Cessna Component Maintenance Manual Model 300 400

REVISION MODEL 300/400 SERIES COMPONENT MAINTENANCE MANUAL REVISION 2 1 JUNE 2005 D5266-2-13 The entire manual is provided with this revision. Please replace your current manual in its entirety.

Cessna A Textron Company Component Maintenance Manual MODEL 300/400 SERIES Member of GAMA COPYRIGHT © 1983 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 1 SEPTEMBER 1983 REVISION 2 1 JUNE 2005 D5266-2-13

CESSNA AIRCRAFT COMPANY MODEL 300 AND 400 SERIES COMPONENT MAINTENANCE MANUAL LIST OF EFFECTIVE PAGES CHAPTER-SECTION-SUBJECT 00-Title 00-List of Effective Pages 00-Record of Revisions 00-Record of Temporary Revisions 00-Table of Contents INTRODUCTION LIST OF REVISIONS LIST OF CHAPTERS © Cessna Aircraft Company 00 - LIST OF EFFECTIVE PAGES Page 1 of 1 Jun 1/2005 PAGE DATE Jun 1/2005 Jun 1/2005 Jun 1/2005 Pages 1-4 Page 1 Page 1

Revision Date Date Page Revision Date Date Page Number Inserted Removed Number Number Inserted Removed Number

Temporary Revision Number RECORD OF TEMPORARY REVISIONS Page Number Issue Date By Date Removed By

CESSNA AIRCRAFT COMPANY MODEL 300 AND 400 SERIES COMPONENT MAINTENANCE MANUAL CONTENTS INTRODUCTION ......... ........... ........... ................................. G eneral.................................................................... Coverage and Format ....................................................... Temporary Revisions ........................................................ Aerofiche (Microfiche) ....................................................... Using the Component Maintenance Manual or Aerofiche ....................... Effectivity Pages ............................................................ Revision Filing Instructions................................................... Identifying Revised Material.................................................. Warnings, Cautions and Notes ............................................... Cessna Propeller Aircraft Customer Care Supplies and Publications Catalog ..... Customer Comments on Manual ............................................. LIST OF REVISIONS............................................................. G en e ra l .................................................................... LIST OF CHAPTERS............................................................. INTRODUCTION Page 1 INTRODUCTION Page 1 INTRODUCTION Page 2 INTRODUCTION Page 2 INTRODUCTION Page 2 INTRODUCTION Page 2 INTRODUCTION Page 3 INTRODUCTION Page 3 INTRODUCTION Page 3 INTRODUCTION Page 3 INTRODUCTION Page 4 INTRODUCTION Page 4 LIST OF REVISIONS Page 1 LIST OF REVISIONS Page 1 LIST OF CHAPTERS Page 1 CONTENTS Page 1 of 1 Jun 1/2005 © Cessna Aircraft Company

CESSNA AIRCRAFT COMPANY MODEL 300 AND 400 SERIES COMPONENT MAINTENANCE MANUAL INTRODUCTION 1. General WARNING: All the inspection intervals, replacement time limits, overhaul time limits, inspection methods, life limits, cycle limits, etc., recommended by Cessna are based on the use of new, repaired, or overhauled Cessna approved parts. The data in Cessna's service/maintenance manuals and parts catalogs is not applicable if the parts are designed, built, repaired, overhauled, and/or approved by entities other than Cessna. The purchaser is warned not to rely on such data for non-Cessna parts. The purchaser must get from the manufacturer and/or seller of non-Cessna parts the inspection intervals, replacement time limits, overhaul time limits, inspection methods, life limits, cycle limits, etc., for all non-Cessna parts. A. The procedures in this manual are based on data that is available at the time of publication. This manual is updated, supplemented, and will automatically change by all data that is issued in the Service News Letters, Service Bulletins, Supplier Service Notices, Publication Changes, Revisions, Reissues and Temporary Revisions. The revisions become part of and are specifically incorporated in this publication. The user must know the latest changes to this publication through data available at the Cessna Authorized Service Stations or from the Cessna Propeller Aircraft Product Support subscription services. Cessna Service Stations are supplied with a group of supplier publications. The supplier publications will give disassembly, overhaul, and parts breakdown data for some of the different supplier items. Suppliers publications are updated, supplemented, and specifically changed by the supplier issued revisions and service data which may be issued by Cessna. This will automatically change this publication and is communicated to the field by the Cessna Authorized Service Stations and/or by Cessna's subscription services. B. The revisions, temporary revisions and reissues can be purchased from your Cessna Service Station or directly from Cessna Propeller Aircraft Product Support, Dept. 751, Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277-7706. Telephone 316-517-5800, Fax 316-942-9006. C. The data in this Component Maintenance Manual is applicable to the included components used on all U.S. and Foreign Certified airplanes listed: Landing Gear Components Flap Components 310 thru 310R 310 thru 310R 320 thru 320F T310P thru T31OR 335 320 thru 320F 340 thru 340A 335 401 thru 401B 340 thru 340A 402 thru 402B 401 thru 401B 411 402 thru 402C 414 411 421 thru 421B 414 thru 414A 421 thru 421C 425 D. The Cessna Service Stations are supplied with all the supplemental maintenance data for this manual. They have the latest authoritative recommendations for servicing Cessna airplanes. INTRODUCTION Page 1 © Cessna Aircraft Company Jun 1/2005

CESSNA AIRCRAFT COMPANY MODEL 300 AND 400 SERIES COMPONENT MAINTENANCE MANUAL 2. Coverage and Format A. The Cessna Models 300 and 400 Series Component Maintenance Manual, is prepared in accordance with the AirTransport Association (ATA) Specification Number 2200 for Manufacturer's Technical Data. 3. Temporary Revisions A. Information that is available may be supplied by a temporary revision. This service is used to supply, without delay, new data that will assist in maintaining safe flight/ground operations. The temporary revisions are numbered consecutively with the ATA chapter assignment. Page numbering uses the three-element number which matches the maintenance manual. The temporary revisions are normally included in the maintenance manual at the next scheduled revision. 4. Aerofiche (Microfiche) A. This component maintenance manual is prepared for aerofiche presentation. A List of Chapters, which identifies the initial fiche/frame of each chapter section, has been assembled and included in the introduction. The List of Chapters is used to assist in the use of the aerofiche index. The List of Chapters is shown in the upper left frame of each aerofiche card. 5. Using the Component Maintenance Manual or Aerofiche A. Division of Subject Matter. (1) Component maintenance information is divided into three chapters: Electrical, Flight Controls, and Landing Gear. Each chapter is subdivided according to repairable components. Each repairable component is an end item not dependent upon a system or airplane. B. List of Effective Pages. (1) A list of effective pages is provided with each chapter. All pages listed are active and shall appear in sequence as recorded in the List of Effective Pages. (2) The List of Effective Pages contains tabular listing of Air Transport Association number, page and date of each page in that chapter. A change in the chapter requires a revision to the chapter's List of Effective Pages. The date corresponds to the date that appears on the individual page which defines when that page was issued. C. Page Numbering System. (1) The page numbering system of the Component Maintenance Manual consists of the Air Transport Association Specification 100 three-element numbers separated by dashes, next to which the page number and date are printed. The three-element number is assigned to a component, with the first set of numbers corresponding to Air Transport Association Specification 2200 assigned chapter number. (2) The page number to the right of the three-element number complies with Air Transport Association Specification 2200 for subdividing a Component Maintenance Manual. Blocks of sequential page numbers are used to identify: Pages 1 through 99 - Description and Operation Pages 101 through 199 - Testing and Troubleshooting Pages 301 through 399 - Disassembly Pages 401 through 499 - Cleaning Pages 501 through 599 - Check Pages 601 through 699 - Repair Pages 701 through 799 - Assembly (Including Storage) INTRODUCTION Page 2 © Cessna Aircraft Company Jun 1/2005

CESSNA AIRCRAFT COMPANY MODEL 300 AND 400 SERIES COMPONENT MAINTENANCE MANUAL Pages 801 through 899 - Fits and Clearances Pages 901 through 999 - Special Tools, Fixtures and Equipment Pages 1001 through 1099 - Illustrated Parts List (3) The date which appears below the page number signifies when the page was issued. All pages were revised by Revision 2. (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. 6. Effectivity Pages A. A List of Effective Pages is supplied at the beginning of each maintenance manual chapter. All pages in the specific chapter are listed in numerical order on the effectivity page(s) with the date of issue for each page. 7. Revision Filing Instructions A. Regular Revision. (1) The pages that are removed or inserted in the maintenance manual are determined by the effectivity page. The pages are listed in sequence 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 must be put in the maintenance manual. The date column on the corresponding chapter effectivity page must verify the active page. B. Temporary Revision. (1) File the temporary revisions in the applicable chapter(s) in accordance with the filing instructions shown on the first page of the temporary revision. (2) The rescission of a temporary revision is completed by including it into the maintenance manual or by a superseding temporary revision. A Record of Temporary Revisions is supplied in the Temporary Revision List. The temporary revision list is located before the Introduction-List of Effective Pages. 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. 8. Identifying Revised Material A. Additions or revisions to the 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. The minimum revisable unit in the Maintenance Manual is a subject (refer to Page Numbering System for definition of subject). All the pages in a subject will have the same date regardless if the data in that page has changed or not. C. When large changes are made to the text in an existing section, revision bars will be shown for the full length of the text. D. Revisions to illustrations are shown by a revision bar along the entire vertical length of one side of illustration. No hand indicators are shown. 9. Warnings, Cautions and Notes A. Warnings, cautions and notes applicable to the instructions being completed are used. These adjuncts to the text are used to highlight or emphasize important data. (1) WARNING - This is applicable to the data that follows it. A warning puts attention to the use of the instructions, materials, methods, or limits that must be obeyed to prevent an injury or death. (2) CAUTION - This is applicable to the data that follows it. A caution puts attention to the use of the instructions, materials, methods, or limits which must be obeyed to prevent damage to the airplane or equipment. (3) NOTE - A NOTE follows the applicable instructions. It is for data only. INTRODUCTION Page 3 © Cessna Aircraft Company Jun 1/2005

CESSNA AIRCRAFT COMPANY MODEL 300 AND 400 SERIES COMPONENT MAINTENANCE MANUAL 10. Cessna Propeller Aircraft Customer Care Supplies and Publications Catalog A. A Cessna Propeller Aircraft Customer Care Supplies and Publications Catalog is available from a Cessna Service Station or directly from Cessna Propeller Aircraft Product Support Dept. 751 Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277-7706. Telephone 316-517-5800, Fax 316- 942-9006. The catalog lists all publications and Customer Care Supplies available from Cessna for prior year models as well as new products. To maintain this catalog in a current status, it is issued yearly in paper and aerofiche form. 11. Customer Comments on Manual A. Cessna Aircraft Company has worked to furnish you with an accurate, useful, up-to-date manual. This manual can be improved with your help. Please use the return card, supplied with your manual, to report any errors, discrepancies, and omissions in this manual as well as any general comments you want to make. INTRODUCTION Page 4 © Cessna Aircraft Company Jun 1/2005

Cessna Component Maintenance Manual Model 300 400

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