 160 to 180 inch-pounds (18.1 to
20.3 N.m)

NOTE 1: Torques are based on clean, dry, and undamaged threads. Damage may result if these torque values
are used on lubricated threads.

2. Hub Assembly
A. Assemble the hub assembly per Standard Practices Manual, Section 61-11-26, Hub Reassembly.
B. Install bulkhead/slipring adapters as required. Torque screws per Table 701, Assembly Torque Values.
C. Install hub to piston rod O-ring after lubricating with Orelube K-2 before you install the O-ring.

3. Piston Assembly
A. Assemble Piston Assembly

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(1) Install one retaining ring (26) in the groove of the piston rod (19) at the end of the piston rod with
the longer distance to the end of the part.
(2) Apply a thin film of Orelube K-2 to O-ring (18) and install in the groove in piston (14) bore.
(3) Install in the following order on the piston rod (19), one spring guide (20 or 25), spring (21 or
23 and 24), the second spring guide (20 or 22), and piston (14) (with O-ring (18) installed in the
inside diameter).

NOTE: Make sure the chamfered end of the spring faces forward (is adjacent to the piston).

(4) Non-oil filled propellers: Apply a coating of Aeroshell 5 grease to the spring (21 or 23 and 24)
and piston rod (19).

CAUTION: The compressed spring is dangerous.

(5) Put the assembly in an arbor press with the piston (14) facing up.
(a) Supply a plate with a hole large enough for the piston rod tube to slip fit into, at the base
of the press, so that the assembly rests on the retaining ring (26) installed at the aft end.
(b) Put the assembly in position so that the press ram engages the top surface of the piston as
close as possible to the piston center, but with enough space to install retaining ring (11)
at the piston end.
(6) Compress spring enough to install low pitch stop spacer (12) and retaining ring (11) in the groove
of piston rod (19).
(7) Remove assembly from the arbor press and set aside for installation in the propeller assembly.

4. Propeller Assembly
A. Bearing Installation.

NOTE: If the parts are serviceable, assemble the same blades and retention parts in the same
hub and hub socket from which they were removed.

(1) Install an O-ring (29) in the hub.

(2) Install hub assembly on propeller assembly tool, D-4661, with No. 1 blade socket up.

CAUTION: Inner and outer bearing races (46) are to be used only in
matched sets. Make sure that the inner race is matched with the
corresponding outer race. Be certain that ball races face each
other.
(3) Apply Orelube K-2 to the convex sides of the outer races (46).
(4) Insert both matched sets of races (46) through the slots in the cylinder end of the hub as follows:

NOTE: Both sets of bearing races must be inserted before you press the first into the socket.

(a) Insert the number 1 outer race first then the corresponding inner race.
(b) Hold the pair of races by hand in the hub with ball races facing each other until the second
set of races is inserted.
(c) Insert the number 2 outer race and then the corresponding inner race.
(d) Support the number 1 inner and outer races and the number 2 inner race with spatulas
and rubber bands. (Refer to Figure 701)
(e) Put the number 2 outer race in position in the number 2 hub socket.
(5) Seat the outer races, one after another, as follows: (Refer to Figure 702)
(a) Insert the adapter, part number C-4696-3, into the hub.
(b) Insert the inner bearing race pressing tool, Part Number C-4696-2 into the hub.
(c) Position the pressing tool against the ball-race side of the outer race.
(d) Make sure the pressing tool pilot is in the bore of the adapter and the convex (rounded)
side of the adapter is in the outer race.

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Supporting Bearing Races

Figure 701 (Sheet 1)

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Bearing Seating Tool

Figure 702 (Sheet 1)

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(e) Install the outer bearing race pressing tool, C-4696-1, in the hub socket and install bolts
and nuts as shown in Figure 702.
(f) Hold the bolt heads and tighten the nuts to seat the outer race.
(g) Loosen bolts and rotate pressing tools to several positions.
1 Tighten the pressing tool at each position.
(h) Insert a rag into the hub to protect from damage by the pressing tool.
(i) Remove the outer pressing tools (do not remove the inner tool from the hub).
(j) Use a 0.001-inch feeler gage to probe between the seated outer race and the hub all around
the circumference.
1 If the feeler gage cannot be inserted between the outer bearing race and the hub, the
race is properly seated.
(k) When outer race is properly seated, position matched inner race against outer and hold it
with spatula and rubber band.
(l) Seat the outer race in the other socket, following the same procedure.
(6) After both outer races (46) are properly seated, and the matched inner races secured with them,
remove the inner pressing tool and adapter from the hub.
(7) Turn assembly tool to locate one hub socket facing down.
(8) Remove spatula and rubber band from the down facing socket. Place the inner race at another
socket and temporarily hold with another spatula and rubber band.

CAUTION: It is most important that 32 bearing balls and separators are installed
in each bearing. Failure to install the correct quantity will result in
improper operation and may result in damage to the blade, to the
hub, or to internal parts.
(9) Non-Oil filled hubs, apply a thin layer of Aeroshell 5 grease to just fill the concave part of the ball
race of the outer race.
(10) Install 32 each balls (47) and separators (48) in the outer race.
(11) Non-Oil filled hubs, apply a thin layer of Aeroshell 5 grease to just fill the concave part of the of
the inner race.

NOTE: Do not apply too much grease. If more is used, it will be thrown out of the bearing
race by centrifugal motion and may cause grease leakage at the blade root.

(a) Put the inner race in place against the balls.

(b) Secure the inner race with spatulas and rubber band. (Refer to Figure 701)
(12) Install the balls and spacers in the remaining hub socket.
(13) Wipe off all grease that has squeezed out of the bearing races.
(14) Apply a thin coating of Orelube K-2 to the inner diameter surfaces of the bearing races.
B. C201, C205, C223 Blade Patch Installation
(1) These propeller blades have a hole drilled just outboard of the retaining ring groove that extends
into the blade bore. The purpose of this is to provide blade shank crack detection, by allowing
dyed red oil which may collect in the blade bore to escape. Any dyed oil that escapes is an
indication of a crack in the blade shank.
(2) Blade Patch Installation
(a) Thoroughly clean the oil escape hole and the area around it with MPK.
(b) Apply 1300L adhesive to the area of the blade shank on either side of the oil escape hole.
Use care to not plug the hole with the adhesive.
(c) Apply 1300L adhesive to one side of the blade patch (62).
(d) Allow the adhesive to dry until it is no longer tacky.
(e) Apply another coating of 1300L adhesive to the blade patch (62), and position it so it is
centered over the oil escape hole.
(f) Allow the blade patch to cure for a minimum of 12 hours.

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CAUTION: Failure to puncture the patches exactly as described,

completely negates the early crack detection of blade shanks.
(g) Use a 0.060 to 0.065 inch (1.5 to 1.6 mm) diameter needle to puncture a hole in the patch
at the center of the oil escape hole.

NOTE: The hole is small enough to prevent moisture from entering the hole but will
allow any oil that accumulates in the blade bore to be thrown out due to normal
centrifugal loads.

(h) Apply a small quantity of blue sentry seal to the edge of the patch to provide a visual
indication that the patch has been punctured.
C. Use of H-90DHA blades on C213 Propellers
(1) H-90DHA blades have a hole drilled for leak detection when installed on C205 propellers. When
this blade is installed on C213 propellers, the hole must be plugged as follows:
(a) Inject RTV 109 sealant into the hole to a depth of 0.25 to 0.5 inch (6 to 13 mm).
(b) Make sure the outside surface of the sealant is flush with the outer surface of the blade
shank.
D. Blade Installation (Refer to Figure 706).
(1) Blade Plug Installation for oil filled models.

NOTE: Two types of blade plugs are installed.

(2) Blade plug retained by an external retaining ring.

(a) Apply a thin film of Orelube K-2 to the O-ring (55) and groove of the plug (54) and to the
inner diameter of the blade bore.
(b) Insert the blade plug (54) into the blade bore.
(c) Install the retaining ring (58).
(3) Blade plug retained by screw (56) and washer (57).
(a) Apply a thin film of Orelube K-2 to the O-ring (55) and groove of the plug (54) and to the
inner diameter of the blade bore.
(b) Insert the blade plug (54) into the blade bore with the screw hole correctly located.
(c) Apply Loctite Gasket Sealant #2 to the threads of the screw (56).
(d) Install washer (57) and screw (56) and torque screw. Refer to Table 701.
(4) Clean each blade (61) butt with methyl n-propyl ketone or other approved solvent.
(a) When the solvent is dry, cover the inboard section of each shank with blade wrap, Part
Number B-4120, out to the 9 inch station.
(5) With butt end up, install parts on blades in the following sequence, allowing them to rest on the
protective wrap:
(a) Retaining ring (53), wire ring (52), shims (51, 50) (the same shims as removed or new
shims of the same thicknesses), and shim carrier (49). Make sure that the cup of shim
carrier faces toward blade tip.

CAUTION: Shim thicknesses must be chosen to limit blade shake and so that
the bottom edge of shim (51) is ALWAYS below the top of the carrier
(49) (refer to Figure 703). One or two split shims (50) are permitted.
If the thickest (0.020 inch) is not enough, use a thicker solid shim
(51) and select a thinner split shim (50) that will be suitable. If two
split shims are used, the thinner must be put closest to the hub.
NOTE: For initial assembly use a 0.063-inch thick shim (51).

NOTE: Thicknesses should be chosen to avoid the necessity for changing shims. The blade
must be removed from the hub to change this shim.

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Position of Parts for Installation of Split Retainer

Figure 703 (Sheet 1)

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(6) Carefully open wire ring (52) and install in groove of blade (61).
(7) Apply lubricant, Orelube K-2 on O-ring (44) and install the O-ring in the groove of the blade butt
or in the hub socket.
(8) Apply a thin coat of Orelube K-2 on the blade butt from the O-ring inboard, all shims, shim carrier,
and inside diameter of hub sockets.
(9) Wash both split retainer ring halves (45 - matched pair) in solvent and dry.
(10) Apply lubricant, Orelube K-2, lightly to the split retainer halves.

NOTE: It is important that bearing parts (inner race, balls, spacers) be held in position while
the blade butt is inserted and moved for installation of retainer ring halves.

(11) With hub socket number 1 facing down, remove the spatulas from the number 1 socket.
(12) Insert the blade up through the hub and bearing races so that the butt end is approximately 0.5
to 1 inch (13 to 25 mm) farther in the hub than the normal position.
(13) Hold the blade in this position, and install the split retainer (45) as follows:

CAUTION: Split retainer halves (45) are manufactured as matched sets and
must be installed as a matched pair (identifiable by serial numbers
etched on outside diameter).
(a) Insert one retainer-half through the front hub opening with the square (non-radiused) step
on the outer diameter facing down, toward the blade tip (Refer to Figure 703).
(b) Position the retainer-half over the collar of the blade butt so that its centerline coincides
with that of the butt.
(c) Grasp the retainer-half at its approximate center and move it out (away from center)
allowing ends of the retainer-half to drop down (angle of approximately 45 degrees)
toward the blade recess below the collar.
(d) Move the retainer-half down, starting at the open ends, into the blade recess. Continue
until the retainer-half seats on the collar ledge in the recess.
(e) Slide retainer-half around the collar to the rear of hub (opposite cylinder opening).
(f) Install the second half in the same manner.
(g) Lower the blade, allowing the split retainer to engage the bearing inner race.

CAUTION: Be careful not to scratch the blade as you move the retaining ring
(53) to engage the groove in the butt. Retaining ring corners are
sharp. If blade shank is scratched by installation of the retaining
ring, the scratch must be polished out and blade shank refinished
(refer to the blade overhaul manual). Scratches are focal points for
corrosion and for the start of fatigue cracks.
(14) Using Snap-On PR8 pliers, carefully expand the retaining ring (53) and install the ring in the
groove in the blade butt.
(15) Rotate the hub and install blades in socket 2 using the same procedure as the first blade.

5. Blade Shimming
A. Seat bearings and tighten the blades to reduce blade shake in the following manner: Refer to Figure
704).
(1) Insert the thick end of the wedge, Part Number C-4099-2, into the hub to rest on the end of one
blade butt.
(2) Slide the longer wedge, Part Number C-4099-1, into the hub between the blade butt and the
other wedge. The inclined faces of both wedges must be against each other.
(3) Tap end of longer wedge with reasonable mallet blows to wedge the blade butts apart and
completely seat the bearings and retainers.

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Bearing Race Seating

Figure 704 (Sheet 1)

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(4) Use a feeler gauge between retaining ring (53) and shim (51) to determine if a thicker split shim
(50) is required. Remove retaining ring (53) and install appropriate split shim (50). Reinstall
retaining ring (53). Refer to Figure 704.
(5) Withdraw seating tools.
(6) Rotate blades back and forth by hand approximately 180 degrees to check proper seating and
operation of the bearings. Rotate each blade 5 times.

6. Blade Shake Check

A. Blade Shake Check.
(1) Position hub so that one blade is straight up.
(2) Hold a wood block (2 x 4-inch nominal) against blade tip with wood grain at right angles to the
blade width. Tap lightly with a mallet to loosen the retention parts preparatory to blade shake
measurement. Suspend or fix a scale slightly above blade tip and, with fingers, move blade tip
back and forth and record total movement.

NOTE: Exert force in a direction in line with blade width, not against blade thickness, to avoid
bending blade.

(3) If total movement exceeds 0.031 inch (an arbitrarily selected amount), install a thicker split shim
(50) and recheck blade shake.
(a) After installation of a thicker split shim, make sure that excessive torque is not required
to rotate the blade (not to exceed 120 inch-pounds (13.6 N.m)). Refer to Blade Friction
Rotation Check.
(4) If the use of the thickest split shim (50) (0.020 inch) does not reduce the blade shake to an
acceptable amount, or if it locates the bottom surface of the shim (51), outboard of the cup of
the shim carrier (49), then a thicker shim (51) and a thinner split shim (50) must be used.

CAUTION: With the parts at the most disadvantageous limit of their respective
tolerances, it is possible that the top of the thickest shim (51) will be
outboard of the cup of the shim carrier (49). As this condition is not
permitted, whenever the 0.018 or 0.020 inch split shim (50) appears
to be required, make a very careful determination that the top of the
split shim will be inboard the cup of the carrier when installed. If split
shim (50) is not entirely within the cup of the shim carrier, the split
shim (50) could shift radially far enough for an arc to be beyond the
retaining ring (53). This would be a dangerous condition.
(5) Disassemble propeller as necessary to replace shims (50 and 51) so that blade shake is
acceptable, and bottom surface of shim (52) is inboard the cup of shim carrier (49). Only 1 of
shim (51) can be used for each blade, 1 or 2 shims (50) can be used with the thinner shim on
the bottom of the carrier.
(6) Repeat the procedure for the remaining blades.

7. Blade Rotation Friction Check

A. Check each blade as follows:
B. Slide a blade torque gage, Part Number B-2399, on the blade to station 30. Install a standard torque
wrench on hex of the torque gage and measure the torque required to rotate blade in the bearing.
Compute the actual torque on the blade from the wrench dial reading as follows:

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C. The actual torque (TB) to rotate the blade must not exceed 120 inch-pounds (13.6 N.m).

8. Install Actuating Pin

A. Install Actuating Pin Assembly.
(1) Immerse links (17) in lubricating oil for a minimum of one hour before you begin assembly.
(2) Lubricate actuating pins (60) and bearing bores of links (17) with a thin film of Orelube K-2.
(3) Clean blade butts with lint free, non-oil based solvent-dampened cloth.
(4) Install links (17) on actuating pins (60).
(5) Insert the aligning pins of the actuating pin assembly (60) into the holes of the blade butt.
(6) Install the screws (59) and torque as indicated in Table 701.
(7) Safety wire the screws (59) together.

9. Pitch Control Parts Installation

A. Complete installation of remaining parts in the hub as follows:
(1) Slide high pitch stop spacer (28) over spring of piston-rod group. Install fiber washer (27) on
rear end of piston rod tube (19) against retaining ring (26). Partially insert piston pins (39) on
piston assembly (piston pins cannot be inserted after piston assembly is installed in hub).
(2) Install piston-rod assembly through the hub opening and into the rear of the hub.
(3) Rotate blades to bring free ends of links (17) into slots of piston (14) and install pins (15).
(4) Insert roll pins (16) to secure the link pins.
(a) Use tool B-4092-1 to align holes of piston rod pin (15) with those in the piston (14).
(b) Insert a roll pin (16) in B-4092-2 Assembly Tool, and start the roll pin into the hole.
(c) Remove the B-4092-2 Assembly Tool and use a B-4092-3 Assembly Tool to tap the roll pin
in to be flush with piston ear.
(d) Install the other roll pin in a similar manner.
(5) Lubricate piston (14) groove and O-ring (13) with Orelube K-2 and install the O-ring in groove.
Be sure there is no twist in the O-ring.
(6) Locate gasket (9) on hub so that ears cover slots and holes align with hub.

NOTE: Oil-filled propellers must use an old gasket. This will be replaced when all adjustments
have been completed.

(7) Install support spacer (10) on the end of the piston rod (19), with the radius side facing forward.
(8) Lubricate the inside of the cylinder (8) with Orelube K-2, slide it over piston (14), align with holes
of gasket and hub and install at least four screws No. 10-24 x 5/8 inch spaced at 90 degrees.
(9) Check blade angles.
(a) If adjustment is required, refer to Pitch Stop Adjustment.

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(10) Check blade track. Refer to the Standard Practices Manual, Blade Track and Blade To Blade
Balance .
B. Non-oil filled propeller cylinder final installation
(1) After test procedure is completed, install tubes (3), cylinder ring (2), balance ring (4) and screws
(1).
(2) Tighten all screws uniformly with torque given in Table 701.
(3) Lockwire screws together in groups of two or three.
C. Oil filled propeller cylinder final installation.
(1) After checking and setting blade angles, remove cylinder and clean cylinder/hub mounting
surface with an approved solvent and allow to dry.
(2) Apply Loctite Gasket Sealant #2 generously to each side of a new, unused B-6480 or C-7380
cylinder gasket (9). Applying sealant too sparingly or neglecting to coat both sides of the gasket
thoroughly may result in leakage.

NOTE: The cylinder gaskets are a specially formed, rubber coated, metal gasket which is
not reusable. Do not install the gasket and torque cylinder screws until after final
installation of pitch stops. Whenever it is necessary to loosen cylinder attaching
screws, the gasket must be replaced.

(3) After applying sealant to both sides of gasket (9), immediately install gasket (9), cylinder (8),
balance ring (4), tubes (3), cylinder ring (2), and screws (2, 30 and 34).
(a) Torque all screws per Table 701 using alternating torquing sequence.
(b) Repeat torque sequence three to four times to ensure seating of gasket.

NOTE: Allow a minimum of 15 minutes between each torque cycle.

(c) Lockwire cylinder attaching screws (2) in groups of two or three.

NOTE: Screws (30 and 34) are patched and do not require safety wire.

10. Pitch Stop Adjustment

A. General
(1) The pitch stops can be changed without total disassembly of the propeller by addition of shim
segments or by removing the existing shims and substituting a thicker or thinner shim segment.
(2) Blade angles for high and low pitch positions, measured at reference stations, must be as listed
in the FAA Aircraft Type Certificate Data Sheet or applicable STC. Allowable limits for these
angles are:
(a) High +0.5 or -0.5 degrees
(b) Low +0.2 or -0.2 degrees

NOTE: Angles for blade sets must be within 0.2 degrees of each other. For example,
if the lowest pitch angle for one blade is 14.6 degrees, the other must not be
more then 14.8 degrees.
B. High Pitch Stop Adjustment
(1) Remove the cylinder (8).
(a) The high pitch stop (28) will be suspended on the piston rod (19).
(2) Protect the work area, and especially the inside of the hub, from chips or other debris from the
cutting operation.
(3) If the high pitch stop is too thick:
(a) Remove a 1.5 inch (39 mm) segment from the high pitch stop and slip it off the piston.
1 Smooth the cut ends of the high pitch stop.
(b) Insert a thinner high pitch stop of appropriate thickness to get the required pitch.

NOTE: A decrease in thickness of approximately 0.013 inch (0.33 mm) will increase the
high pitch angle 0.2 degrees.

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(4) If the high pitch stop is too thin:

(a) Determine the additional thickness required to get the proper high pitch.

NOTE: An increase in thickness of approximately 0.013 inch (0.33 mm) will decrease
the high pitch angle 0.2 degrees.

(b) If necessary, cut out a 1.5 inch (39 mm) segment from the shim that you will insert.
(c) Insert the shim between the existing high pitch stop (28) and the hub.
(5) If the low pitch stop requires adjustment, refer to Adjust Low Pitch Spacer
(6) If the low pitch stop does not require adjustment, install the cylinder. Refer to Assembly.
C. Adjust Low Pitch Spacer. (Refer to Figure 604)
(1) Remove the cylinder (8) if it has not been removed.
(2) Install an adjusting cylinder (part number C-4128) and adjusting cylinder spacer (part number
B-2362) onto the hub with four number 10-24 5/8 inch long screws.
(a) As the screws are tightened, the spring (21 or 23 and 24) will be compressed.
(b) Remove the retaining ring (11).
(c) If the spacer (12) is too thick, substitute a thinner spacer.
(d) If the spacer (12) is too thin, install a thicker spacer or insert a NAS1149F1216 (0.016 inch
thick) or NAS1149F1232 (0.032 inch thick) washer.

NOTE: A increase in thickness of approximately 0.007 inch (0.18 mm) will increase the
low pitch angle 0.2 degrees.

NOTE: If neither of these washers is of the correct thickness, another washer or spacer
with the appropriate inner diameter and thickness may be used.

11. Decal Installation

A. The part number decal consists of two parts, a decal which contains information and a clear lamination.
The clear laminate is located under the decal.
(1) The decal must have the correct dash number, part number, and blade angles preprinted or
added to a blank decal before the clear laminate is applied.
B. Install part number decal as follows:
(1) Clean cylinder (8) with solvent or thinner and dry thoroughly.
(2) Remove pressure sensitive decal (64) from top of clear laminate, position on cylinder (8)
centered in front of socket number one and roll down tight.
(3) Remove and discard backing from clear laminate, position so that laminate is centered over
decal and roll down tight.

NOTE: Installation of decal may be deferred until propeller assembly is completed.

NOTE: When part is received, clear laminate is located under decal. At time of installation,
clear laminate is to be placed on top of decal.

NOTE: Both the decal and clear laminate must be installed on the propeller cylinder.

NOTE: Decals for all C200 Series Propellers must be installed sideways, per Figure 706 and
Figure 707, Decal Installation.

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Low Pitch Spacer Change

Figure 705 (Sheet 1)

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Decal Installation
Figure 706 (Sheet 1)

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Decals
Figure 707 (Sheet 1)

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Decals
Figure 707 (Sheet 2)

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TESTING AND BALANCE

1. General
A. Refer to the Standard Practice Manual, Section 60-00-07, Blade Track and Blade to Blade Balance .

2. Leakage Check for Oil Fill Propellers

A. Perform a pressure leakage test per the Standard Practice Manual, Section 60-00-08, Pressure
Leakage Tests.

3. Static Balance
A. Perform static balance procedures per the Standard Practice Manual, Section 60-00-07, Blade Track
and Blade to Blade Balance.

4. Oil Filling
A. Following assembly, the propeller must be serviced with red-dyed oil (part number A-1637-11). Filling
is accomplished through the oil-filler plug in the side of hub. Following servicing, an A-4714 Plug must
be installed using Loctite Gasket Sealant #2 to prevent oil leakage. Torque plug per the Assembly
section, Table 702. Apply sentry seal to plug and hub.

Propeller Oil Quantity

C201, C203, C204, C205, C209, C227, C228, C230, 1.05 Quart (1000 ml)
C231, C232, C233, C234, C235, C236, C237, C238,
C239, C241,
C223 0.99 Quart (940 ml)

5. Placing Attaching Parts on Propeller

A. Place propeller assembly attaching parts and O-ring in a suitable small bag and attach to the propeller
after balancing and angle adjustments have been completed.

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ILLUSTRATED PARTS LIST

1. Illustrated Parts List

A. The propeller assemblies covered in this Service Manual are listed in the Illustrated Parts Lists by
the significant portion of the hub model designation, such as C209. These designations appear as
column headings. Listed down the page in the order of disassembly are the detail parts. Usage of
parts in specific propellers is shown by an "X" in the column for that propeller or by actual quantity
when quantities vary among propellers.
B. Through the years, parts have been obsoleted and replaced. Usage of the new parts may be
mandatory or optional. All part numbers which are acceptable for usage in a propeller assembly are
listed in the Master Parts List, Tables 1001 through 1005. The information contained in Repair and
Replacement, Table 603, Change Letter Stamping Requirements, specify the correct usage and
combination of parts.
C. An exploded view of a typical C200 Series non-oil filled and oil filled propeller is shown after the Master
Parts List (Refer to Figure 1001. The index numbers for the parts in the illustration are used to identity
detail part numbers, assemblies, or groups of similar part numbers in the Master Parts List.
D. Views of typical C200 Series spinner assemblies are shown after the Spinner Assembly Parts List
(Refer to Figure 1002). The index numbers for the parts in the illustration are used to identity detail
part numbers, assemblies, or groups of similar part numbers in the Spinner Assembly Parts List.

Table 1001. Master Parts List C201 through C209

INDEX PART
NO. NUMBER DESCRIPTION QTY. C201 C202 C203 C204 C205 C206 C207 C208 C209
1 A-1635-70 Screw, cylinder 14 X X X X X X X X X
attaching
2 B-6631 Ring, cylinder mounting 1 X X X X X X X X X
3 B-4354-1 Tube, cylinder mounting 14 X X X X X X X X X
4 C-5727 Balancing ring 1 X X X X
4 C-6560 Balancing ring 1 X X X X X
5 A-1635-36 Screw, balance weight AR X X X X X X X X X
5 A-1635-37 Screw, balance weight AR X X X X X X X X X
5 A-1635-40 Screw, balance weight AR X X X X X X X X X
5 A-1635-56 Screw, balance weight AR X X X X X X X X X
5 A-1635-57 Screw, balance weight AR X X X X X X X X X
5 A-1635-67 Screw, balance weight AR X X X X X X X X X
5 A-1635-68 Screw, balance weight AR X X X X X X X X X
6 A-1639-23 Nut, self-locking AR X X X X X X X X X
7 B-5525-1 Balance weight AR X X X X X X X X X
7 B-5525-2 Balance weight AR X X X X X X X X X
7 B-5525-3 Balance weight AR X X X X X X X X X
7 B-5525-4 Balance weight AR X X X X X X X X X
7 B-5525-5 Balance weight AR X X X X X X X X X
8 C-5263 Cylinder 1 X X X X
8 C-6549 Cylinder 1 X X X X X
9 B-4138 Gasket, cylinder 1 X X X X
9 B-6480 Gasket, cylinder 1 X X X X X

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Table 1001. Master Parts List C201 through C209 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C201 C202 C203 C204 C205 C206 C207 C208 C209
10 B-6911 Spacer support 1 X X X X X X X X X
11 A-1636-7 Retaining ring, external 1 X X X X X X X X X
12 A-2108-100 Spacer, low pitch stop AR X X X X X X X X X
(0.100 inch (2.54 mm)
thick
12 A-2108-200 Spacer, low pitch stop AR X X X X X X X X X
(0.200 inch (5.08 mm)
thick
12 A-2108-300 Spacer, low pitch stop AR X X X X X X X X X
(0.300 inch (7.62 mm)
thick
12 A-2108-400 Spacer, low pitch stop AR X X X X X X X X X
(0.400 inch (10.16 mm)
thick
12 A-1368-32 Shim, low pitch stop AR X X X X X X X X X
(0.004 inch (0.10 mm)
thick
12 A-1368-33 Shim, low pitch stop AR X X X X X X X X X
(0.008 inch (0.20 mm)
thick
12 A-1368-39 Shim, low pitch stop AR X X X X X X X X X
(0.016 inch (0.41 mm)
thick
12 A-1368-40 Shim, low pitch stop AR X X X X X X X X X
(0.032 inch (0.81 mm)
thick
12 A-1368-41 Shim, low pitch stop AR X X X X X X X X X
(0.064 inch (1.63 mm)
thick
13 A-1633-12 O-ring, piston to cylinder 1 X X X X X X X X X
14 C-3418 Piston, blade actuating 1 X X X X X X X X X
15 B-3414 Pin, piston rod 2 X X X X X X X X X
16 A-3150-5 Roll pin 2 X X X X X X X X X
17 A-3902 Link, blade actuating 2 X X X X X X X X X
18 A-1633-9 O-ring, tube to piston 1 X X X X X X X X X
19 B-2345 Tube, piston rod 1 X X X X X X X X X
20 A-3124 Guide, spring 2 X X X X X X X X X
21 A-3125 Spring, pitch return 1 X X X X X X X X X
26 A-1636-7 Retaining ring, external 1 X X X X X X X X X
27 A-2351 Washer, fiber 1 X X X X X X X X X
28 A-1937-X Spacer, high pitch stop 1 X X X X X X X X X
29 A-1633-9 O-ring, tube to hub 1 X X X X X X X X X
30 A-1635-86 Screw, slot block 2 X X X X X
31 A-1750-4 Stat-O-Seal 2 X X X X X

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Table 1001. Master Parts List C201 through C209 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C201 C202 C203 C204 C205 C206 C207 C208 C209
32 A-1633-58 O-ring, slot block 2 X X X X X
33 B-4746 Slot block 2 X X X X X
35 D-4149 Hub assembly (NP) 1 X
35 D-4326 Hub assembly 1 X X X
35 D-4801 Hub assembly 1 X
35 D-6608 Hub assembly 1 X
35 D-7292 Hub assembly 1 X X X
36 D-4054 ..Hub (NP) 1 X
36 D-4800 ..Hub (NP) 1 X
36 D-5044 ..Hub (NP) 1 X X X
36 D-6591 ..Hub (NP) 1 X
36 D-7291 ..Hub (NP) 1 X X X
37 B-3921 ..Stud, hub mounting 6 X X X X X
37 B-5077 ..Stud, hub mounting 6 X X X X
38 A-1638-10 ..Washer 6 X X X X
39 B-5478 ..Nut, hub mounting 6 X X X X
40 A-3150-1 ..Roll pin 6 X X X X
41 A-4001 ..Dowel, hub alignment 2 X X X X X
41 A-4001-30 ..Dowel, hub alignment AR X X X X X
(0.0015 inch oversize for
hub repair)
41 A-4001-45 ..Dowel, hub alignment AR X X X X X
(0.0030 inch oversize for
hub repair)
42 A-4714 ..Plug, pipe 1 X X X X X
42 A-4714-1 ..Plug, pipe (oversize) AR X X X X X
43 A-3150-4 ..Roll pin 2 X X
44 A-1633-109 O-ring, blade to hub 2 X X X X X
44 A-1633-96 O-ring, blade to hub 2 X X X X
45 C-3903 Retainer, split (matched 2 X X X X X X X X X
halves)
46 C-5270 Bearing, blade retention 2 X X X X X X X X X
(matched set)
46 C-7233 Bearing, blade retention AR X X X X X X X X X
(Oversize) (matched
set)
47 A-1634-9 Ball, bearing 64 X X X X X X X X X
48 B-5223 Separator, ball 64 X X X X X X X X X
49 B-4649 Shim carrier 2 X X X X X X X X X
50 B-4277-3 Split shim (anti-blade AR X X X X X X X X X
shake) (0.003-inch (0.08
mm) thick)

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Table 1001. Master Parts List C201 through C209 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C201 C202 C203 C204 C205 C206 C207 C208 C209
50 B-4277-4 Split shim (anti-blade AR X X X X X X X X X
shake) (0.004-inch (0.10
mm) thick)
50 B-4277-5 Split shim (anti-blade AR X X X X X X X X X
shake) (0.005-inch (0.13
mm) thick)
50 B-4277-6 Split shim (anti-blade AR X X X X X X X X X
shake) (0.006-inch (0.15
mm) thick)
50 B-4277-7 Split shim (anti-blade AR X X X X X X X X X
shake) (0.007-inch (0.18
mm) thick)
50 B-4277-8 Split shim (anti-blade AR X X X X X X X X X
shake) (0.008-inch (0.20
mm) thick)
50 B-4277-10 Split shim (anti-blade AR X X X X X X X X X
shake) (0.010-inch (0.25
mm) thick)
50 B-4277-12 Split shim (anti-blade AR X X X X X X X X X
shake) (0.012-inch (0.30
mm) thick)
50 B-4277-14 Split shim (anti-blade AR X X X X X X X X X
shake) (0.014-inch (0.36
mm) thick)
50 B-4277-15 Split shim (anti-blade AR X X X X X X X X X
shake) (0.015-inch (0.38
mm) thick)
50 B-4277-16 Split shim (anti-blade AR X X X X X X X X X
shake) (0.016-inch (0.41
mm) thick)
50 B-4277-18 Split shim (anti-blade AR X X X X X X X X X
shake) (0.018-inch (0.46
mm) thick)
50 B-4277-20 Split shim (anti-blade AR X X X X X X X X X
shake) (0.020-inch (0.51
mm) thick)
51 B-4407 Solid shim (0.032-inch AR X X X X X X X X X
(0.81 mm) thick)
51 B-4407-1 Solid shim (0.063-inch AR X X X X X X X X X
(1.60 mm) thick)
51 B-4407-2 Solid shim (0.050-inch AR X X X X X X X X X
(1.27 mm) thick)
51 B-4407-3 Solid shim (0.040-inch AR X X X X X X X X X
(1.02 mm) thick)
51 B-4407-4 Solid shim (0.071-inch AR X X X X X X X X X
(1.80 mm) thick)

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Table 1001. Master Parts List C201 through C209 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C201 C202 C203 C204 C205 C206 C207 C208 C209
51 B-4407-5 Solid shim (0.080-inch AR X X X X X X X X X
(2.03 mm) thick)
52 A-4427 Wire ring 2 X X X X X X X X X
53 B-4426 Retaining ring 2 X X X X X X X X X
54 B-6481 Plug, blade 2 X X X X X
55 A-1633-76 O-ring, plug to blade 2 X X X X X
56 A-1635-36 Screw 2 X X X X X
57 A-1638-18 Washer 2 X X X X X
59 A-1635-113 Screw, 12 point 4 X X X X X X X X X
60 B-3905 Actuating pin and base 2 X X X X X X X X X
assembly
61 78TA-X Blade 2 X
61 82PA-X Blade 2 X X
61 G-78CCA-X Blade 2 X
61 G-78TCA-X Blade 2 X
61 G-90DCA-X Blade 2 X
61 G-90DCB-X Blade 2 X
61 H-90DA-X Blade 2 X
61 H-90DHA-X Blade 2 X
62 A-6590 Patch 2 X X
63 B-6172 Decal, trademark 2 X X X X X X X X X
64 B-4862-X Decal, part number 1 X X X X X X X X X
65 A-2230 Decal, installation 1 X X X X
65 A-2230-9 Decal, installation 1 X X X X X
66 B-6494 Decal, warning 1 X
66 B-7367 Decal, notice 1 X X X X
67 A-1633-11 O-ring 1 X X X X
67 A-1633-3 O-ring 1 X X X X X
68 A-1639-2 Nut 6 X X X X X

Table 1002. Master Parts List C210 through C217

INDEX PART
NO. NUMBER DESCRIPTION QTY. C210 C211 C212 C213 C214 C215 C216 C217
1 A-1635-70 Screw, cylinder attaching 14 X X X X X X X X
2 B-6631 Ring, cylinder mounting 1 X X X X X X X X
3 B-4354-1 Tube, cylinder mounting 14 X X X X X X X X
(short)
4 C-5727 Balancing ring 1 X X X X X X X X
5 A-1635-36 Screw, balance weight AR X X X X X X X X

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Table 1002. Master Parts List C210 through C217 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C210 C211 C212 C213 C214 C215 C216 C217
5 A-1635-37 Screw, balance weight AR X X X X X X X X
5 A-1635-40 Screw, balance weight AR X X X X X X X X
5 A-1635-56 Screw, balance weight AR X X X X X X X X
5 A-1635-57 Screw, balance weight AR X X X X X X X X
5 A-1635-67 Screw, balance weight AR X X X X X X X X
5 A-1635-68 Screw, balance weight AR X X X X X X X X
6 A-1639-23 Nut, self-locking AR X X X X X X X X
7 B-5525-1 Balance weight AR X X X X X X X X
7 B-5525-2 Balance weight AR X X X X X X X X
7 B-5525-3 Balance weight AR X X X X X X X X
7 B-5525-4 Balance weight AR X X X X X X X X
7 B-5525-5 Balance weight AR X X X X X X X X
8 C-5263 Cylinder 1 X X X X X X X X
9 B-4138 Gasket, cylinder 1 X X X X X X X X
10 B-6911 Spacer support 1 X X X X X X X X
11 A-1636-7 Retaining ring, external 1 X X X X X X X X
12 A-2108-100 Spacer, low pitch stop (0.100 AR X X X X X X X X
inch (2.54 mm) thick
12 A-2108-200 Spacer, low pitch stop (0.200 AR X X X X X X X X
inch (5.08 mm) thick
12 A-2108-300 Spacer, low pitch stop (0.300 AR X X X X X X X X
inch (7.62 mm) thick
12 A-2108-400 Spacer, low pitch stop (0.400 AR X X X X X X X X
inch (10.16 mm) thick
12 A-1368-32 Shim, low pitch stop (0.004 AR X X X X X X X X
inch (0.10 mm) thick
12 A-1368-33 Shim, low pitch stop (0.008 AR X X X X X X X X
inch (0.20 mm) thick
12 A-1368-39 Shim, low pitch stop (0.016 AR X X X X X X X X
inch (0.41 mm) thick
12 A-1368-40 Shim, low pitch stop (0.032 AR X X X X X X X X
inch (0.81 mm) thick
12 A-1368-41 Shim, low pitch stop (0.064 AR X X X X X X X X
inch (1.63 mm) thick
13 A-1633-12 O-ring, piston to cylinder 1 X X X X X X X X
14 C-3418 Piston, blade actuating 1 X X X X X X X X
15 B-3414 Pin, piston rod 2 X X X X X X X X

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Table 1002. Master Parts List C210 through C217 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C210 C211 C212 C213 C214 C215 C216 C217
16 A-3150-5 Roll pin 2 X X X X X X X X
17 A-3902 Link, blade actuating 2 X X X X X X X X
18 A-1633-9 O-ring, tube to piston 1 X X X X X X X X
19 B-2345 Tube, piston rod 1 X X X X X X X X
20 A-3124 Guide, spring 2 X X X X X X X
21 A-3125 Spring, pitch return 1 X X X X X X X
22 A-4503 Guide, spring (front) 1 X
23 A-4501 Spring, inner 1 X
24 A-4502 Spring, outer 1 X
25 A-4989 Guide, spring (rear) 1 X
26 A-1636-7 Retaining ring, external 1 X X X X X X X X
27 A-2351 Washer, fiber 1 X X X X X X X
28 A-1937-X Spacer, high pitch stop 1 X X X X X X X X
29 A-1633-9 O-ring, tube to hub 1 X X X X X X X X
35 D-4531 Hub assembly 1 X X
35 D-5098 Hub assembly 1 X
35 D-4326 Hub assembly 1 X X X X X
36 D-5044 ..Hub (NP) 1 X X X X X
36 E-4530 ..Hub (NP) 1 X X
36 D-5079 ..Hub (NP) 1 X
37 B-3921 ..Stud, hub mounting 6 X X
37 B-5077 ..Stud, hub mounting 6 X X X X X X
38 A-1638-10 ..Washer 6 X X X X X X
39 B-5478 ..Nut, hub mounting 6 X X X X X X
40 A-3150-1 ..Roll pin 6 X X X X X X
41 A-4001 ..Dowel, hub alignment 2 X X
41 A-4001-30 ..Dowel, hub alignment AR X X
(0.0015 inch oversize for hub
repair)
41 A-4001-45 ..Dowel, hub alignment AR X X
(0.0030 inch oversize for hub
repair)
43 A-3150-4 ..Roll pin 2 X X X X X X X X
44 A-1633-96 O-ring, blade to hub 2 X X X X X X X X
45 C-3903 Retainer, split (matched 2 X X X X X X X X
halves)

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Table 1002. Master Parts List C210 through C217 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C210 C211 C212 C213 C214 C215 C216 C217
46 C-7233 Bearing, blade retention AR X X X X X X X X
(oversize) (matched set)
46 C-5270 Bearing, blade retention 2 X X X X X X X X
(matched set)
47 A-1634-9 Ball, bearing 64 X X X X X X X X
48 B-5223 Separator, ball 64 X X X X X X X X
49 B-4649 Shim carrier 2 X X X X X X X X
50 B-4277-3 Split shim (anti-blade shake) AR X X X X X X X X
(0.003-inch (0.08 mm) thick)
50 B-4277-4 Split shim (anti-blade shake) AR X X X X X X X X
(0.004-inch (0.10 mm) thick)
50 B-4277-5 Split shim (anti-blade shake) AR X X X X X X X X
(0.005-inch (0.13 mm) thick)
50 B-4277-6 Split shim (anti-blade shake) AR X X X X X X X X
(0.006-inch (0.15 mm) thick)
50 B-4277-7 Split shim (anti-blade shake) AR X X X X X X X X
(0.007-inch (0.18 mm) thick)
50 B-4277-8 Split shim (anti-blade shake) AR X X X X X X X X
(0.008-inch (0.20 mm) thick)
50 B-4277-10 Split shim (anti-blade shake) AR X X X X X X X X
(0.010-inch (0.25 mm) thick)
50 B-4277-12 Split shim (anti-blade shake) AR X X X X X X X X
(0.012-inch (0.30 mm) thick)
50 B-4277-14 Split shim (anti-blade shake) AR X X X X X X X X
(0.014-inch (0.36 mm) thick)
50 B-4277-15 Split shim (anti-blade shake) AR X X X X X X X X
(0.015-inch (0.38 mm) thick)
50 B-4277-16 Split shim (anti-blade shake) AR X X X X X X X X
(0.016-inch (0.41 mm) thick)
50 B-4277-18 Split shim (anti-blade shake) AR X X X X X X X X
(0.018-inch (0.46 mm) thick)
50 B-4277-20 Split shim (anti-blade shake) AR X X X X X X X X
(0.020-inch (0.51 mm) thick)
51 B-4407 Solid shim (0.032-inch (0.81 AR X X X X X X X X
mm) thick)
51 B-4407-1 Solid shim (0.063-inch (1.60 AR X X X X X X X X
mm) thick)
51 B-4407-2 Solid shim (0.050-inch (1.27 AR X X X X X X X X
mm) thick)
51 B-4407-3 Solid shim (0.040-inch (1.02 AR X X X X X X X X
mm) thick)

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Table 1002. Master Parts List C210 through C217 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C210 C211 C212 C213 C214 C215 C216 C217
51 B-4407-4 Solid shim (0.071-inch (1.80 AR X X X X X X X X
mm) thick)
51 B-4407-5 Solid shim (0.080-inch (2.03 AR X X X X X X X X
mm) thick)
52 A-4427 Wire ring 2 X X X X X X X X
53 B-4426 Retaining ring 2 X X X X X X X X
59 A-1635-113 Screw, 12 point 4 X X X X X X X X
60 B-3905 Actuating pin and base 2 X X X X X X X X
assembly
61 G-78CDA-X Blade 2 X
61 G-90DHB-X Blade 2 X X X
61 G-82PCA-X Blade 2 X
61 H-90DHA-X Blade 2 X
61 G-90DJA-X Blade 2 X
61 G-78CCA-X Blade 2 X
63 B-6172 Decal, trademark 2 X X X X X X X X
64 B-4862-X Decal, part number 1 X X X X X X X X
65 A-2230 Decal, installation 1 X X X X X X
65 A-2230-9 Decal, installation 1 X X
67 A-1633-3 O-ring 1 X X
67 A-1633-11 O-ring 1 X X X X X X
68 A-1639-2 Nut 6 X X

Table 1003. Master Parts List C218 through C221 and C223 through C225

INDEX PART
NO. NUMBER DESCRIPTION QTY. C218 C219 C220 C221 C223 C224 C225
1 A-1635-70 Screw, cylinder attaching 14 X X X X X X X
2 B-6631 Ring, cylinder mounting 1 X X X X X X X
3 B-4354-1 Tube, cylinder mounting 14 X X X X X X X
(short)
4 C-5727 Balancing ring 1 X X X X X X
4 C-6560 Balancing ring 1 X
5 A-1635-36 Screw, balance weight AR X X X X X X X
5 A-1635-37 Screw, balance weight AR X X X X X X X
5 A-1635-40 Screw, balance weight AR X X X X X X X
5 A-1635-56 Screw, balance weight AR X X X X X X X
5 A-1635-57 Screw, balance weight AR X X X X X X X
5 A-1635-67 Screw, balance weight AR X X X X X X X

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Table 1003. Master Parts List C218 through C221 and C223 through C225 (continued)
INDEX PART
NO. NUMBER DESCRIPTION QTY. C218 C219 C220 C221 C223 C224 C225
5 A-1635-68 Screw, balance weight AR X X X X X X X
6 A-1639-23 Nut, self-locking AR X X X X X X X
7 B-5525-1 Balance weight AR X X X X X X X
7 B-5525-2 Balance weight AR X X X X X X X
7 B-5525-3 Balance weight AR X X X X X X X
7 B-5525-4 Balance weight AR X X X X X X X
7 B-5525-5 Balance weight AR X X X X X X X
8 C-5263 Cylinder 1 X X X X X X
8 C-6549 Cylinder 1 X
9 B-4138 Gasket, cylinder 1 X X X X X X
9 B-6480 Gasket, cylinder 1 X
10 B-7093 Spacer support 1 X
10 B-6911 Spacer support 1 X X X X X X
11 A-1636-7 Retaining ring, external 1 X X X X X X X
12 A-2108-100 Spacer, low pitch stop (0.100 AR X X X X X X X
inch (2.54 mm) thick
12 A-2108-200 Spacer, low pitch stop (0.200 AR X X X X X X X
inch (5.08 mm) thick
12 A-2108-300 Spacer, low pitch stop (0.300 AR X X X X X X X
inch (7.62 mm) thick
12 A-2108-400 Spacer, low pitch stop (0.400 AR X X X X X X X
inch (10.16 mm) thick
12 A-1368-32 Shim, low pitch stop (0.004 AR X X X X X X X
inch (0.10 mm) thick
12 A-1368-33 Shim, low pitch stop (0.008 AR X X X X X X X
inch (0.20 mm) thick
12 A-1368-39 Shim, low pitch stop (0.016 AR X X X X X X X
inch (0.41 mm) thick
12 A-1368-40 Shim, low pitch stop (0.032 AR X X X X X X X
inch (0.81 mm) thick
12 A-1368-41 Shim, low pitch stop (0.064 AR X X X X X X X
inch (1.63 mm) thick
13 A-1633-12 O-ring, piston to cylinder 1 X X X X X X X
14 C-6096 Piston, blade actuating 1 X
14 C-3418 Piston, blade actuating 1 X X X X X X
15 B-3414 Pin, piston rod 2 X X X X X X X
16 A-3150-5 Roll pin 2 X X X X X X X
17 A-3902 Link, blade actuating 2 X X X X X X
17 B-6232 Link, blade actuating 2 X
18 A-1633-9 O-ring, tube to piston 1 X X X X X X X
19 B-7094 Tube, piston rod 1 X

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MODEL C200 SERIES
OVERHAUL MANUAL

Table 1003. Master Parts List C218 through C221 and C223 through C225 (continued)
INDEX PART
NO. NUMBER DESCRIPTION QTY. C218 C219 C220 C221 C223 C224 C225
19 B-2345 Tube, piston rod 1 X X X X X X
20 A-3124 Guide, spring 2 X X X X
21 A-3125 Spring, pitch return 1 X X X X
22 A-6233 Guide, spring (Front) 1 X
22 A-4503 Guide, spring (Front) 1 X X
23 A-4501 Spring, inner 1 X X X
24 A-4502 Spring, outer 1 X X X
25 A-4504 Guide, spring (Rear) 1 X X
25 A-4989 Guide, spring (Rear) 1 X
26 A-1636-7 Retaining ring, external 1 X X X X X X X
27 A-2351 Washer, fiber 1 X X X X
28 A-1937-X Spacer, high pitch stop 1 X X X X X X
29 A-1633-9 O-ring, tube to hub 1 X X X X X X X
30 A-1635-86 Screw, slot block 2 X
31 A-1750-4 Stat-O-Seal 2 X
32 A-1633-58 O-ring, slot block 2 X
33 B-4746 Slot block 2 X
35 D-4531 Hub assembly 1 X
35 D-5045 Hub assembly 1 X X X
35 D-5078 Hub assembly 1 X
35 D-6237 Hub assembly 1 X
35 D-7108 Hub assembly 1 X
36 E-4530 ..Hub (NP) 1 X
36 E-4955 ..Hub (NP) 1 X
36 D-5044 ..Hub (NP) 1 X X X
36 D-6236 ..Hub (NP) 1 X
36 D-7107 ..Hub (NP) 1 X
37 B-3921 ..Stud, hub mounting 6 X X
37 B-5077 ..Stud, hub mounting 6 X X X X
37 B-4071 ..Stud, hub mounting 6 X
38 A-1638-10 ..Washer 6 X
39 B-5478 ..Nut, hub mounting 6 X X X X
40 A-3150-1 ..Roll pin 6 X X X X
41 A-4001 ..Dowel, hub alignment 2 X X X
41 A-4001-30 ..Dowel, hub alignment AR X X X
(0.0015 inch oversize for hub
repair)
41 A-4001-45 ..Dowel, hub alignment AR X X X
(0.0030 inch oversize for hub
repair)

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1003. Master Parts List C218 through C221 and C223 through C225 (continued)
INDEX PART
NO. NUMBER DESCRIPTION QTY. C218 C219 C220 C221 C223 C224 C225
42 A-4714 ..Plug, pipe 1 X
42 A-4714-1 ..Plug, pipe (oversize) 1 X
43 A-3150-4 ..Roll pin 2 X X X X X
44 A-1633-109 O-ring, blade to hub 2 X
44 A-1633-96 O-ring, blade to hub 2 X X X X X X
45 C-3903 Retainer, split (matched 2 X X X X X X X
halves)
46 C-7233 Bearing, blade retention AR X X X X X X X
(oversize) (matched set)
46 C-5270 Bearing, blade retention 2 X X X X X X X
(matched set)
47 A-1634-9 Ball, bearing 64 X X X X X X X
48 B-5223 Separator, ball 64 X X X X X X X
49 B-4649 Shim carrier 2 X X X X X X X
50 B-4277-3 Split shim (anti-blade shake) AR X X X X X X X
(0.003-inch (0.08 mm) thick)
50 B-4277-4 Split shim (anti-blade shake) AR X X X X X X X
(0.004-inch (0.10 mm) thick)
50 B-4277-5 Split shim (anti-blade shake) AR X X X X X X X
(0.005-inch (0.13 mm) thick)
50 B-4277-6 Split shim (anti-blade shake) AR X X X X X X X
(0.006-inch (0.15 mm) thick)
50 B-4277-7 Split shim (anti-blade shake) AR X X X X X X X
(0.007-inch (0.18 mm) thick)
50 B-4277-8 Split shim (anti-blade shake) AR X X X X X X X
(0.008-inch (0.20 mm) thick)
50 B-4277-10 Split shim (anti-blade shake) AR X X X X X X X
(0.010-inch (0.25 mm) thick)
50 B-4277-12 Split shim (anti-blade shake) AR X X X X X X X
(0.012-inch (0.30 mm) thick)
50 B-4277-14 Split shim (anti-blade shake) AR X X X X X X X
(0.014-inch (0.36 mm) thick)
50 B-4277-15 Split shim (anti-blade shake) AR X X X X X X X
(0.015-inch (0.38 mm) thick)
50 B-4277-16 Split shim (anti-blade shake) AR X X X X X X X
(0.016-inch (0.41 mm) thick)
50 B-4277-18 Split shim (anti-blade shake) AR X X X X X X X
(0.018-inch (0.46 mm) thick)
50 B-4277-20 Split shim (anti-blade shake) AR X X X X X X X
(0.020-inch (0.51 mm) thick)
51 B-4407 Solid shim (0.032-inch (0.81 AR X X X X X X X
mm) thick)
51 B-4407-1 Solid shim (0.063-inch (1.60 AR X X X X X X X
mm) thick)

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1003. Master Parts List C218 through C221 and C223 through C225 (continued)
INDEX PART
NO. NUMBER DESCRIPTION QTY. C218 C219 C220 C221 C223 C224 C225
51 B-4407-2 Solid shim (0.050-inch (1.27 AR X X X X X X X
mm) thick)
51 B-4407-3 Solid shim (0.040-inch (1.02 AR X X X X X X X
mm) thick)
51 B-4407-4 Solid shim (0.071-inch (1.80 AR X X X X X X X
mm) thick)
51 B-4407-5 Solid shim (0.080-inch (2.03 AR X X X X X X X
mm) thick)
52 A-4427 Wire ring 2 X X X X X X X
53 B-4426 Retaining ring 2 X X X X X X X
54 B-7090 Plug, blade 2 X
55 A-1633-99 O-ring, plug to blade 2 X
56 A-1635-36 Screw 2 X
57 A-1638-7 Washer 2 X
59 A-1635-113 Screw, 12 point 4 X X X X X X 2
59 A-1635-171 Screw, 12 point 2 X
60 B-3905 Actuating pin and base 2 X X X X X
assembly
60 B-6235 Actuating pin and base 2 X
assembly
60 B-7092 Actuating pin and base 2 X
assembly
61 G-90DJA-X Blade 2 X
61 G-90DHC- Blade 2 X
XXEP
61 90RB-X Blade 2 X
61 G-90DHB-X Blade 2 X X
61 G-80VHA-X Blade 2 X
61 G-90RA-X Blade 2 X
62 A-6590 Patch 2 X
63 B-6172 Decal, trademark 2 X X X X X X X
64 B-4862-X Decal, part number 1 X X X X X X X
65 A-2230 Decal, installation 1 X X X X
65 A-2230-9 Decal, installation 1 X X X
66 B-6494 Decal, warning 1 X
67 A-1633-3 O-ring 1 X X X
67 A-1633-11 O-ring 1 X X X X
68 A-1639-2 Nut 6 X X X
69 C-5046 Plate, bulkhead attaching 2 X X X

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1004. Master Parts List C227 through C233

INDEX PART
NO. NUMBER DESCRIPTION QTY. C227 C228 C229 C230 C231 C233
1 A-1635-70 Screw, cylinder attaching 14 X X X X X X
2 B-6631 Ring, cylinder mounting 1 X X X
2 B-7407 Ring, cylinder mounting 1 X X X
3 B-4354-1 Tube, cylinder mounting 14 X X X X X X
(short)
4 C-5727 Balancing ring 1 X
4 C-6560 Balancing ring 1 X X
4 C-7383 Balancing ring 1 X X X
5 A-1635-36 Screw, balance weight AR X X X X X X
5 A-1635-37 Screw, balance weight AR X X X X X X
5 A-1635-40 Screw, balance weight AR X X X X X X
5 A-1635-56 Screw, balance weight AR X X X X X X
5 A-1635-57 Screw, balance weight AR X X X X X X
5 A-1635-67 Screw, balance weight AR X X X X X X
5 A-1635-68 Screw, balance weight AR X X X X X X
6 A-1639-23 Nut, self-locking AR X X X X X X
7 B-5525-1 Balance weight AR X X X X X X
7 B-5525-2 Balance weight AR X X X X X X
7 B-5525-3 Balance weight AR X X X X X X
7 B-5525-4 Balance weight AR X X X X X X
7 B-5525-5 Balance weight AR X X X X X X
8 C-5263 Cylinder 1 X
8 C-6549 Cylinder 1 X X
8 C-7382 Cylinder 1 X X X
9 B-6480 Gasket, cylinder 1 X X
9 C-7380 Gasket, cylinder 1 X X X
9 B-4138 Gasket, cylinder 1 X
10 B-6911 Spacer support 1 X X X X X X
11 A-1636-7 Retaining ring, external 1 X X X X X X
12 A-2108-100 Spacer, low pitch stop (0.100 AR X X X X X X
inch (2.54 mm) thick
12 A-2108-200 Spacer, low pitch stop (0.200 AR X X X X X X
inch (5.08 mm) thick
12 A-2108-300 Spacer, low pitch stop (0.300 AR X X X X X X
inch (7.62 mm) thick
12 A-2108-400 Spacer, low pitch stop (0.400 AR X X X X X X
inch (10.16 mm) thick
12 A-1368-32 Shim, low pitch stop (0.004 AR X X X X X X
inch (0.10 mm) thick

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1004. Master Parts List C227 through C233 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C227 C228 C229 C230 C231 C233
12 A-1368-33 Shim, low pitch stop (0.008 AR X X X X X X
inch (0.20 mm) thick
12 A-1368-39 Shim, low pitch stop (0.016 AR X X X X X X
inch (0.41 mm) thick
12 A-1368-40 Shim, low pitch stop (0.032 AR X X X X X X
inch (0.81 mm) thick
12 A-1368-41 Shim, low pitch stop (0.064 AR X X X X X X
inch (1.63 mm) thick
13 A-1633-12 O-ring, piston to cylinder 1 X X X X X X
14 C-3418 Piston, blade actuating 1 X X X X X X
15 B-3414 Pin, piston rod 2 X X X X X X
16 A-3150-5 Roll pin 2 X X X X X X
17 A-3902 Link, blade actuating 2 X X X X X X
18 A-1633-9 O-ring, tube to piston 1 X X X X X X
19 B-2345 Tube, piston rod 1 X X X X X X
20 A-3124 Guide, spring 2 X X X X X X
21 A-3125 Spring, pitch return 1 X X X X X X
26 A-1636-7 Retaining ring, external 1 X X X X X X
27 A-2351 Washer, fiber 1 X X X X X X
28 A-1937-X Spacer, high pitch stop 1 X X X X X X
29 A-1633-9 O-ring, tube to hub 1 X X X X X X
30 A-1635-86 Screw, slot block 2 X X
31 A-1750-4 Stat-O-Seal 2 X X
32 A-1633-58 O-ring, slot block 2 X X
33 B-4746 Slot block 2 X X
34 A-1635-207 Screw, cylinder attaching 4 X X X
35 D-5045 Hub assembly 1 X
35 D-6953 Hub assembly 1 X
35 D-6962 Hub assembly 1 X X
35 D-6740 Hub assembly 1 X
35 D-7292 Hub assembly 1 X
36 D-5044 ..Hub (NP) 1 X
36 D-6739 ..Hub (NP) 1 X
36 E-6952 ..Hub (NP) 1 X
36 D-6961 ..Hub (NP) 1 X X
36 E-7291 ..Hub (NP) 1 X
37 B-3921 ..Stud, hub mounting 6 X X
37 B-3921 ..Stud, hub mounting 4 X X
37 B-3939 ..Stud, hub mounting 2 X X
37 A-4957 ..Stud, hub mounting 6 X

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1004. Master Parts List C227 through C233 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C227 C228 C229 C230 C231 C233
37 B-5077 ..Stud, hub mounting 6 X
39 B-5478 ..Nut, hub mounting 6 X
40 A-3150-1 ..Roll pin 6 X
41 A-4001 ..Dowel, hub alignment 2 X X X X X
41 A-4001-30 ..Dowel, hub alignment AR X X X X X
(0.0015 inch oversize for hub
repair)
41 A-4001-45 ..Dowel, hub alignment AR X X X X X
(0.0030 inch oversize for hub
repair)
42 A-4714 ..Plug, pipe 1 X X X X X
42 A-4714-1 ..Plug, pipe (oversize) AR X X X X X
43 A-3150-4 ..Roll pin 2 X
44 A-1633-56 O-ring, blade to hub 2 X X X
44 A-1633-96 O-ring, blade to hub 2 X
44 A-1633-109 O-ring, blade to hub 2 X X
45 C-3903 Retainer, split (matched 2 X X X X X X
halves)
46 C-5270 Bearing, blade retention 2 X X X X X X
(matched set)
46 C-7233 Bearing, blade retention AR X X X X X X
(oversize) (matched set)
47 A-1634-9 Ball, bearing 64 X X X X X X
48 B-5223 Separator, ball 64 X X X X X X
49 B-4649 Shim carrier 2 X X X X X X
50 B-4277-3 Split shim (anti-blade shake) AR X X X X X X
(0.003-inch (0.08 mm) thick)
50 B-4277-4 Split shim (anti-blade shake) AR X X X X X X
(0.004-inch (0.10 mm) thick)
50 B-4277-5 Split shim (anti-blade shake) AR X X X X X X
(0.005-inch (0.13 mm) thick)
50 B-4277-6 Split shim (anti-blade shake) AR X X X X X X
(0.006-inch (0.15 mm) thick)
50 B-4277-7 Split shim (anti-blade shake) AR X X X X X X
(0.007-inch (0.18 mm) thick)
50 B-4277-8 Split shim (anti-blade shake) AR X X X X X X
(0.008-inch (0.20 mm) thick)
50 B-4277-10 Split shim (anti-blade shake) AR X X X X X X
(0.010-inch (0.25 mm) thick)
50 B-4277-12 Split shim (anti-blade shake) AR X X X X X X
(0.012-inch (0.30 mm) thick)
50 B-4277-14 Split shim (anti-blade shake) AR X X X X X X
(0.014-inch (0.36 mm) thick)

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1004. Master Parts List C227 through C233 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C227 C228 C229 C230 C231 C233
50 B-4277-15 Split shim (anti-blade shake) AR X X X X X X
(0.015-inch (0.38 mm) thick)
50 B-4277-16 Split shim (anti-blade shake) AR X X X X X X
(0.016-inch (0.41 mm) thick)
50 B-4277-18 Split shim (anti-blade shake) AR X X X X X X
(0.018-inch (0.46 mm) thick)
50 B-4277-20 Split shim (anti-blade shake) AR X X X X X X
(0.020-inch (0.51 mm) thick)
51 B-4407 Solid shim (0.032-inch (0.81 AR X X X X X X
mm) thick)
51 B-4407-1 Solid shim (0.063-inch (1.60 AR X X X X X X
mm) thick)
51 B-4407-2 Solid shim (0.050-inch (1.27 AR X X X X X X
mm) thick)
51 B-4407-3 Solid shim (0.040-inch (1.02 AR X X X X X X
mm) thick)
51 B-4407-4 Solid shim (0.071-inch (1.80 AR X X X X X X
mm) thick)
51 B-4407-5 Solid shim (0.080-inch (2.03 AR X X X X X X
mm) thick)
52 A-4427 Wire ring 2 X X X X X X
53 B-4426 Retaining ring 2 X X X X X X
54 B-6052 Plug, blade 2 X X X X
54 B-6481 Plug, blade 2 X
55 A-1633-76 O-ring, plug to blade 2 X
55 A-1633-99 O-ring, plug to blade 2 X X X X
56 A-1635-36 Screw 2 X
57 A-1638-18 Washer 2 X
58 A-1636-42 Retaining ring 2 X X X X
59 A-1635-113 Screw, 12 point 4 X X X X X X
60 B-3905 Actuating pin and base 2 X X X X X X
assembly
61 H-90RDA-X Blade 2 X
61 G-90RHC-X Blade 2 X
61 H-90REB-X Blade 2 X X
61 G-90DHB-X Blade 2 X
61 H-90REC-X Blade 2 X
63 B-6172 Decal, trademark 2 X X X X X X
64 B-4862-X Decal, part number 1 X X X X X X
65 A-2230 Decal, installation 1 X
65 A-2230-9 Decal, installation 1 X X X X X
66 B-6494 Decal, warning 1 X

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1004. Master Parts List C227 through C233 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C227 C228 C229 C230 C231 C233
66 B-7367 Decal, notice 1 X X X X
67 A-1633-3 O-ring 1 X X X X X
67 A-1633-11 O-ring 1 X
68 A-1639-2 Nut 6 X X X X X
69 C-5046 Plate, bulkhead attaching 2 X

Table 1005. Master Parts List C234 through C241

INDEX PART
NO. NUMBER DESCRIPTION QTY. C234 C235 C236 C238 C239 C240 C241
1 A-1635-70 Screw, cylinder attaching 14 X X X X X X X
2 B-6631 Ring, cylinder mounting 1 X
2 B-7407 Ring, cylinder mounting 1 X X X X X X
3 B-4354-1 Tube, cylinder mounting 14 X X X X X X X
(short)
4 C-5727 Balancing ring 1 X
4 C-7383 Balancing ring 1 X X X X X X
5 A-1635-36 Screw, balance weight AR X X X X X X X
5 A-1635-37 Screw, balance weight AR X X X X X X X
5 A-1635-40 Screw, balance weight AR X X X X X X X
5 A-1635-56 Screw, balance weight AR X X X X X X X
5 A-1635-57 Screw, balance weight AR X X X X X X X
5 A-1635-67 Screw, balance weight AR X X X X X X X
5 A-1635-68 Screw, balance weight AR X X X X X X X
6 A-1639-23 Nut, self-locking AR X X X X X X X
7 B-5525-1 Balance weight AR X X X X X X X
7 B-5525-2 Balance weight AR X X X X X X X
7 B-5525-3 Balance weight AR X X X X X X X
7 B-5525-4 Balance weight AR X X X X X X X
7 B-5525-5 Balance weight AR X X X X X X X
8 C-5263 Cylinder 1 X
8 C-7382 Cylinder 1 X X X X X X
9 B-4138 Gasket, cylinder 1 X
9 C-7380 Gasket, cylinder 1 X X X X X X
10 B-6911 Spacer support 1 X X X X X X X
11 A-1636-7 Retaining ring, external 1 X X X X X X X
12 A-2108-100 Spacer, low pitch stop (0.100 AR X X X X X X X
inch (2.54 mm) thick
12 A-2108-200 Spacer, low pitch stop (0.200 AR X X X X X X X
inch (5.08 mm) thick

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1005. Master Parts List C234 through C241 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C234 C235 C236 C238 C239 C240 C241
12 A-2108-300 Spacer, low pitch stop (0.300 AR X X X X X X X
inch (7.62 mm) thick
12 A-2108-400 Spacer, low pitch stop (0.400 AR X X X X X X X
inch (10.16 mm) thick
12 A-1368-32 Shim, low pitch stop (0.004 AR X X X X X X X
inch (0.10 mm) thick
12 A-1368-33 Shim, low pitch stop (0.008 AR X X X X X X X
inch (0.20 mm) thick
12 A-1368-39 Shim, low pitch stop (0.016 AR X X X X X X X
inch (0.41 mm) thick
12 A-1368-40 Shim, low pitch stop (0.032 AR X X X X X X X
inch (0.81 mm) thick
12 A-1368-41 Shim, low pitch stop (0.064 AR X X X X X X X
inch (1.63 mm) thick
13 A-1633-12 O-ring, piston to cylinder 1 X X X X X X X
14 C-3418 Piston, blade actuating 1 X X X X X X
14 C-6096 Piston, blade actuating 1 X
15 B-3414 Pin, piston rod 2 X X X X X X X
16 A-3150-5 Roll pin 2 X X X X X X X
17 A-3902 Link, blade actuating 2 X X X X X X
17 B-6232 Link, blade actuating 2 X
18 A-1633-9 O-ring, tube to piston 1 X X X X X X X
19 B-2345 Tube, piston rod 1 X X X X X X X
20 A-3124 Guide, spring 2 X X X X
21 A-3125 Spring, pitch return 1 X X X X
22 A-4503 Guide, spring (Front) 1 X X
22 B-6233 Guide, spring (Front) 1 X
23 A-4501 Spring, inner 1 X X X
24 A-4502 Spring, outer 1 X X X
25 A-4504 Guide, spring (Rear) 1 X
25 A-4989 Guide, spring (Rear) 1 X X
26 A-1636-7 Retaining ring, external 1 X X X X X X X
27 A-2351 Washer, fiber 1 X X X X
28 A-1937-X Spacer, high pitch stop 1 X X X X X X
29 A-1633-9 O-ring, tube to hub 1 X X X X X X X
34 A-1635-207 Screw, cylinder attaching 4 X X X X X X
35 D-4531 Hub assembly 1 X
35 D-6953 Hub assembly 1 X
35 D-7301 Hub assembly 1 X
35 D-7546 Hub assembly 1 X
35 D-7450 Hub assembly 1 X

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 McCAULEY PROPELLER SYSTEMS
MODEL C200 SERIES
OVERHAUL MANUAL

Table 1005. Master Parts List C234 through C241 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C234 C235 C236 C238 C239 C240 C241
35 D-7585 Hub assembly 1 X X
36 E-4530 ..Hub (NP) 1 X
36 E-6952 ..Hub (NP) 1 X
36 E-7300 ..Hub (NP) 1 X
36 E-7449 ..Hub (NP) 1 X
36 E-7545 ..Hub (NP) 1 X
36 E-7586 ..Hub (NP) 1 X X
37 B-3921 ..Stud, hub mounting 6 X X X X
37 A-4957 ..Stud, hub mounting 6 X
37 B-5077 ..Stud, hub mounting 6 X X
38 A-1638-10 ..Washer 6 X
39 B-5478 ..Nut 6 X X
40 A-3150-1 ..Roll pin 6 X X
41 A-4001 ..Dowel, hub alignment 2 X X X X X
41 A-4001-30 ..Dowel, hub alignment AR X X X X X
(0.0015 inch oversize for hub
repair)
41 A-4001-45 ..Dowel, hub alignment AR X X X X X
(0.0030 inch oversize for hub
repair)
42 A-4714 ..Plug, pipe 1 X X X X X X
42 A-4714-1 ..Plug, pipe (oversize) 1 X X X X X X
43 A-3150-4 ..Roll pin 2 X
44 A-1633-56 O-ring, blade to hub 2 X X X X X X
44 A-1633-96 O-ring, blade to hub 2 X
45 C-3903 Retainer, split (matched 2 X X X X X X X
halves)
46 C-5270 Bearing, blade retention 2 X X X X X X X
(matched set)
46 C-7233 Bearing, blade retention AR X X X X X X X
(oversize) (matched set)
47 A-1634-9 Ball, bearing 64 X X X X X X X
48 B-5223 Separator, ball 64 X X X X X X X
49 B-4649 Shim carrier 2 X X X X X X X
50 B-4277-3 Split shim (anti-blade shake) AR X X X X X X X
(0.003-inch (0.08 mm) thick)
50 B-4277-4 Split shim (anti-blade shake) AR X X X X X X X
(0.004-inch (0.10 mm) thick)
50 B-4277-5 Split shim (anti-blade shake) AR X X X X X X X
(0.005-inch (0.13 mm) thick)
50 B-4277-6 Split shim (anti-blade shake) AR X X X X X X X
(0.006-inch (0.15 mm) thick)

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Table 1005. Master Parts List C234 through C241 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C234 C235 C236 C238 C239 C240 C241
50 B-4277-7 Split shim (anti-blade shake) AR X X X X X X X
(0.007-inch (0.18 mm) thick)
50 B-4277-8 Split shim (anti-blade shake) AR X X X X X X X
(0.008-inch (0.20 mm) thick)
50 B-4277-10 Split shim (anti-blade shake) AR X X X X X X X
(0.010-inch (0.25 mm) thick)
50 B-4277-12 Split shim (anti-blade shake) AR X X X X X X X
(0.012-inch (0.30 mm) thick)
50 B-4277-14 Split shim (anti-blade shake) AR X X X X X X X
(0.014-inch (0.36 mm) thick)
50 B-4277-15 Split shim (anti-blade shake) AR X X X X X X X
(0.015-inch (0.38 mm) thick)
50 B-4277-16 Split shim (anti-blade shake) AR X X X X X X X
(0.016-inch (0.41 mm) thick)
50 B-4277-18 Split shim (anti-blade shake) AR X X X X X X X
(0.018-inch (0.46 mm) thick)
50 B-4277-20 Split shim (anti-blade shake) AR X X X X X X X
(0.020-inch (0.51 mm) thick)
51 B-4407 Solid shim (0.032-inch (0.81 AR X X X X X X X
mm) thick)
51 B-4407-1 Solid shim (0.063-inch (1.60 AR X X X X X X X
mm) thick)
51 B-4407-2 Solid shim (0.050-inch (1.27 AR X X X X X X X
mm) thick)
51 B-4407-3 Solid shim (0.040-inch (1.02 AR X X X X X X X
mm) thick)
51 B-4407-4 Solid shim (0.071-inch (1.80 AR X X X X X X X
mm) thick)
51 B-4407-5 Solid shim (0.080-inch (2.03 AR X X X X X X X
mm) thick)
52 A-4427 Wire ring 2 X X X X X X X
53 B-4426 Retaining ring 2 X X X X X X X
54 B-6052 Plug, blade 2 X X X X X X
55 A-1633-99 O-ring, plug to blade 2 X X X X X X
58 A-1636-42 Retaining ring 2 X X X X X X
59 A-1635-113 Screw, 12 point 4 X X X X X 2 X
59 A-1635-171 Screw, 12 point 2 X
60 B-3905 Actuating pin and base 2 X X X X X X
assembly
60 B-6235 Actuating pin and base 2 X
assembly
61 H-90REA-X Blade 2 X X
61 90DJA-X Blade 2 X
61 82PGC-X Blade 2 X

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Table 1005. Master Parts List C234 through C241 (continued)

INDEX PART
NO. NUMBER DESCRIPTION QTY. C234 C235 C236 C238 C239 C240 C241
61 H-90REC-X Blade 2 X
61 90DKB-X Blade 2 X
61 90DMC-X Blade 2 X
63 B-6172 Decal, trademark 2 X X X X X X X
64 B-4862-X Decal, part number 1 X X X X X X X
65 A-2230 Decal, installation 1 X X
65 A-2230-9 Decal, installation 1 X X X X X
66 B-7367 Decal, notice 1 X X X X X X
67 A-1633-11 O-ring 1 X X
67 A-1633-3 O-ring 1 X X X X X
68 A-1639-2 Nut 6 X X X X X
69 C-5046 Plate, bulkhead attaching 2 X

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C200 Model Propellers

Figure 1001 (Sheet 1)

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C200 Model Propellers

Figure 1001 (Sheet 2)

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C200 Model Propellers

Figure 1001 (Sheet 3)

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Table 1006. Spinner Assembly Parts List D-3290, D-3290-2, D-3396, D-3396-2, D-5255-1, D-5255-2

INDEX PART D-3290 D-3396 D-5255 D-5255

NO. NUMBER DESCRIPTION QTY. D-3290 -2 D-3396 -2 -1 -2
101 D-2820 Spinner shell, satin finish 1 X X
101 D-3395 Spinner shell satin finish 1 X X
101 D-5252 Spinner shell polished 1 X X
102 D-7713-1 Bulkhead and adapter 1 X
assembly
102 D-7713-4 Bulkhead and adapter 1 X X
assembly
102 D-7714-1 Bulkhead and slip ring 1 X
assembly
102 D-7714-4 Bulkhead and slip ring 1 X X
assembly
103 D-7655 ..Bulkhead assembly 1 X X
103 D-7681 ..Bulkhead assembly 1 X X X X
104 C-4044 ..Adapter plate 1 X X X
104A D-40720 ..Slip ring assembly 1 X X X
105 A-1635-36 ..Screw 12 X X X X X X
106 A-1638-20 ..Washer 12 X X X X X X
107 B-7712 ..Bulkhead assembly 1 X X X X X X
decal
108 B-3292 Fillet assembly 2 X X
108 B-3394 Fillet assembly 2 X X
108 B-5254 Fillet assembly 2 X X
109 B-2800 Spinner support 1 X X
109 B-3243 Spinner support 1 X X X X
110 B-3410-16 Support shim AR X X X X X X
110 B-3410-32 Support shim AR X X X X X X
111 A-1635-39 Screw 28 X X X X
111 A-1635-133 Screw 28 X X
112 A-1638-5 Washer 28 28 28 28 28 28
115 A-1639-4 Nut 12
116 B-6624 Decal - Installation 1 X X X X X X

Table 1007. Spinner Assembly Parts List D-5915, D-6195, D-7267-1, and D-7267-2

INDEX PART D-7267 D-7267

NO. NUMBER DESCRIPTION QTY. D-5915 D-6195 -1 -2
101 D-5914 Spinner shell polished 1 X
101 D-6203 Spinner shell polished 1 X
101 D-7265-1 Spinner shell polished 1 X
101 D-7265-2 Spinner shell satin finish 1 X

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Table 1007. Spinner Assembly Parts List D-5915, D-6195, D-7267-1, and D-7267-2 (continued)
INDEX PART D-7267 D-7267
NO. NUMBER DESCRIPTION QTY. D-5915 D-6195 -1 -2
102 D-5913 Bulkhead assembly 1 X
102 D-6210 Bulkhead assembly 1 X
102 D-7266 Bulkhead assembly 1 X X
108 B-5673-2 Fillet assembly 2 X
108 B-6193 Fillet assembly 2 X
109 B-3243 Spinner support 1 X
109 C-4383 Spinner support 1 X
109 C-6359 Spinner support 1 X X
110 B-3410-16 Support shim AR X X X X
110 B-3410-32 Support shim AR X X X X
111 A-1635-39 Screw 12 X
111 A-1635-133 Screw 28 X
111 A-1635-133 Screw 26 X
111 A-1635-133 Screw 12 X
112 A-1638-5 Washer 28 X
112 A-1638-5 Washer 26 X
112 A-1638-5 Washer 12 X X
113 A-2513-42 Bolt 12 X X
114 A-1638-26 Washer 24 X X
114 A-1638-25 Washer 24 X
115 A-1639-4 Nut 12 X X X
116 B-6624 Decal - Installation 1 X X X
118 A-2513-90 Bolt 12 X

Table 1008. Spinner Assembly Parts List D-7519-1, D-7519-2, D-7520, D-7569

INDEX PART D-7519 D-7519

NO. NUMBER DESCRIPTION QTY. -1 -2 D-7520 D-7569
101 D-7521 Spinner shell polished 1 X
101 D-7523-1 Spinner shell polished 1 X
101 D-7523-2 Spinner shell satin finish 1 X
101 D-7570 Spinner shell polished 1 X
102 D-7522 Bulkhead assembly 1 X
102 D-7524 Bulkhead assembly 1 X X
102 D-7572 Bulkhead assembly 1 X
108 C-7512-1 Fillet assembly 2 X
108 C-7512-2 Fillet assembly 2 X
108 C-7516 Fillet assembly 2 X
108 C-7573 Fillet assembly 2 X
109 C-4383-2 Spinner support 1 X X

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Table 1008. Spinner Assembly Parts List D-7519-1, D-7519-2, D-7520, D-7569 (continued)
INDEX PART D-7519 D-7519
NO. NUMBER DESCRIPTION QTY. -1 -2 D-7520 D-7569
109 C-6597 Spinner support 1 X
109 C-7568 Spinner support 1 X
110 B-3410-16 Support shim AR X X X X
110 B-3410-32 Support shim AR X X X X
111 A-1635-39 Screw 30 X
111 A-1635-133 Screw 30 X
111 A-1635-133 Screw 26 X
111 A-1635-133 Screw 18 X
112 A-1638-5 Washer 30 X X
112 A-1638-5 Washer 26 X
112 A-1638-5 Washer 18 X
116 B-6624 Decal - Installation 1 X X X

Table 1009. Spinner Assembly Parts List D-7519-1, D-7519-2, D-7587, D-7587-2

INDEX PART D-7579 D-7579 D-7587

NO. NUMBER DESCRIPTION QTY. -1 -2 D-7587 -2
101 D-7581-1 Spinner shell polished 1 X
101 D-7581-2 Spinner shell satin finish 1 X
101 D-7634 Spinner shell polished 1 X X
102 D-7582 Bulkhead assembly 1 X X
102 D-7713-5 Bulkhead and adapter 1 X
assembly
102 D-7714-5 Bulkhead and slip ring 1 X
assembly
104 C-4044 ..Adapter plate 1 X
104A D-40720 ..Slip ring assembly 1 X
105 A-1635-36 ..Screw 12 X X
106 A-1638-20 ..Washer 12 X X
107 B-7712 ..Bulkhead assembly 1 X X
decal
108 C-6202 Fillet assembly 2 X
108 C-6202-1 Fillet assembly 2 X
108 C-7065 Fillet assembly 2 X X
109 C-6359 Spinner support 1 X X
109 C-6619 Spinner support 1 X X
110 B-3410-16 Support shim AR X X X X
110 B-3410-32 Support shim AR X X X X
111 A-1635-39 Screw 26 X
111 A-1635-133 Screw 26 X
111 A-1635-133 Screw 22 X X

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Table 1009. Spinner Assembly Parts List D-7519-1, D-7519-2, D-7587, D-7587-2 (continued)
INDEX PART D-7579 D-7579 D-7587
NO. NUMBER DESCRIPTION QTY. -1 -2 D-7587 -2
112 A-1638-5 Washer 26 X X
112 A-1638-5 Washer 22 X X
113 A-2513-42 Bolt 12 X X
114 A-1638-26 Washer 12 X X

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Table 1009. Spinner Assembly Parts List D-7519-1, D-7519-2, D-7587, D-7587-2 (continued)
INDEX PART D-7579 D-7579 D-7587
NO. NUMBER DESCRIPTION QTY. -1 -2 D-7587 -2
115 A-1639-4 Nut 12 X X
116 B-6624 Decal - Installation 1 X X X X
117 B-7772 Bulkhead Gasket 2 X X

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Spinner Assembly
Figure 1002 (Sheet 1)

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