1963-1974 Cessna 172 Illustrated Parts Catalog

A Textron Company Illustrated Parts Catalog MODL 72 & MOE 12 REVISION 15 INCORPORATES TEMPORARY REVISION 172RPC14TR80-1 DATED 13 FEBRUARY 2007 Member of GAMA COPYRIGHT©1997 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 172 RPC 15 2 DECEMBER 1997 REVISION 15 1 JULY 2007

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG LIST OF EFFECTIVE PAGES CHAPTER-SECTION-SUBJECT Title Introduction-List of Effective Pages Record of Revisions List of Revisions Introduction Modification Kit List Supplier Address List Alphabetical Index Part Number Index © Cessna Aircraft Company PAGE DATE 1 Jul 1/2007 1 Jul 1/2007 1 thru 10 Jan 1/2007 1 thru 3 Jul 1/2007 1 thru 5 Jul 1/2007 1 thru 19 Jul 1/2007 1 thru 78 Jul 1/2007 INTRO - LIST OF EFFECTIVE PAGES Page 1 of 1 Jul 1/2007

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG LIST OF REVISIONS 1. Revision List A. This Illustrated Parts Catalog includes the original issue and the following listed revisions. To ensure that information in this manual is current, the revisions must be incorporated in the manual as they are issued. Original Issue - 3 February 1997 Revision Number Date Revision Number Date 1 16 May 1997 9 lS February 2002 2 6 April 1998 10 3 February 2003 3 6 January 1999 11 6 December 2004 4 16 July 1999 12 2 January 2006 5 l5 January 2000 1 3 3 July 2006 6 1 June 2000 14 1 January 2007 37 15 January 2001 1 5 1 July 2007 8 18 August 2001 Cessna Aircraft Company LIST OF REVISIONS Page 1 Jul 1/2007

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG DATE DATE INSERTED REMOVED PAGE NUMBER REVISION NUMBER RECORD OF REVISIONS DATE DATE PAGE INSERTED REMOVED NUMBER REVISION NUMBER

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG INTRODUCTION 1.General A. The purpose of this Illustrated Parts Catalog is to illustrate and identify replacement parts and assemblies necessary for the support of the model covered herein. The information in the catalog is based on data available at the time of publication. DO NOT USE this Illustrated Parts Catalog to determine removal and installation procedures, refer to the Maintenance Manual. The airplane operator, using applicable rules, is responsible for determining the status (or airworthiness) of the airplane. B. Chapter 11 contains procurable placards. Placards required by particular countries, determined by foreign certification authorities, are segregated into groups identified by International Civil Aviation Organization (ICAO) two-letter identifier located in the page footer. Cessna recommends all placards be present and readable on the airplane. C. Placards identified by the Code of Federal Regulations (CFRs) include: cockpit information including instrument markings and any related limitations, aircraft operating limitations, powerplant and auxiliary power unit instruments, flight control markings, fuel, oil, door and emergency exit information, limitations on storage compartments, loading, passenger cabin safety, and safety equipment operation. D. This Illustrated Parts Catalog is divided into chapters which correspond to equivalent chapters in the Maintenance Manual and is prepared in accordance with the Air Transport Association 2200 Specification format. E. The information in this publication is based on data available at the time of publication and is updated, supplemented, and automatically amended by Service Bulletins, Publication Revisions, Reissues, and Temporary Revisions which are issued through subscriptions service available from Cessna Propeller Aircraft Product Support. 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 Cessna Propeller Aircraft Product Support subscription services and/or Cessna Authorized Service Stations. Cessna Propeller Aircraft Product Support may be contacted by phone at (316)517-5800 or fax at (316)517-7271 or (316)942-9006, or in writing at 2121 S. Hoover Wichita, KS 67209. WARNING: ALL INSPECTION INTERVALS, REPLACEMENT TIME LIMITS, OVERHAUL TIME LIMITS, THE METHOD OF INSPECTION, LIFE LIMITS, CYCLE LIMITS, ETC., RECOMMENDED BY CESSNA ARE SOLELY BASED ON THE USE OF NEW, REMANUFACTURED, OR OVERHAULED CESSNA APPROVED PARTS. IF PARTS ARE DESIGNED, MANUFACTURED, REMANUFACTURED, OVERHAULED, ANID/OR APPROVED BY ENTITIES OTHER THAN CESSNA, THEN THE DATA IN CESSNA'S MAINTENANCE/ SERVICE MANUALS AND PARTS CATALOGS ARE NO LONGER APPLICABLE AND THE PURCHASER IS WARNED NOT TO RELY ON SUCH DATA FOR NON-CESSNA PARTS. ALL INSPECTION INTERVALS, REPLACEMENT TIME LIMITS, OVERHAUL TIME LIMITS, THE METHOD OF INSPECTION, LIFE LIMITS, CYCLE LIMITS, ETC., FOR SUCH NON-CESSNA PARTS MUST BE OBTAINED FROM THE MANUFACTURER AND/OR SELLER OF SUCH NON-CESSNA PARTS. F. Inspection, maintenance and parts requirements for Supplemental Type Certification (STC) installations are not included in this catalog. When an STC installation is incorporated on the airplane, those portions of the airplane affected by the installation must be inspected in accordance INTRODUCTION Page 1 © Cessna Aircraft Company Janl1/2007

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG with the inspection program published by the owner of the STC. Since STC installations may change systems interface, operating characteristics and component loads or stresses on adjacent structures, Cessna provided inspection criteria may not be valid for airplanes with STC installations. 2. Effectivity A. Numbers in the effectivity column indicate usage of the part is restricted. For example, the numbers 0001 in the Effect From column and 0023 in the Effect To column indicate that the part is used on airplanes 1 thru 23. If this column is blank opposite a first column listing of the figure, the usage is applicable to all models and serials covered by this catalog. If this column is blank opposite any indented listing, the usage is applicable to all models and serials covered by the next higher assembly or assemblies under which it appears. NOTE: Information in this Illustrated Parts Catalog is applicable to U.S. and Foreign Certified airplanes. Information unique to a particular country is identified in the chapter(s) affected. 3. Aerofiche A. The Illustrated Parts Catalog has been designed for Aerofiche presentation. Refer to the header of the applicable fiche for location of various indexing information. 4. Compact Disc (CD-ROM) A. Publications for this model are available in paper and as electronic media CD-ROM (Compact Disc - Read Only Memory). The paper publications are available as individual publications, such as Maintenance Manual, Illustrated Parts Catalog, etc., while the electronic service publications are grouped together on the CD. One CD includes all the service publications (Maintenance Manual, Illustrated Parts Catalog, Wiring Diagram Manual, Component Maintenance Manual, Nondestructive Testing Manual, Structural Repair Manual, and Illustrated Tools and Equipment List and all the Service Bulletins). These publications are kept up-to-date through routine revisions. 5. Part Number Index (Paper and Aerofiche) A. Part numbers in the Part Number Index are arranged in order according to the extreme left digit, then the next digit to the right, etc. The digits are used in the following sequence: space, symbols (such as #), decimal, slash (I), numbers in numerical order, then letters of the alphabet. B. The Part Number Index is a complete listing of all parts included in the Detailed Parts List. 6. Nomenclature Column A. The indention system used in the nomenclature column of this catalog shows the relationship of one part to another. For a given item, the indention code shows a system, installation, or general heading starting in the extreme left position continuing on down into succeeding columns until the end detail is reached (refer to Figure 1). B. The relationship of the items listed is shown by the degree of indention of each item. For example: The battery installation is listed in the first indenture of the nomenclature column. The Battery Assembly - Manifold is the next lower assembly and is therefore listed in the second indenture of nomenclature column. Refer to paragraph A. C. If two or more assemblies contain a majority of identical parts, or if the assemblies are left or right, the assemblies are listed together and the next lower assemblies or detail parts are listed as common for both assemblies with the differing parts coded for usage on the correct assembly. D. Attaching parts are listed immediately beneath the item to be attached and preceding any detail parts of the item. They are listed in the same indention as the item they attach and are preceded by the caption "Attaching Parts". The end of the attaching parts listing is followed by a separating symbol" -- -- Component parts which are not included in any assembly, but are used in conjunction with, or attach to certain assemblies, are listed either preceding the first detail or following the last detail of the assembly or installation and in the same indenture as the major assembly or installation. INTRODUCTION Page 2 © Cessna Aircraft Company Janl1/2007

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG B1515 1 2 3 4 5 6 7 Installation * Detailed Parts for Installation * Assembly * Attaching Parts for Assembly * ~~Detailed Parts for Assembly * . Sub-Assembly * . Attaching Parts for Sub-Assembly * ~~~Detailed Parts for Sub-Assembly * . ~Sub-Assembly * . . ~Attaching Parts for Sub-Assembly * . ~~~Detailed Parts for Sub-Sub-Assembly Order of Assembly Figure 1 7. List of Effective Pages (Paper and Aerofiche Versions) A. A List of Effective Pages is provided in the front of each chapter of the catalog. All pages in the catalog are listed in sequence on the List of Effective Pages with the most recent revision date for each page. A revised List of Effective Pages is provided for every Illustrated Parts Catalog revision. 8. Revision Filing Instructions (Paper Version) A. Regular Revision. (1) Refer to the List of Effective Pages of each chapter while inserting a revision. (2) Pages changed by the revision will be indicated by the revision date on the page and on the List of Effective Pages for that chapter. The revised page replaces the existing page in the catalog. (3) Existing pages no longer needed in the catalog are indicated by "Deleted" on the List of Effective Pages. These pages are to be removed and discarded. When a page has been deleted by a revision, the List of Effective Pages for subsequent revisions do not list the page. B. Temporary Revisions. (1) File Temporary Revisions in the applicable chapter in accordance with the filing instructions on the first page of the Temporary Revision. (2) Temporary Revisions should be removed from the catalog only when replaced by a revision to the catalog or by instructions noted on the superseding Temporary Revision. 9. Revision Indicators A. Additions or revisions to the parts list will be identified by the letter "R" in the right margin of the page adjacent to the change or addition. When technical changes cause unchanged text to appear on a different page, an "R" will be placed in the margin opposite of the affected items. 10. Cessna Part Numbering System A. The basic number identifies the Cessna drawing only. Each Installation, Assembly or Detailed Part is assigned a part number which consists of a seven digit drawing number and an appropriate dash number (refer to Figure 2) © Cessna Aircraft Company INTRODUCTION Page 3 Janl1/2007

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG B1518 Basic Number (Drawing Identification Only) Part Number 0553031 -1 Dash Number Part Number System Figure 2 11. Standard Parts A. Many parts having standard usage have been incorporated into the Cessna Standard System. Parts in this group are designated with the part number prefix "5", "CM", or "C". B. For standard hardware items such as screws, nuts, clamps, etc., AN, NAS, and MS standard numbers are listed. 12. Page Numbering System A. The Page Numbering System used in the Illustrated Parts Catalog consists of three-element numbers separated by a dash with the figure number, page number and date printed to the side (refer to Figure 3). Chapter/System (Flight Controls) Subject/Subsystem (Aileron System) Subject/Unit (Ailerons) Figure 01 - Figur 27-10-00 Page Numbering System Figure 3 13. Part Number Column A. This column contains the manufacturer's part number used to identify the item. 14. Units Per Assembly Column A. The quantity listed in the Units Per Assembly column is the quantity used per item. The quantity listed for attaching parts denotes the quantity necessary to attach only one item. The total quantity necessary to attach more than one item may be obtained by multiplying the quantity of attaching parts by the number of items to be attached. 15. Symbols and Part Number Terms A. When the term, "REFER TO", appears in the Nomenclature column and the Units Per Assembly column indicates "RF", the figure referred to will be the next highest assembly of the referred item. INTRODUCTION Page 4 © Cessna Aircraft Company Janl1/2007 B1518 'e Number 0nnn _-4 r-awoV - FI Q U VO0 VJI Dec 2/96 Aileron System I .. Date of Page Issue

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG B. When the term, "DELETED-NOT USED", appears in the Nomenclature column, it signifies that the index number was used but is no longer required. This procedure is used to eliminate re-indexing of all items following the deleted part. C. When the letters BKI (Bulk Item) appear in the Nomenclature column and the units per assembly column indicates "AR" (As Required). refer to Cessna Service Parts Center for prices and units of measure. 16. Abbreviations Commonly Used ALT alternate IPC illustrated parts catalog AR as required NP non-procurable ASSY assembly RE reference BKI bulk item SB service bulletin FSO for spares order TR temporary revision 17. Serial and Color A. When ordering upholstery material, carpet, or interior trim, include airplane model and serial number. Model and serial number are important to assure that the correct color combination is received. 18. Modification Kits A. A record of Modification Kits and Service Bulletins are provided in the Modification Kit List section. B. The Modification Kits List provides the kit number, title, date the kit was issued, Service Bulletin or applicable document number, and catalog incorporation date. 19. Definition of Text Page Information A. Refer to Figure 4. (1) The figure number refers to the corresponding illustration. (2) The number in the Figure and Item Number column corresponds to the item number of the part in the corresponding illustration. (3) Attaching parts are listed immediately following the part(s) attached. The symbol -- *- follows the last item of the attaching parts. (4) Parts with the item number preceded by a dash are not indexed on the illustration. (5) A Supplier's part number is identified in the Part Number column and the federally supplied vendor code follows the nomenclature in the Nomenclature column. (6) A number in the Units Per Assembly column indicates the quantity of the part used per next higher assembly or installation. (7) Numbers in the Effectivity column indicate usage of the part is restricted. For example, the numbers 0001 0023 indicate that the part is used on airplanes 1 thru 23. (8) This cross-reference indicates the figure in which the installation of assembly is broken down to its component parts. (9) Parts with the quantity "as required" are indicated by "AR" in the Units Per Assembly column. (1 0) Alternate part numbers are listed immediately following the part for which they may be substituted. The entry "ALT FOR" will be shown in the Nomenclature column. (11) "RF" indicates the installation or assembly is listed again in the figure cross-referenced in the Nomenclature column. The Units Per Assembly is given in the referenced figure. (12) Parts used only on a left or right installation or assembly are designated by "LH" or "RH" in the Nomenclature column. (13) A "USED ON" or "USED WITH" note in the Nomenclature column indicates the next proper higher assembly of a part when the part is not common to all of the next higher assemblies listed preceding the part. (14) The letter "R" in the right margin indicates text added or revised by the latest catalog revision. INTRODUCTION Page 5 © Cessna Aircraft Company Janl1/2007

CESSNA AIRCRAFT COMPANY MODEL 172 ILLUSTRATED PARTS CATALOG CESSNA AIRCRAFT COMPANY MODEL 172 0117 ILLUSTRATED PARTS CATALOG ~XNTS FIGURE PART NtJMIER NOMENCLATURE EFFECT PER ITEM 1 234 5 67 FROM TO ASSY -01 - ~~~~~NOSE GEAR INSTALLATION . ... RF 1 .SHOCK STRUT ASSY-NOSE GEARREFER TO032-20-01.. RF- FIGURE 0 1 ...................... ATTACHING PARTS 2 AN5-31A S OLT ......................... 0 1 3 MS21042L_5 .NUT. ........................ 03 4 0543018-I CAP. ........................ 01 5 AN5-10A BOLT. ........................ 02 6 NAS1149F0563P .WASHER .............. I III 02 7 0543042-1 .SHIM .032 THICK. .................. AR- a- 0543042-2 .SHIM .0 16 THICK .................... AR 9 .DAMPENER ASSY-SHIMMY REFER TO 32-20-02 ..... 01 FIGURE 0 1 ...................... 10 0543022-1 .TUBE ASSY-STEERING LH 01 11 0543022-2 TUBE ASSY-STEERING RH..0 ATTACHING PARTS 12 ANJ3-10A .BOLT .............. . ..... 1 13 MS21045L3 .NUT..01 14 S 1823-3 . BEARING-ROD END ............ .02 15 AN316-6R NUT .............. ..... 02 16 NAS397-16 CLAMP 02 17 WHEEL AgSS~-N6s GEARi REFER TO3 32-31i-00 01 FIGURE 01 ... ATTACHING PARTS 15 AN5-47 .BOLT ............... .......... 01 19 AN310-5 .NUT .... .01. . 20 MS24665-134 .COTTER PIN.:::::::::. ::::.. :01 21 0543001-0 .FERRULE-AXLE BOLT .......... .02.. .. 22 0543037-1 .SPACER-AXLE NOSE WHEEL ........ . .. 02 23 0543003-0 .TUBE-AXLE ............. ...... 01 24 0743627-5 .HUB CAP-NOSE GEAR VALVE STEM SIDE. .... 01 - 25 0743627-5 . ~HUB CAP-NOSE GEAR. ................ 01 ____ ___ ____ ___ ____ ___ ATTACHING PARTS - ----- 41 SCREW. ....................... 03 -27 AN936A5 WASHER. ...................... 03 - -- 213 6241M EXTENSION VALVE. .............. (V 17875) 01 - 29 3680C .EXTENSION VALVE ALT FOR 624 M ....... I(Vi 7875) 01 - ITEM NOT ILLUSTRATED Figure 0 1 32-20-00 Dec "2g19 6 Sample Page Figure 4 © Cessna Aircraft Company INTRODUCTION Page 6 Janl1/2007 B409 1 - 8- 2-- 4 - 7 _11 ___ 9 - 12 -- -6 -5

1963-1974 Cessna 172 Illustrated Parts Catalog

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