Cessna 441 Maintenance manual D2518-15-13 mm

REVISION MODEL 441 MAINTENANCE MANUAL REVISION 15 1 JULY 2002 D2518R1 5-13 Insert the following revised pages into the existing manual.

Cessna A Textron Company Maintenance Manual MODEL 441 CONQUEST/ CONQUEST II REVISION 15 TO THE BASIC MANUAL PROVIDES ADDITIONAL INFORMATION NECESSARY TO MAINTAIN THE AIRPLANE AND INCORPORATES TEMPORARY REVISION NUMBER 21-1 Dated 15 June 1999. 0 Member of GAMA FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN. COPYRIGHT © 1977 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 1 AUGUST 1977 REVISION 15 1 JULY 2002 D2518-15-13

Cessna A Textron Company TEMPORARY REVISION NUMBER 5-2 DATED 2 FEBRUARY 2004 MANUAL TITLE MANUAL NUMBER - PAPER COPY MANUAL NUMBER - AEROFICHE TEMPORARY REVISION NUMBER MANUAL DATE 1 August 1977 Model 441 Conquest /Conquest II Maintenance Manual D2518-15-13 D2518-15-13AF D2518-15TR5-2 REVISION NUMBER 15 DATE 1 July 2002 This Temporary Revision consists of the following pages, which affect and replace existing copy manual and supersede aerofiche information. AEROFICHE FICHE/FRAME 1/B11 1/B12 1/B14 1/B15 1/B16 1/B17 1/B18 1/B19 1/B20 1 /B21 1/B22 1/B23 1/B24 1/C01 1/C01 1/C02 1/C03 1/C04 CHAPTER/ SECTION/ SUBJECT 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-12-05 5-12-05 5-12-05 5-12-05 5-12-05 5-12-05 PAGE 17 18 19 20 21 22 23 24 25 26 27 1 2 3 4 5 6 pages in the paper AEROFICHE FICHE/FRAME 1/C06 1/C07 1/C08 1/C09 1/C10 1/C11 1/C12 1/C13 1/C14 1/C15 1/C16 1/E06 1/E07 1/E08 1/E09 1/E10 1/E11 © Cessna Aircraft Company CHAPTER/ SECTION/ SUBJECT 5-10-00 5-10-00 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 5-10-01 PAGE 1 2 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16

REASON FOR TEMPORARY REVISION 1. To revise Section 5-10-00, Inspections, paragraph 2. Interval and Phase Cross-Reference for Inspection Time Limits. The time interval for Interval Z and Phase 28 Inspection was changed to the current interval of a Phase 28 Inspection. 2. To add a requirement to perform a functional test of the oxygen system cabin Altitude Barometric Pressure Switch in Section 5-10-01, Inspection Time Limits. 3. To add a requirement to perform a functional test of the oxygen system cabin Altitude Barometric Pressure Switch in Section 5-12-05, Inspection Phase 5. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION 1. For Paper Publications, file this cover sheet behind the publication's title page to identify inclusion of the temporary revision in the manual. Insert the new pages in the publication at the appropriate locations and remove and discard the superseded pages. 2. For Aerofiche Publications, draw a line, with permanent red ink marker, through any aerofiche frame (page) affected by the temporary revision. This will be a visual identifier that the information on the frame (page) is no longer valid and the temporary revision should be referenced. For "added" pages in a temporary revision, draw a vertical line between the applicable frames. Line should be wide enough to show on the edges of the pages. Temporary revisions should be collected and maintained in a notebook or binder near the aerofiche library for quick reference. © Cessna Aircraft Company

Cessna A Textron Company TEMPORARY REVISION NUMBER 5-1 DATED 1 DECEMBER 2003 MANUAL TITLE Model 441 Conquest /Conquest II Maintenance Manual MANUAL NUMBER - PAPER COPY D2518-15-13 MANUAL NUMBER - AEROFICHE D2518-15-13AF TEMPORARY REVISION NUMBER D2518-15TR5-1 MANUAL DATE 1 August 1977 REVISION NUMBER 15 DATE 1 July 2002 This Temporary Revision consists of the following pages, which affect and replace existing pages in the paper copy manual and supersede aerofiche information. CHAPTER/ SECTION/ AEROFICHE SUBJECT PAGE FICHE/FRAME 5-11-00 1 1/C17 5-11-00 2 1/C18 REASON FOR TEMPORARY REVISION 1. To change the replacement schedule for the aileron hinge brackets. These changes add replacement requirements for the inboard aileron hinge brackets and additional airplane serial numbers for the outboard aileron hinge brackets. 2. To revise and update information as required to Section 5-11-00,.Component Time Limits. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION 1. For Paper Publications, file this cover sheet behind the publication's title page to identify inclusion of the temporary revision in the manual. Insert the new pages in the publication at the appropriate locations and remove and discard the superseded pages. 2. For Aerofiche Publications, draw a line, with permanent red ink marker, through any aerofiche frame (page) affected by the temporary revision. This will be a visual identifier that the information on the frame (page) is no longer valid and the temporary revision should be referenced. For "added" pages in a temporary revision, draw a vertical line between the applicable frames. Line should be wide enough to show on the edges of the pages. Temporary revisions should be collected and maintained in a notebook or binder near the aerofiche library for quick reference. © Cessna Aircraft Company

Cessna A Textron Company TEMPORARY REVISION NUMBER 35-1 DATED 1 DECEMBER 2003 MANUAL TITLE Model 441 Conquest /Conquest II Maintenance Manual MANUAL NUMBER - PAPER COPY D2518-15-13 MANUAL NUMBER - AEROFICHE D2518-15-13AF TEMPORARY REVISION NUMBER D2518-15TR35-1 MANUAL DATE 1 Auqust 1977 REVISION NUMBER 15 This Temporary Revision consists of the following pages, which affect and replace existing pages in the paper copy manual and supersede aerofiche information. PAGE 201 202 203 204 205 206 207 208 209 AEROFICHE FICHE/FRAME 11/H14 11/H15 11/H16 11/H17 11/H18 11/H19 Added Added Added REASON FOR TEMPORARY REVISION 1. To add an Altitude Barometric Pressure Switch Removal/Installation procedure. 2. To add a functional test procedure for the cabin Altitude Barometric Pressure Switch. 3. To revise and update information as required to Section 35-00-00, Oxygen System - Maintenance Practices. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION 1. For Paper Publications, file this cover sheet behind the publication's title page to identify inclusion of the temporary revision in the manual. Insert the new pages in the publication at the appropriate locations and remove and discard the superseded pages. 2. For Aerofiche Publications, draw a line, with permanent red ink marker, through any aerofiche frame (page) affected by the temporary revision. This will be a visual identifier that the information on the frame (page) is no longer valid and the temporary revision should be referenced. For "added" pages in a temporary revision, draw a vertical line between the applicable frames. Line should be wide enough to show on the edges of the pages. Temporary revisions should be collected and maintained in a notebook or binder near the aerofiche library for quick reference. © Cessna Aircraft Company DATE 1 July 2002 CHAPTER/ SECTION/ SUBJECT 35-00-00 35-00-00 35-00-00 35-00-00 35-00-00 35-00-00 35-00-00 35-00-00 35-00-00

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL RECORD OF REVISIONS REVISION DATE NUMBER INSERTED DATE PAGE REVISION DATE DATE PAGE REMOVED NUMBER NUMBER INSERTED REMOVED NUMBER

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL LIST OF EFFECTIVE PAGES CHAPTER-SECTION-SUBJECT Intro-Title Intro-List of Effective Pages Introduction Service Letter/Kit List List of Revisions Manufacturer's List List of Chapters Specifications PAGE DATE 1 Jul 1/2002 1 Jul 1/2002 2 Jul 1/2002 3 Jul 1/2002 4 Jul 1/2002 1 Sep3/1984 1 Jul 1/2002 1 Feb 2/1998 2 Feb 2/1998 3 Feb 2/1998 4 Feb 2/1998 1 Jul 1/2002 1 Sep3/1984 2 Apr 1/1985 INTRODUCTION - LIST OF EFFECTIVE PAGES Page 1 Jul 1/2002

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL INTRODUCTION 1. Coverage A. The Cessna Model 441 Maintenance Manual is prepared in accordance with Air Transport Association for Manufacturer's Technical Data, dated January 15, 1981. B. The maintenance manual provides sufficient information to enable a mechanic, who is unfamiliar with the Cessna Model 441 airplane, to service, troubleshoot, test, adjust and repair systems; and to remove and install any unit normally requiring such action on the line or in the maintenance hangar. If properly used, the maintenance manual will enable the mechanic to better maintain the Cessna Model 441. 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, AND/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. C. 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 Newsletters, Service Bulletins, Supplier Service Notices, Publication Changes, Revisions, Reissues and Temporary Revisions. 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 at Cessna Authorized Service Stations or through the Cessna Product Support subscription services. Cessna Service Stations have also been supplied with a group of supplier publications which provide disassembly, overhaul, and parts breakdowns for some of the various supplier equipment items. Suppliers publications are updated, supplemented, and specifically amended by supplier issued revisions and service information which may be reissued by Cessna, thereby automatically amending this publication and are communicated to the field through Cessna's Authorized Service Stations and/or through Cessna's subscription services. D. Inspection, maintenance and parts requirements for STC installations are not included in this manual. When an STC installation is incorporated on the airplane, those portions of the airplane affected by the installation must be inspected in accordance 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. E. Information beyond the scope of the maintenance manual may be found in the Wiring Diagram Manual and supplier publications that are available from Cessna Parts Distribution. The supplier manuals describe complete disassembly, overhaul and parts breakdown of some of the vendor equipment items. A listing of the available publications is issued periodically in Service News Letters. F. A Customer Care Supplies and Publications Catalog is available from your Cessna Service Station or directly from the Cessna Parts Distribution, Department 701, CPD2, Cessna Aircraft Company, 5800 East Pawnee Road, Wichita Kansas 67218-5590. This catalog lists all publications and Customer Care Supplies available from Cessna for prior year models, as well as new products. INTRODUCTION Page 1 Jul 1/2002

CESSNA AIRCRAFT COMPANY MODEL 441 MAINTENANCE MANUAL 2. Serialization A. The configuration of each Cessna Model 441 airplane is tailored to the request of the customer. The maintenance manual contains maintenance data for all Cessna Model 441 airplanes. The airplane serial number is listed on the identification plate. 3. Using The Maintenance Manual A. Division of Subject Matter (1) The Cessna Model 441 Maintenance Manual is divided into a chapters and section/arrangement. The chapters are separated into sections/subsystems. Each chapter has its own effectivity page and table of contents. A list of chapters is also provided at the front of the manual. B. Page Numbering System (1) The page numbering system used in the Cessna Model 441 Maintenance Manual consists of three-element numbers separated by dashes, under or beside which the page number and date are printed. A2005 Chapter/System 28-21-01 Subject/Unit (Fuel) (Fuel Boost Pump) Section/Subsystem (Distribution) (2) When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number (28-00-00), the information is applicable to the entire system. (3) When the section/subsystem element number is followed with zeros in the subject/unit element number (28-20-00), the information is applicable to subsystems within the system. (4) The subject/unit element number is used to identify information applicable to units within the subsystems. The subject/unit element number progresses sequentially from the number -01 in accordance with the number of subsystem units requiring maintenance information. (5) All system/subsystem/unit (chapter/section/subject) maintenance data is separated into specific types of information: description and operation, troubleshooting, maintenance practices. Blocks of sequential page numbers are used to identify the type of information: Pages 1 through 99 - Description and Operation Pages 101 through 199 - Troubleshooting Pages 201 through 299 - Maintenance Practices (6) Relatively simple units may not require description and operation, and/or troubleshooting information; in such cases, unused page-number blocks are omitted. In addition, for those items requiring many types of maintenance practices, page block 201 through 299 is omitted, and page numbering and maintenance practices are broken out as follows: Pages 301 through 399 - Servicing Pages 401 through 499 - Removal/Installation Pages 601 through 699 - Inspection/Check INTRODUCTION Page 2 Jul 1/2002

Cessna 441 Maintenance manual D2518-15-13 mm

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