Cessna Aircraft Company Model 182/T182 Maintenance Manual

©D Cessna Aircraft Company SERVICE BULLETIN LIST Page 2 Jul 1/2007 Service Bulletin Number SB98-27-06 SB98-28-01 SB98-34-01 R1 SB98-71 -02 SB98-78-02 R1 SB98-37-01 R1 SB98-55-03 SB98-78-03 SB99-1 1-02 SB99-21 -01 SB99-24-01 SB99-24-02 SB99-25-01 R1 SB99-28-01 SB99-32-01 SB99-34-01 R1 SB99-37-01 SB99-53-01 SB99-53-02 SB99-71 -01 R2 SB99-71 -05 SBOO-22-01 SBOO-24-01 SBOO-24-02 SBOO-27-0 1 R1 SBOO-34-01 Dec 27/99 Mar 8/99 Apr 26/99 Jul 12/99 Oct 25/99 Feb 14/00 Mar 13/00 Jun 5/00 Aug 28/00 Apr 10/00 Nov 1/00 Dec 1/99 Dec 1/99 Dec 1/99 Jun 1/00 Nov 1/00 Nov 1/00 Nov 1/00 Nov 1/00 Nov 1/00 CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL Service Bulletin Date Title Manual Incorporation Vacuum System Air Filter Element Inspection/Replacement Center Cabin Rivet Inspection/Installation Engine Fuel Injection Lines and Support Clamps Inspection Engine Low Oil Pressure Switch Replacement Pilot's Operating Handbook and Pilot's Checklist Revision Aileron Control Cable Quadrant Inspection Inspection/Modification Engine Driven Fuel Pump Inspection Ignition Switch Center Ground Terminal Inspection Engine Turbocharger Mounting Bolt Replacement Glareshield Shroud Installation Fuel Quantity Level Sender/Transmitter Inspection Coin Antenna Replacement Pilot's Operating Handbook Revisions Pilot's Operating Handbook Revisions Honeywell Kap 140 Autopilot System Modification Pilot and Copilot Shoulder Harness Guide Removal Fuel Line Inspection Goodrich WX-500 Weather Mapping Sensor Modification Vacuum System Reducer Fitting Replacement Dry Vacuum Pump and Coupling Replacement Requirements Vacuum System Reducer Fitting Replacement Airborne Air and Fuel Products Check Valve Manifold Inspection Cabin Door Handle Replacement Fuselage Ballast Weight Installation ©Cessna Aircraft Company SERVICE BULLETIN LIST Page 3 Jul 1/2007 Service Bulletin Number SBOO-37-01 SBOO-53-01 R1 SBOO-73-01 R2 SBOO-79-01 R1 S BOO-i11-05 SBOO-27-02 R1 SBO1 -73-01 R2 SBO1 -74-01 SBO01 -71 -03 SBO1 -25-01 SBO1 -28-04 SBO1 -34-01 SB02-1 1-1 SB02-11-02 SB02-22-01 SB02-25-01 SB02-28-01 R1 SB02-34-01 SB02-37-01 SB02-37-02 SB02-37-03 SB02-37-04 SB02-52-01 SB02-53-01 Aug 14/00 Apr 10/00 Dec 24/01 Feb 21/00 Dec 26/00 Nov 6/00 Oct 10/05 Jun 25/01 Aug 20/01 Dec 24/01 Oct 1/01 Sep 3/01 Jan 21/02 Jan 21/02 Nov 25/02 Apr 29/02 Dec 16/02 Nov 25/02 Jan 21/02 Feb 18/02 Feb 18/02 Oct 28/02 Jan 21/02 Sep 9/02 Nov 1/00 Jun 18/01 Jan 2/06 Nov 1/00 Jun 18/01 Jun 18/01 No Effect Jun 18/01 No Eff ect No Eff ect No Eff ect No Eff ect No Effect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect CESSNA AIRCRAFT COMPANY MODEL 182/Ti182 MAINTENANCE MANUAL Title Elevator Rivet Installation Engine Crankshaft Gear Retaining Bolt Replacement Engine Induction System Fuel Overboard Drain Relocation Engine Oil Pump Plug Inspection Service Bulletin Date Oct 14/02 May 10/04 Nov 25/02 Feb 03/03 Manual Incorporation No Eff ect No Eff ect No Eff ect No Eff ect SB03-23-01 SB03-24-01 SB03-24-02 SB03-27-01 SB03-27-02 SB03-28-01 SB03-32-01 SB03-34-01 SB03-34-02 R1 SB03-37-01 SB03-53-01 SB03-53-03 R1 SB03-71 -02 SB03-73-01 SB04-11-03 SB04-22-01 SB04-23-01 SB04-24-0 1 SB04-25-01 R4 SB04-25-02 R1 SB04-25-04 SB04-27-01 R2 SB04-28-02 Honeywell KMA 26 Audio Panel Modification Alternator Replacement MC01 -3A Main Electrical Power Junction Box Modification Flap Actuator Motor Inspection Flap Control Bracket Attach Bolts Replacement Fuel Cap Lanyard Removal Nose Landing Gear Wheel Fairing Modification Honeywell KS 2700, KS 271 C and KS 272C Servo Friction Inspection Altimeter Inspection Vacuum Manifold Inspection/Replacement Aft Cabin Stringer Inspection Nose Landing Gear Fairing Attachment Inspection Fuel Injection Servo Inspection Throttle Arm Retention Inspection NAV III Pilot's Checklist Autopilot Circuit Breaker Extension Cap Installation Garmin GIA 63 Inspection/Modification Alternator Control Unit Inspection/Replacement Crew Seat Recline Modification Crew Seat Back Cylinder Lock Inspection and Crank Arm Modification Crew Seat Back Cylinder Lock Control Inspection/Adjustment Elevator Rivet Inspection Fuel Strainer Installation Inspection C Cessna Aircraft Company SERVICE BULLETIN LIST Page 4 Jul 1/2007 Service Bulletin Number SB02-55-01 SB02-71 -03 R2 SB02-7 1-04 SB02-71 -05 R1 Jul 28/03 Jul 28/03 Oct 13/03 Sep 29/03 Dec 22/03 Oct 27/03 Sep 29/03 Oct 27/03 Feb 16/04 Nov 10/03 May 26/03 Mar 15/04 May 26/03 Nov 4/03 Aug 30/04 Sep 13/04 Sep 13/04 Mar 1/04 Dec 26/06 Oct 17/05 Oct 11/04 Sep 13/04 May 10/04 No Eff ect No Effect No Effect No Eff ect No Eff ect Jan 2/06 No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL Title Marker Beacon Placard Installation Vertical Navigation Placard Installation Security Lock Installation Firewall Doubler Flange Modification and Shock Mount Inspection Forward Door Post Bulkhead Washer Inspection Engine Cowl Flap Rivet Inspection Engine Starter Inspection/Replacement Engine Fuel Injection Lines and Support Clamps Inspection Pilot's Operating Handbook Revisions Trim Servo Cable Chain Inspection Honeywell KAP-140 Autopilot Software Modification MC01 -3A Main Electrical Power Junction Box Circuit Breakers Inspection Inflatable Seat Belt Restraint Installation Inspection Inflatable Seat Restraints Installation Fuel Strainer Gasket Inspection High Intensity Discharge (HID) Landing and Taxi Light Installation Garmin G1000 System Software Upgrade Garmin GMA 1347 Audio Panel Modifications Garmin GMA 63 Integrated Avionics Unit Modification Garmin GMA 63 Integrated Avionics Unit Modification Garmin G1000 System Software Upgrade Garmin G1000 GDL-69A Weather and Digital Audio Entertainment Interface Installation Garmin G1lOQO Obstacle And Terrain Avoidance System Database Update Garmin G1000 System Software Upgrade Garmin G 1000 GDL-69A Weather And Digital Audio Entertainment Interface Installation Aft Avionics And Electrical Wire Bundle Inspection Service Bulletin Date Nov 22/04 Dec 27/04 Jun 28/04 Apr 11/05 Oct 11 /04 Apr 26/04 Nov 8/04 Aug 30/04 Mar 28/05 Dec 5/05 Dec 5/05 Jan 31/05 Mar 7/05 Apr 25/05 Jan 17/05 May 9/05 Jan 31/05 Feb 14/05 Feb 14/05 Apr 25/05 Jul 29/05 Jul 29/05 Sep 26/05 Sep 26/05 Sep 26/05 Nov 21/05 Manual Incorporation No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Effect No Eff ect Jan 2/06 No Eff ect No Effect No Effect No Effect No Eff ect No Eff ect No Eff ect Jan 2/06 No Eff ect No Eff ect No Eff ect No Eff ect No Effect No Effect No Effect No Eff ect No Eff ect No Eff ect ©Cessna Aircraft Company SERVICE BULLETIN LIST Page 5 Jul 1/2007 Service Bulletin Number SB04-34-01 SB04-34-02 SB04-52-01 SB04-53-02 R1 SB04-53-03 SB04-71 -01 SB04-71 -02 SB04-73-01 SB05-1 1-02 SB05-22-01 SB05-22-02 SB05-24-01 SB05-25-01 SB05-25-02 SB05-28-01 SB05-33-01 SB05-34-01 SB05-34-02 SB05-34-03 SB05-34-04 SB05-34-05 SB05-34-06 SB05-34-07 SB05-34-08 SB05-34-09 SB05-34-1 0 CESSNA AIRCRAFT COMPANY MODEL 182/7182 MAINTENANCE MANUAL Title Garmin GIA 63 Integrated Avionics Unit Outside Cover Replacement Garmin G1000 Display Unit (GDU) 1040 Cover Glass Delamination Vacuum Pump Inspection/Replacement Tunnel Bulkhead Rivet Inspection Wing Trailing Edge Rib Inspection Engine Crankshaft Replacement Engine Driven Fuel Pump Inspection Service Bulletin Date Nov 21/05 Dec 5/05 Nov 7/05 Sep 12/05 Oct 10/05 Jul 18/05 Mar 7/05 Manual Incorporation No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect Pilot's Operating Handbook Revisions Pilot's Checklist Revisions Honeywell KS270C Pitch Servo and KS271C Roll Servo Tach Generator Modification Electrical Ground Strap Inspection 60 Ampere Alternator Rotor Replacement 60 Ampere Alternator Brush Replacement Circuit Breaker Inspection Circuit Breaker Panel Assembly Inspection Flap Aft Roller Bearing Installation Modification Brake Master Cylinder Covers Inspection Honeywell KT 73 MODE S Transponder Installation Garmin G1000 System Software Upgrade Enablement of Garmin G1000 Terrain Awareness Warning System CLASS-B (TAWS-B) Automatic Direction Finder (ADF) and Distance Measuring Equipment (DMVE) Installation Cabin Door Modification Fuselage Stringer Rivet Inspection Engine Crankshaft Retirement Engine Compartment Fuel Hoses Security Inspection © Cessna Aircraft Company SERVICE BULLETIN LIST Page 6 Jul 1/2007 Service Bulletin Number SB05-34-1 1 SB05-34-1 2 SB05-37-01 SB05-53-02 SB05-57-01 SB05-71 -01 SB05-73-01 SB06-11 -01 SB06-1 1-02 SB06-22-01 SB06-24-01 SB06-24-02 R1 SB06-24-03 SB06-24-04 SB06-24-05 SB06-27-0 1 SB06-32-01 SB06-34-01 SB06-34-02 R1 SB06-34-03 SB06-34-04 SB06-52-01 SB06-53-01 SB06-71 -01 R1 SB06-71 -02 Mar 27/06 Nov 6/06 Apr 24/06 May 8/06 Dec 18/06 Dec 18/06 Dec 26/06 Dec 26/06 Apr 10/06 Sep 25/06 Feb 27/06 Mar 27/06 May 22/06 Oct 23/06 Mar 27/06 Oct 23/06 May 8/06 Jun 19/06 No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect No Eff ect CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL INTRODUCTION 1. General 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. A. 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 Propeller Aircraft 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. B. 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. C. REVISIONS, REISSUES and TEMPORARY REVISIONS can be purchased from your Cessna Service Station or directly from Cessna Propeller Aircraft Product Support, Department 751, Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277-7706. D. Information in this Maintenance Manual is applicable to all U.S. and Foreign Certified Model 182 airplanes beginning at serial 18280001 and T182 airplanes beginning at serial T18208001. Information unique to a particular country is identified in the chapter affected. E. All supplemental service information concerning this manual is supplied to all appropriate Cessna Service Stations so they have the latest authoritative recommendations for servicing these Cessna airplanes. It is recommended that Cessna owners utilize the knowledge and experience of the Cessna Service Station. 2. Cross Reference Listing of Popular Name Verses Model Numbers and Serials A. All airplanes regardless of the manufacturer, are certified under model number designations. Popular names are often used for marketing purposes. To provide a consistent method of referring to these airplanes, the model number will be used in this publication unless the popular name is necessary to differentiate between versions of the same basic model. The following table provides a listing of popular names, model numbers and serial numbers. INTRODUCTION Page 1 © Cessna Aircraft Company April 1/2002 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL NAME MODEL SERIALS SERIALS ENDING BEGINNING Skylane 182S 18280001 18280944 Skylane 182T 18280945 Skylane TC T182T T18208001 3. Coverage and Format A. The Cessna Model 182/T182 1996 And On Maintenance Manual has been prepared to help maintenance personnel in servicing and maintaining the Model 182/T182 airplanes (beginning at Serial 18280001 and T18208001). This manual provides the necessary information required to enable the mechanic to service, inspect, troubleshoot, remove and replace components or repair systems. NOTE: This manual is not intended to cover Model 182 airplanes produced prior to 1996. For manuals related to these airplanes, please refer to applicable listings in the Cessna Propeller Aircraft Customer Care Supplies & Publications Catalog. B. This manual has been prepared in accordance with the Air Transport Association (ATA) Specification Number 100 for Manufacturer's Technical Data. C. Information beyond the scope of this manual may be found in the applicable Model 182 Wiring Diagram Manual, Model 182 Illustrated Parts Catalog and the Single Engine Models 172, 182, T182, 206 and T206 1996 And On Structural Repair Manual. D. Technical Publications are also available for the various components and systems which are not covered in this manual. These manuals must be utilized as required for maintenance of those components and systems, and may be purchased from the manufacturer. 4. Temporary Revisions A. Additional information which becomes available may be provided by temporary revision. This service is used to provide, without delay, new information which will assist in maintaining safe flight/ground operations. Temporary revisions are numbered consecutively within the ATA chapter assignment. Page numbering utilizes the three-element number which matches the maintenance manual. Temporary revisions are normally incorporated into the maintenance manual at the next regularly scheduled revision. 5. Serialization A. All Model 182 airplanes are issued a serial number. This number is assigned as construction begins and remains with the airplane throughout its service life. This serial number appears on the airplane ID plate, located below the horizontal stabilizer, and on a trim plate located on the pilot side doorpost. This serial number is used to identify changes within the text or within an illustration. The absence of a serial number in text or illustration indicates the material is applicable to all airplanes. 6. Material Presentation A. This Maintenance Manual is available on paper, aerofiche or Compact Disc (CD/ROM). The CD/ROM contains the Maintenance Manual, Illustrated Parts Catalog Manual, Wiring Diagram Manual and Structural Repair Manual on a single disc. INTRODUCTION Page 2 © Cessna Aircraft Company April 1/2002 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL 7. Service Bulletins A. Service Bulletins may require special inspections and authorize modifications to the airplane and/or system. As service bulletins are issued, they will be incorporated in the next scheduled revision and noted in the Service Bulletin List, located previous to the Introduction. The list of service bulletins utilizes four columns to summarize information. (1) Service Bulletin Number - This Service Bulletin number column identifies the bulletin by number. Service Bulletins are numbered consecutively within ATA chapter assignment. (2) Service Bulletin Date - The service bulletin date column indicates the initial date the bulletin became active. (3) Title - The title column identifies the service bulletin by nomenclature. It is the same title displayed on page one of the service bulletin. (4) Manual Incorporation - The manual incorporation column indicates if the service bulletin has been incorporated in the maintenance manual by date, if the service bulletin had no effect on the maintenance manual (No Effect), or if the service bulletin has not been worked (dashed lines). 8. Using the Maintenance Manual A. Division of Subject Matter. (1) The Maintenance Manual is divided into four major sections. The major sections are in turn separated into chapters, with each chapter having its own effectivity page and table of contents. The manual divisions are as follows: (a) Major Section 1 - Airplane General Chapter Title 5 Time Limits/Maintenance Checks 6 Dimensions and Areas 7 Lifting and Shoring 8 Leveling and Weighing 9 Towing and Taxiing 10 Parking, Mooring, Storage and Return to Service 11 Placards and Markings 12 Servicing (b) Major Section 2 - Airframe Systems Chapter Title 20 Standard Practices - Airframe 21 Air Conditioning 22 Auto Flight 23 Communications 24 Electrical Power 25 Equipment/Furnishings 26 Fire Protection 27 Flight Controls 28 Fuel INTRODUCTION Page 3 © Cessna Aircraft Company April 1/2002 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL Chapter Title 30 Ice and Rain Protection 31 Indicating/Recording Systems 32 Landing Gear 33 Lights 34 Navigation 35 Oxygen 37 Vacuum (c) Major Section 3 - Structures Chapter Title 51 Standard Practices and Structures - General 52 Doors 55 Stabilizers 56 Windows 57 Wings (d) Major Section 4 - Power Plant Chapter Title 61 Propeller 71 Power Plant 73 Engine Fuel and Control 74 Ignition 76 Engine Controls 77 Engine Indicating 78 Exhaust 79 Oil 80 Starting 81 Turbines B. Page Numbering System. (1) The page numbering system used in the Maintenance Manual consists of three-element numbers separated by dashes. Refer to the example below for an illustration of typical numbering layout as used in the ATA format. INTRODUCTION Page 4 © Cessna Aircraft Company April 1/2002 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL Chapter/System 22-10-00 Subject/Unit (Auto Flight) (Auto Pilot) Section/Subsystem (Auto Pilot) (2) When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number (21-00-00), 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 (21-51-00), the information is applicable to the subsystem 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: Page 1 through 99 - Description and Operation Page 101 through 199 - Troubleshooting Page 201 through 299 - Maintenance Practices Page 301 through 399 - Servicing Page 401 through 499 - Removal/Installation Page 501 through 599 - Adjustment/Test Page 601 through 699 - Inspection/Check Page 701 through 799 - Cleaning/Painting Page 801 through 899 - Approved Repairs NOTE: In most cases, the individual topics have been combined into a 200-series document (Maintenance Practices). When specific topics require lengthy explanation, they will utilize the page blocks mentioned above. (6) A typical page number: 22-10-00 Page 202 Second Page of Nov 3/97 Auto Pilot Auto Flight Auto Pilot Date of Page Issue Auto Pilot (7) Illustrations are also tied into the page block numbering system. For example, all illustrations within a Maintenance Practices section will begin with the number 2 (i.e. Figure 201, Figure 202, etc.). Conversely, all illustrations within an Approved Repair section will begin with the number 8 (i.e. Figure 801, Figure 802, etc.). INTRODUCTION Page 5 © Cessna Aircraft Company April 1/2002 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL 9. Effectivity Pages A. A list of effectivity pages are provided at the beginning of each maintenance manual 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. 10. Revision Filing Instructions A. Regular Revision. (1) Pages to be removed or inserted in the maintenance manual are determined by the effectivity page. 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 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 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 maintenance 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. 11. 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. Chapter 5 may contain revision bars to indicate revised text. However, inspection items are noted as revised, added or deleted by the date of changed item code. Also, a revision date is indicated below the page number. D. 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. E. Revised and new illustrations will be indicated by either a revision bar along the side of the page or a hand indicator directing attention to the area. 12. Warnings, Cautions and Notes A. Throughout the text in this manual, warnings, cautions and notes pertaining to the procedures being accomplished are utilized. 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) WARNINGS - Calls attention to use of materials, processes, methods, procedures or limits which must be followed precisely to avoid injury or death to persons. (2) CAUTIONS - Calls attention to methods and procedures which must be followed to avoid damage to airplane and equipment. (3) NOTES - Contains information only. INTRODUCTION Page 6 0 Cessna Aircraft Company April 1/2002 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL 13. 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. 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 revised yearly and issued in paper and aerofiche form. 14. Customer Comments on Manual A. Cessna Aircraft Company has endeavored to furnish you with an accurate, useful, up-to-date manual. This manual can be improved with your help. Please use the return card, provided with your manual, to report any errors, discrepancies, and omissions in this manual as well as any general comments you wish to make. INTRODUCTION Page 7 © Cessna Aircraft Company April 1/2002 CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL LIST OF REVISIONS 1.Revisions A. This Maintenance Manual includes the original issue and the revisions listed in Table 1. Make sure that the information in this manual is current and that the latest maintenance and inspection procedures are available. The revisions must be incorporated in the manual as they are issued. Table 1. Basic Manual - Original Issue 3 February 1997 Date Writer 1 December 1998 3 1 June 2000 5 l8 June 2001 1 April 2002 1 March 2004 11 2 January 2006 1 13 1 January 2007 Revision Number 2 Date Writer 1 December 1999 4 1 November 2000 6 15 December 2001 8 4 August 2003 10 1 March 2005 12 3 July 2006 jgb rdg bjo jcn 14 1 July 2007 ©D Cessna Aircraft Company jgb jgb tks bjo jcn LIST OF REVISIONS Page 1 Jul 1/2007 Revision Number 7 9 CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL LIST OF MANUFACTURERS TECHNICAL PUBLICATIONS 1. List of Manufacturers Technical Publications A. Outlined below is a list of manufacturers publications. Table 1. CHAPTER 22 - AUTOFLIGHT Publica- tion Part Number Publication Title 190- G1000 Line 00352-00 Maintenance Manual GSA 190- 8X/GSM 85 00303-72 Installation Manual KAP 140 006- 00991- 0002 Manufacturer Garmin USA 1200 East 151 st Street Olathe, KS 66062 Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Table 2. CHAPTER 23 - COMMUNICATIONS Publication Title Manufacturer KX-155A 006- 10542- 0000 KMA 26 006- 10544- 0000 Installation Manual Installation Manual Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 LIST OF MANUFACTURERS TECHNICAL PUBLICATIONS Page 1 ©Cessna Aircraft Company Janl1/2007 Item Cessna Part Number Manufact- urer's Part Number GFC -700 Autopilot Autopilot Servo Autopilot Item Cessna Part Number Manufact- urer's Part Number NAV/ Comm Publica- tion Part Number Audio Amplifier/ Intercom/ Marker Beacon Receiver Item CESSNA AIRCRAFT COMPANY MODEL 182/Ti182 MAINTENANCE MANUAL Table 3. CHAPTER 24 - ELECTRICAL POWER Publication Title Cyclon Selection Guide (Third Edition) (NOTE 1) Manufacturer AVT Inc. DBA Electritek - AVT 400 East Mineral Avenue Littleton, CO 80122-2604 Hawker 617 North Ridgeview Drive Warrensburg, MO 64093-9301 NOTE 1: The power cells inside the Standby Battery are manufactured by Hawker and the manufacturer publication that is shown above is from Hawker. AVT is the supplier of the Standby Battery pack as installed in the airplane. The data shown in the Hawker manual is informational only. Maintenance procedures for the Standby Battery given in Chapter 24, Standby Battery - Maintenance Practices must be followed. CHAPTER 25 - EQUIPMENT FURNISHING Publica- tion Part Number Publication Title E508804 Supplemental Maintenance Manual E508804 Supplemental Maintenance Manual E508804 Supplemental Maintenance Manual Manufacturer AmSafe Aviation 5456 E. McDowell Rd. Mesa, AZ 85215 www.amsafe.com AmSafe Aviation 5456 E. McDowell Rd. Mesa, AZ 85215 www.amsafe.com AmSafe Aviation 5456 E.McDowell Rd. Mesa, AZ 85215 www.amsafe.com LIST OF MANUFACTURERS TECHNICAL PUBLICATIONS ©Cessna Aircraft Company Item Cessna Part Number Standby Battery Manufact- urer's Part Number AVT- 200413 Publica- tion Part Number Item Cessna Part Number Manufac- turer's Part Num- ber 7035-1 - 011- 8105 (GO-Pilot Seat) 7035-1 - 021- 8105 (Pilot Seat) 7035-2- 011- 8105 (LH Rear Seat) 7035-2- 021- 8105 (RH Rear Seat) 508792- 401 (Co- Pilot Seat) 508794- 401 (Pilot Seat) 508358- 409 Seat Belt Airbag Assembly Inflation Assembly Electronics Module Assembly Page 2 an 1/2007 J CESSNA AIRCRAFT COMPANY MODEL 182/Ti182 MAINTENANCE MANUAL CHAPTER 25 - EQUIPMENT FURNISHING Publication Title Manufacturer 7035- 20301181 05 (Co-Pilot Seat) 7035- 2040218105 (Pilot Seat) 7035- 205021 8105 (LH Rear Seat) 7035- 206021 81 05 (RH Rear Seat) 508668- 201 E508804 Supplemental Maintenance Manual E508804 Supplemental Maintenance Manual AmSafe Aviation 5456 E. McDowell Rd. Mesa, AZ 85215 www.amsafe.com AmSafe Aviation 5456 E. McDowell Rd. Mesa, AZ 85215 www.amsafe.com Table 4. CHAPTER 26 - FIRE PROTECTION Publication Title Manufacturer Fire Extin- C421001- A352 GS guisher 0201 Hand Portable Halon 1211 Fire Extinguisher Maintenance Manual Amerex Corp. P.O. Box 81 Trussville, AL 351 73-0081 Table 5. CHAPTER 32 - LANDING GEAR Cessna Part Number Manufact- urer's Part Number Publica- tion Part Number C163006- 40-75B 0301 30- 0521 9-1 30-52U Publication Title Cleveland Wheels & Brakes Component Maintenance Manual Cleveland Wheels & Brakes Component Maintenance Manual Manufacturer Parker Hannifin Corporation Aircraft Wheel & Brake 1160 Center Road P.O. Box 158 Avon, OH 44011 Parker Hannifin Corporation Aircraft Wheel & Brake 1160 Center Road P.O. Box 158 Avon, OH 44011 LIST OF MANUFACTURERS TECHNICAL ©Cessna Aircraft Company PUBLICATIONS Page 3 Janl1/2007 Part Number Man ufac- turer's Part Num- ber Publica- tion Part Number Three- Point Air Bag Belt V23 System Diagnostic Tool Item Cessna Part Number Manufact- urer's Part Number Publica- tion Part Number Item Wheel Brakes Item Item CESSNA AIRCRAFT COMPANY MODEL 182/T 182 MAINTENANCE MANUAL Table 6. CHAPTER 34 - NAVIGATION Item Blind Encoder Cessna Part Number Manufact- urer's Part Number 3940408-1 SSD1 20-20 Navigation 066- Indicator 03056- 0011 Automatic Direction Finder Mode C Transpon- der 066- 01 072- 0014 066- 01156- 0101 NAV 066- Indicators 03056- 0002 GPS 066- 01148- 1111 Publica- tion Part Number Publication Title M881000D Altitude Encoder/ Digitizer Owner/ Installation Manual KI 209A 006- 10543- 0000 KR 87 006- 001 84- 0005 KT 76C 006- 10545- 0000 KI 208/209 006- 00140- 0003 KLN 89/89B Autopilot 3900008-1 KAP140 2-axis 006- 10522- 0001 Installation Manual Installation Manual Installation Manual Installation Manual Installation Manual Installation Manual Manufacturer Trans-Cal Industries, Inc. 16141 Cohasset St. Van Nuys, CA 91406 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Allied Signal 101 N. Industrial Parkway New Century, KS 66031 Table 7. CHAPTER 71 - POWER PLANT Publica- Publication Title tion Part Number 60294-7 Direct Drive Engine Overhaul Manual Manufacturer Textron Lycoming LIST OF MANUFACTURERS TECHNICAL PUBLICATIONS Item Cessna Part Number Engine Manufact- urer's Part Number 10540- AB1A5 Page 4 an 1/2007 i Q Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 182/Ti182 MAINTENANCE MANUAL Table 8. CHAPTER 73 - ENGINE FUEL AND CONTROL Publica- tion Part Number Publication Title 15-338D RSA-5 & RSA- 10 Fuel Injection Systems Operation & Service Manual 15-81 OB Troubleshooting Techniques for the Precision Airmotive RSA Fuel Metering System 15-895G Index of Manuals, Bulletins, and Service Information Letters for Precision Airmotive Fuel Controls Manufacturer Precision Airmotive 14800 40th Ave. NE Marysville, WA 98271 Precision Airmotive 14800 40th Ave. NE Marysville, WA 98271 Precision Airmotive 14800 40th Ave. NE Marysville, WA 98271 Table 9. CHAPTER 74 - IGNITION Publica- tion Part Number Publication Title L-1363C 4300/6300 Series Magneto Maintenance and Overhaul Manual Manufacturer Slick Aircraft Products 530 Blackhawk Park Ave. Rockford, IL 61104 LIST OF MANUFACTURERS TECHNICAL PUBLICATIONS Page5 ©Cessna Aircraft Company Janl1/2007 Item Cessna Part Number Fuel Injection System Fuel Injection System Fuel Injection System Manufact- urer's Part Number RSA-5 RSA-5 RSA-5 Item Cessna Part Number Magneto Manufact- urer's Part Number 6351 CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL LIST OF CHAPTERS CHAPTER Time Limits/Maintenance Checks Dimensions and Areas Lifting and Shoring Leveling and Weighing Towing and Taxiing Parking and Mooring Placards and Markings Servicing Standard Practices - Airframe Air Conditioning Auto Flight Communications Electrical Power Equipment/Furnishings Fire Protection Flight Controls Fuel Ice and Rain Protection Indicating/Recording Systems Landing Gear Lights Navigation Oxygen Vacuum Standard Practices - Structures Doors Stabilizers Windows Wings Propellers Powerplant Engine Fuel and Control Ignition Engine Controls Engine Indicating Exhaust Oil Starting Turbines EFFECTIVE DATE* Jul 1/2007 Jul 1/2007 Mar 1/2004 Mar 1/2004 Mar 1/2004 Jul 1/2007 Mar 1/2005 Jul 3/2006 Jan 1/2007 Jan 1/2007 Jul 1/2007 Jan 1/2007 Jul 3/2006 Jan 1/2007 Mar 1/2004 Jul 1/2007 Jul 1/2007 Jan 1/2007 Jan 2/2006 Jul 3/2006 Jul 3/2006 Jul 1/2007 Jul 3/2006 Jan 2/2006 Mar 1/2004 Jul 1/2007 Mar 1/2004 Jan 2/2006 Mar 1/2004 Jul 1/2007 Jan 1/2007 Jan 1/2007 Jul 1/2007 Jan 2/2006 Jul 1/2007 Jan 1/2007 Jan 2/2006 Jul 1/2007 Mar 1/2004 FICHE/FRAME 1 B2 1 E14 1 F12 1 G2 1 G9 1 G16 1 H4 1 H10 2 A2 2 D7 2 E7 2 F6 2 G2 2 Ill 2 L2 3 A2 3 Dll 3 F2 3 G2 3 H2 3 Jill 4 A2 4 D16 4 E6 4 F2 4 F12 4 G7 4 G16 4 H7 4 12 4 115 4 L2 5 A2 5 A17 5 B4 5 C2 5 C15 5 D5 5 D12 NOTE 1: *Represents date of page one of each chapter's List of Effective Pages which is applicable to Manual revision date. LIST OF CHAPTERS Page 1 ©Cessna Aircraft Company Jul 1/2007 5 6 7 8 9 10 11 12 20 21 22 23 24 25 26 27 28 30 31 32 33 34 35 37 51 52 55 56 57 61 71 73 74 76 77 78 79 80 81 CHAPTER TIME LIMITS/ MAINTENANCE CHECKS CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL LIST OF EFFECTIVE PAGES CHAPTER-SECTION-SUBJECT 05-Title 05-List of Effective Pages 05-Record of Temporary Revisions 05-Table of Contents 5-00-00 5-00-10 5-10-00 5-1 0-01 5-11-00 5-12-00 5-12-0 1 5-1 2-02 5-12-03 5-12-04 5-1 2-05 5-12-06 5-12-07 5-1 2-08 5-1 2-09 5-12-10 5-12-11 5-12-13 5-12-14 5-12-15 5-12-16 5-12-17 5-12-18 5-12-19 5-12-20 5-12-2 1 5-1 2-22 5-1 2-23 5-12-24 5-1 2-25 5-12-26 5-50-00 Q Cessna Aircraft Company 05 - LIST OF EFFECTIVE PAGES Page 1 of 1 Jul 1/2007 PAGE Pages 1-2 Page 1 Pages 1-2 Pages 1-17 Pages 1-3 Pages 1-2 Pages 1-7 Pages 1-6 Pages 1-7 Pages 1-5 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Page 1 Pages 1-5 DATE Jul 1/2007 Mar 1/2004 Jul 3/2006 Jul 3/2006 Jul 1/2007 Jul 1/2007 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 April 1/2002 Jul 3/2006 April 1/2002 Jul 3/2006 Jul 3/2006 Jul 3/2006 April 1/2002 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jul 3/2006 Jan 2/2006 Temporary Revision Number RECORD OF TEMPORARY REVISIONS Page Number Issue Date By Date Removed By CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL CONTENTS TIME LIMITS/MAINTENANCE CHECKS ...................... Scope.................................... Inspection Requirements........................... Inspection Program Selection......................... Description ................................. General Inspection Terms and Guidelines ................... AIRWORTHINESS LIMITATIONS - FAA APPROVED DATA.............. Scope.................................... Airworthiness Limitations........................... INSPECTION TIME INTERVALS.......................... General................................... Procedure.................................. Inspection Terms and Guidelines ....................... Chart Legend ................................ INSPECTION TIME LIMITS ............................ Inspection Items............................... COMPONENT TIME LIMITS............................ General................................... Cessna-Supplied Replacement Time Limits .................. Supplier-Supplied Replacement Time Limits .................. PROGRESSIVE CARE PROGRAM ........................ General................................... Procedure.................................. Inspection Terms and Guidelines ....................... INSPECTION OPERATION 1........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 2 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 3 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 4 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION S........................... Description ................................. General Inspection Criteria .......................... PROGRESSIVE CARE .............................. Operation 6................................. INSPECTION OPERATION 7 ........................... Description ................................. General Inspection Criteria .......................... PROGRESSIVE CARE .............................. Operation 8................................. 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 1 5-00-00 Page 2 5-00-10 Page 1 5-00-10 Page 1 5-00-10 Page 1 5-10-00 Page 1 5-10-00 Page 1 5-10-00 Page 1 5-10-00 Page 1 5-1 0-00 Page 1 5-1 0-01 Pagel1 5-1 0-01 Page 1 5-11 -00 Page 1 5-11 -00 Page 1 5-11 -00 Page 1 5-11 -00 Page 2 5-12-00 Page 1 5-12-00 Page 1 5-12-00 Page 2 5-12-00 Page 2 5-12-01 Page 1 5-12-01 Page 1 5-12-01 Page 1 5-12-02 Page 1 5-12-02 Page 1 5-12-02 Page 1 5-12-03 Page 1 5-12-03 Page 1 5-12-03 Page 1 5-12-04 Page 1 5-12-04 Page 1 5-12-04 Page 1 5-12-05 Page 1 5-12-05 Page 1 5-12-05 Page 1 5-12-06 Page 1 5-12-06 Page 1 5-12-07 Page 1 5-12-07 Page 1 5-1 2-07 Page 1 5-12-08 Page 1 5-12-08 Page 1 05 - CONTENTS Page 1 of 3 Jul 1/2007 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL INSPECTION OPERATION 9 ........................... Description ............ General Inspection Criteria .......................... INSPECTION OPERATION 10........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 11........................... Description ................................. General Inspection Criteria .......................... PROGRESSIVE CARE .............................. Operation 13 ................................ INSPECTION OPERATION 14........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 15........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 16........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 17........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 18........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 19........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 20........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 21........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 22 ........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 23........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 24........................... Description ................................. General Inspection Criteria .......................... INSPECTION OPERATION 25........................... Description ................................. General Inspection Criteria .......................... 5-12-09 Page 1 5-12-09 Page 1 5-12-09 Page 1 5-12-10 Page 1 5-12-10 Page 1 5-12-10 Page 1 5-12-11 Page 1 5-12-11 Page 1 5-12-11 Page 1 5-12-13 Page 1 5-12-13 Page 1 5-12-14 Page 1 5-12-14 Page 1 5-12-14 Page 1 5-12-15 Page 1 5-12-15 Page 1 5-12-15 Page 1 5-12-16 Page 1 5-12-16 Page 1 5-12-16 Page 1 5-12-17 Page 1 5-12-17 Page 1 5-12-17 Page 1 5-12-18 Page 1 5-12-18 Page 1 5-12-18 Page 1 5-12-19 Page 1 5-12-19 Page 1 5-12-19 Page 1 5-12-20 Page 1 5-12-20 Page 1 5-12-20 Page 1 5-12-21 Page 1 5-12-21 Page 1 5-12-21 Page 1 5-12-22 Page 1 5-12-22 Page 1 5-12-22 Page 1 5-12-23 Page 1 5-12-23 Page 1 5-12-23 Page 1 5-12-24 Page 1 5-12-24 Page 1 5-12-24 Page 1 5-12-25 Page 1 5-12-25 Page 1 5-12-25 Page 1 05 - CONTENTS Page 2 of 3 Jul 1/2007 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL INSPECTION OPERATION 26........................... Description ................................. General Inspection Criteria .......................... UNSCHEDULED MAINTENANCE CHECKS .................... General................................... Unscheduled Maintenance Checks Defined and Areas of Inspection ....... 5-12-26 Page 1 5-12-26 Page 1 5-12-26 Page 1 5-50-00 Page 1 5-50-00 Page 1 5-50-00 Page 1 05 - CONTENTS Page 3 of 3 Jul 1/2007 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL TIME LIMITS/MAINTENANCE CHECKS 1.Scope A. This chapter provides the time limits and maintenance checks for the Model 182 airplanes. It is divided into several sections, each with a specific purpose toward providing information necessary to establish inspection criteria. 2. Inspection Requirements A. As required by U.S. Federal Aviation Regulations, all civil aircraft of U.S. registry must undergo a complete inspection (annual) each twelve calendar months. In addition to the required annual inspection, aircraft operated commercially (for hire) must have a complete inspection every 100 hours of operation. B. Compliance with the regulations is accomplished using one of three methods: (1) Traditional (Annual/i100 Hour) inspection program which utilizes 14 CFR 43, Appendix D (scope and detail) to inspect the airplane. In addition, Cessna recommends certain components or items be inspected at 50 hour intervals. These inspection items are listed in Inspection Time Intervals, Section 5-10-01. (2) Progressive Care inspection program which allows the work load to be divided into smaller operations that can be accomplished in a shorter time period. This method is detailed in Progressive Care Program, Section 5-12-00. (3) PhaseCard inspection program which is geared toward high-utilization flight operations (approximately 600 flight hours per year). This system utilizes 50-hour intervals (Phase 1 and Phase 2) to inspect high-usage systems and components. At 12 months or 600 flight hours, whichever occurs first, the airplane undergoes a complete (Phase 3) inspection. PhaseCard Inspection programs can be ordered through Propeller Aircraft Product Support. P.O. Box 7706, Wichita, KS 67277, Phone (316) 517-5800, Fax (316) 942-9006. 3. Inspection Program Selection A. The selection of an inspection program (Annual, Progressive Care or PhaseCard) is primarily based on owner/operator preferences, whether an airplane is flown for hire, and numbers of hours flown during the year. 4. Description A. Listed below is a brief description and intended purpose of each section of this chapter. For detailed information related to each particular inspection program, refer to the specific section within this chapter. B. Section 5-00-00, Time Limits/Maintenance Checks - General. This section provides a general overview of inspection requirements. C. Section 5-1 0-01, Inspection Time Intervals. The primary purpose of this section is to provide a central location for inspection time intervals. This section may also be utilized in conjunction with 14 CFR Part 43 to provide greater detail on inspection criteria when performing Annual/i 00 Hour inspections. D. Section 5-11 -00, Component Time Limits. This section provides a list of components which are life- or time-limited. Although these components are not listed in any of Cessna's inspection programs, they must be considered and included in whatever inspection program is used. E. Section 5-12-00, Progressive Care Program. This section outlines the progressive inspection program. The program is divided into four primary operations which cover all inspection requirements up through the 200-hour interval inspection items. The remaining operations cover inspections which are at intervals other than what the four primary operations cover. Refer to the Progressive Care Program section for a more detailed description of the Progressive Care Program. 5-00-00 Page 1 C Cessna Aircraft Company Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL 5. General Inspection Terms and Guidelines NOTE: When inspections criteria are required, these criteria are spelled out in the text. If more detailed instructions are required for an inspection, these instructions will refer to the appropriate locations (supplier publications and/or the maintenance manual). A. Definitions of terms used through the inspection programs are as follows: (1) ON CONDITION is defined as the necessary inspections and/or checks to determine that a malfunction or failure of the component will not occur prior to the next scheduled inspection. (2) CONDITION is defined as inspection for (but not limited to) cleanliness, cracks, deformation, corrosion, wear, and loose or missing fasteners. (3) SECURITY is defined as an inspection for looseness of fasteners and fastener securing devices such as safety wire, cotter pins and self-locking nuts. B. During Inspections, use the following general guidelines: (1) MOVABLE PARTS: Inspect for lubrication, servicing, security of attachment, binding, excessive wear, safetying, proper operation, proper adjustment, correct travel, cracked fittings, security of hinges, defective bearings, cleanliness, corrosion, deformation, sealing, and tension. (2) FLUID LINES AND HOSES: Inspect for leaks, cracks, bulging, collapsed, twisted, dents, kinks, chafing, proper radius, security, discoloration, bleaching, deterioration, and proper routing; rubber hoses for hardness or flexibility and metal lines for corrosion. (3) METAL PARTS: Inspect for security of attachment, cracks, metal distortion, and heat deterioration. (4) WIRING: Inspect for security, chafing, burning, arcing, defective insulation, loose or broken terminals, heat deterioration, and corroded terminals. CAUTION: Torque values listed in this manual are not to be used for checking tightness of installed parts during service. (5) STRUCTURAL FASTENERS: Inspect for correct torque in accordance with applicable torque values. Refer to Chapter 20, Torque Data - Maintenance Practices, during installation or when visual inspection indicates the need for a torque check. (6) FILTERS, SCREENS, AND FLUIDS: Inspect for cleanliness and the need for replacement at specified intervals. (7) A system check (operation or function) that requires electrical power, must be performed using 28.5 Volts, +0.25 or -1 .00 Volts, bus voltage. This will make sure that all components are I ~ ~~~operating at their operational voltage. C. Airplane file. (1) Miscellaneous data, information, and licenses are a part of the airplane file. Check that the following documents are up-to-date and in accordance with current Federal Aviation Regulations. Most of the items listed are required by the Federal Aviation Regulations. Since the regulations of other nations may require other documents and data, owners of airplanes operated outside the United States should check with their own aviation officials to determine their individual requirements. (a) To be displayed in the airplane at all times: 1 Standard Airworthiness Certificate (FAA Form 8100-2). 2 Aircraft Registration Certificate (FAA Form 8050-3). 3 Aircraft Radio Station License (Federal Communication Commission Form 556 if transmitter is installed). (b) To be carried in the airplane at all times: 1 Weight and Balance Data Sheets and associated papers (all copies of the Repair and Alteration Form, FAA Form 337, are applicable). 2 Equipment List. 3 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. (c) To be made available upon request: 1 Airplane, Engine and Propeller Logbooks. 5-00-00 Page 2 © Cessna Aircraft Company Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL AIRWORTHINESS LIMITATIONS - FAA APPROVED DATA 1. Scope A. The Airworthiness Limitations section is FAA approved and specifies maintenance required under Parts 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. 2. Airworthiness Limitations A. There are no airworthiness limitations associated with this airplane. 5-00-10 Page 1 Mar 1/2004 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL INSPECTION TIME INTERVALS 1. General A. The primary purpose of this section is to provide for inspection time intervals. The section 5-10-01 may be utilized in conjunction with 14 CFR Part 43 inspection scope and detail, but is not intended to be utilized as the primary checklist for inspection of the airplane. NOTE: The inspection guidelines contained in this section are not intended to be all inclusive, for no such charts can replace the good judgment of certified airframe and powerplant mechanics in performance of their duties. As the one primarily responsible for the airworthiness of the airplane, the owner or operator should select only qualified personnel to maintain the airplane. 2. Procedure A. A complete airplane inspection includes all inspection items as required by 14 CFR 43, Appendix D, Scope and Detail of annual/100 hour inspections. The chart provided in this section should be used to augment the inspection. B. The Component Time Limits section (5-11-00) should be checked in conjunction with this inspection to ensure proper overhaul and replacement requirements are accomplished at the specified times. C. The intervals shown are recommended intervals at which items are to be inspected based on normal usage under average environmental conditions. Airplanes operated in extremely humid areas (tropics), or in exceptionally cold, damp climates, etc., may need more frequent inspections for wear, corrosion, and lubrication. Under these adverse conditions, perform periodic inspections in compliance with this chart at more frequent intervals until the operator can set his own inspection periods based on field experience. (1) The 14 CFR Part 91 operator's inspection intervals shall not deviate from the inspection time limits shown in this manual except as provided below: (Refer to 14 CFR 91.409) (a) The aircraft can only exceed its inspection point up to ten hours if the aircraft is enroute to a facility to have the inspection completed. (b) In the event of late compliance of any operation scheduled, the next operation in sequence retains a due point from the time the late operation was originally scheduled (reschedule if late). (c) In the event of early compliance of any operation scheduled, that occurs 10 hours or less ahead of schedule, the next phase due point may remain where originally set. (d) In the event of early compliance on any operation scheduled, that occurs more than 10 hours ahead of schedule, the next phase due point must be rescheduled to establish a new due point from the time of early accomplishment. 3. Inspection Terms and Guidelines A. For inspection terms and guidelines, refer to Chapter 5, Time Limits/Maintenance Checks - General. 4. Chart Legend A. Each page of the inspection listed in Inspection Time Limits, section 5-10-01 contains the following five columns: (1) REVISION STATUS - This column provides the date that a given item was added, deleted or revised. A blank entry in this column indicates no change since the original issue of this manual. (2) INSPECTION ITEM CODE NUMBER - This column lists a six-digit number permanently assigned to a scheduled maintenance item. A given inspection item code number will never change and will not be reused in the event the scheduled maintenance item is deleted. (3) REQUIREMENTS - This column provides a short description of the inspection and/or servicing procedures. Where a more detailed description of the procedure is required, a reference will be made to either another selection located within the maintenance manual or a specific reference to a supplier publication. 5-10-00 Page 1 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL (4) INTERVAL - This column lists the frequency of inspection in alphabetic coded form. The legend for the alpha code is listed below. (5) OPERATION - The Progressive Care inspection program allows the work load to be divided into smaller operations that can be accomplished in a shorter time period. This program is detailed in section 5-12-00, which is the Progressive Care Program. (6) ZONE - This column locates the components within a specific zone. For a breakdown of how the airplane is zoned, refer to Chapter 6, Airplane Zoning - Description and Operation. INTERVAL A. B. C. D. E. F. G. H. 1. J. K. L. M. N. O. P. Q. R. S. T. U. V. W. X. Y. Z. OPERATION 1, 2, 3, 4 1, 2, 3, 4 1, 2, 3, 4 5 7 9 10 11 14 15 16 17 18 19 20 21 22 23 24 25 26 INTERVAL Every 50 hours. Every 100 hours. Every 200 hours. Every 400 hours or 1 year, whichever occurs first. (Not used) Every 600 hours or 1 year, whichever occurs first. (Not used) Every 500 hours. Every 1000 hours. Every 2 years. (Not used) (Not used) Every 2 years, or any time components are added or removed which have the potential to affect the magnetic accuracy and/or variation of the compass calibration, or any time the accuracy of the compass is in question. Every 2000 hours. Every 1000 hours or 1 year, whichever occurs first. Every 12 calendar months. Every 6 years. Every 12 years. Every 1 year. Every 3 years. (Not used) Beginning five years from the date of the manufacture, you must make sure of the serviceability of the components every twelve months. Refer to Airborne Air and Fuel Products Service Letter Number 39A or latest revision. Every 100 hours or every one year, whichever occurs first. Every 100 hours, every annual inspection, every overhaul, and any time fuel lines or clamps are serviced, removed or replaced. First 600 hours and as defined by the manufacturer thereafter. Every 1000 hours or 3 years, whichever occurs first. 5-10-00 Page 2 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL INSPECTION TIME LIMITS 1. Inspection Items REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Added 110000 Interior Placards, Exterior Placards, B 1,2,3,4 ALL Mar 1/05 Decals, Markings and Identification Plates - Inspect for security of installation and legibility. Refer to Chapter 11, Placards and Markings - Inspection/Check. Deleted 112101 Mar 1/04 Deleted 113101 Mar 1/04 212001 Ventilation System - Inspect clamps, D 5 211 hoses, and valves for condition and security. Revised 212002 Primary Flight Display (PFD) Fan, W 23 220, 225 Mar 1/05 Multi-Function Display (MFD) Fan, Deck Skin Fan, and Remote Avionics Cooling Fan - Operational Check. Refer to Chatper 21, Avionics Cooling - Maintenance Practices. 214001 Cold and Hot Air Hoses - Check B 2, 4 120 condition, routing, and security. Revised 214002 Heater Components, Inlets, and B 1,3 211 Dec 1/98 Outlets - Inspect all lines, ducts, clamps, seals, and gaskets for condition, restriction, and security. Revised 214003 Cabin Heat and Ventilation Controls - B 1 211 Jun 1/00 Check freedom of movement through full travel. Check friction locks for proper operation. 221001 Autopilot Rigging- Refer to Autopilot- F 7 610 Maintenance Practices. Added 221002 Autopilot Servo Capstan Assemblies. O 16 610 Dec 1/98 Check slip-clutch torque settings. Refer to Autopilot - Maintenance Practices. Added 221003 Autopilot Servo Actuators. Inspect for O 16 610 Dec 1/98 evidence of corrosion and or buildup of dirt or other particulate matter which may interfere with servo operation. Refer to Autopilot - Maintenance Practices. 5-10-01 Page 1 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER 231001 Communication Antennas and Cables C 3 210 - Inspect for security of attachment, connection, and condition. 235001 Microphones, Headsets, and Jacks - C 1 211 Inspect for cleanliness, security, and evidence of damage. Added 235002 Microphone Push-To-Talk Switch B 1, 3 222, 223 4/03 - Clean the pilot's and copilot's microphone switches. Refer to Chapter 23, Communication Maintenance Practices. 242001 Alternator, Mounting Bracket, and A 1,2, 3, 4 120 Electrical Connections - Check condition and security. Check alternator belts for condition and proper adjustment. Check belt tension. Revised 243001 Main Battery - Examine the general B 2, 4 310 Jun 3/06 condition and security. Complete a check of the level of electrolyte. Refer to Chapter 12, Battery - Servicing. Revised 243002 Main Battery Box and Cables - Clean B 2, 4 310 Jun 3/06 and remove any corrosion. Examine the cables for routing, support, and security of the connections. 243003 General Airplane and System Wiring C 1 210 - Inspect for proper routing, chafing, broken or loose terminals, general condition, broken or inadequate clamps, and sharp bends in wiring. 243004 External Power Receptacle and C 2 120 Power Cables - Inspect for condition and security. Added 243005 Standby Battery - Complete the S 20 220 Mar 1/05 Standby Battery Capacity Test. Refer to Chapter 24, Standby Battery - Maintenance Practices. 246001 Switch and Circuit Breaker Panel, C 1 222 Terminal Blocks, and Junction Boxes - Inspect wiring and terminals for condition and security. Revised 246002 Power Junction Box - Check B 1, 3 222 Jun 1/00 operation and condition. Check availability and condition of spare fuse (if applicable). 5-10-01 Page 2 Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Added 246003 Alternator Control Unit - Complete J 11 222 Jul 3/06 the Over-voltage Protection Circuit Test. Refer to Chapter 24, Alternator Control Unit. Revised 246101 Essential and Crossfeed Bus Diodes - S 20 224 Mar 1/05 Check for proper operation. Complete the Essential and Crossfeed Bus Diode Inspection. Refer to Chapter 24, Essential and Crossfeed Bus Diodes - Maintenance Practices. Revised 251001 Seats - Examine the seats to make B 1, 3 211 Jul 3/06 sure they are serviceable and installed correctly. Make sure the seat stops and adjustment mechanism operate correctly. Examine the seat recline control and attaching hardware to make sure the hardware and lock are not damaged and are correctly installed. Lubricate the threads of the Seat Crank Handle Assembly with MIL-PRF-81322 general purpose grease. 251002 Seat Tracks and Stops - Inspect seat B 2, 4 230 tracks for condition and security of installation. Check seat track stops for damage and correct location. Inspect seat rails for cracks. 251101 Restraint System, front and rear - B 1,3 211 Check belts for thinning, fraying, cutting, broken stitches, or ultra-violet deterioration. Check system hardware for security of installation. Added 251102 AMSAFE Aviation Inflatable Restraint S 20 211 Mar 1/05 (AAIR) - Examine the restraint for dirt, frayed edges, unserviceable stitching, loose connections, and other wear. 252201 Upholstery, Headliner, Trim, and D 5 211 Carpeting - Check condition and security. Revised 256001 Emergency Locator Transmitter - B 1, 3 310 Jan 2/05 Inspect for security of attachment and check operation by verifying transmitter output. Check cumulative time and useful life of batteries in accordance with 14 CFR Part 91.207. 262001 Portable Hand Fire Extinguisher - B 1, 3 230 Inspect for proper operating pressure, condition, security of installation, and servicing date. 5-10-01 Page 3 © Cessna Aircraft Companv Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Added 262002 Cockpit Mounted Halon Type Fire P 17 211 Dec 1/98 Extinguisher - Weigh bottle. Bottle must be reserviced by qualified individual if more than 2 ounces is lost. Added 262003 Cockpit Mounted Halon Type Fire R 19 211 Dec 1/98 Extinguishers - Perform hydrostatic test. The hydrostatic test shall be at twelve-year intervals based on initial servicing or date of last hydrostatic test. Added 262004 Cockpit Mounted Halon Type Fire Q 18 211 Dec 1/98 Extinguishers - Empty, inspect for damage, and recharge. Revised 271001 Aileron Controls - Check freedom B 1,3 120, 520, Dec 1/98 of movement and proper operation 620 through full travel. 271002 Ailerons and Cables - Check C 3 120, 520, operation and security of stops. 620 Check cables for tension, routing, fraying, corrosion, and turnbuckle safety. Check travel if cable tension requires adjustment or if stops are damaged. Check fairleads and rub strips for condition. 271003 Aileron Structure, Control Rods, B 1,3 520, 620 Hinges, Balance Weights, Bellcranks, Linkage, Bolts, Pulleys, and Pulley Brackets - Check condition, operation, and security of attachment. 271004 Ailerons and Hinges - Check B 1, 3 520, 620 condition, security, and operation 271005 Control Wheel Lock - Check general C 1 222 condition and operation. Revised 271006 Control Linkage - Inspect pulleys, C 1 222, 223 Dec 1/98 cables, bearings, and turnbuckles for condition and security. 272001 Rudder - Check internal surfaces for C 3 340 corrosion, condition of fasteners, and balance weight attachment. 5-1 0-01 Page 4 Jul 3/2006 Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Revised 272002 Rudder - Inspect the rudder skins for B 1, 3 340 Jun 1/00 cracks and loose rivets, rudder hinges for condition, cracks and security; hinge bolts, hinge bearings, hinge attach fittings, and bonding jumper for evidence of damage and wear, failed fasteners, and security. Inspect balance weight for looseness and the supporting structure for damage. Revised 272003 Rudder, Tips, Hinges, Stops, Clips B 1, 3 340 Dec 1/98 and Cable Attachment - Check condition, security, and operation. 272004 Rudder Pedals and Linkage - Check C 1 230 for general condition, proper rigging, and operation. Check for security of attachment. Added 272005 Rudder Control - Check freedom B 1, 3 340 Dec 1/98 of movement and proper operation through full travel. Check rudder stops for damage and security. Revised 273001 Elevator Control - Check freedom B 1,3 222, 223 Dec 1/98 of movement and proper operation through full travel. Revised 273002 Elevator Control System - Inspect B 1, 3 222, 223 Jun 1/00 pulleys, cables, sprockets, bearings, chains, and turnbuckles for condition, security, and operation. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety Revised 273003 Elevator, Hinges, Stops, and Cable B 1, 3 320, 330 Dec 1/98 Attachment - Check condition, security, and operation. Added 273004 Elevator Downspring - Check B 1,3 310 Dec 1/98 structure, bolts, linkage, bell crank, and push-pull tube for condition, operation, and security. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety. Check travels if cables require tension adjustment or if stops are damaged. 273101 ElevatorTrim System - Check cables, B 1, 3 224, 240, push-pull rods, bellcranks, pulleys, 310 turnbuckles, fairleads, rub strips, etc. for proper routing, condition, and security. 5-10-01 Page 5 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Revised 273102 Elevator Trim Control and Indicator C 1 224, 240, Jun 1/00 - Check freedom of movement and 310 proper operation through full travel. Check pulleys, cables, sprockets, bearings, chains, and turnbuckles for condition and security. Check electric trim controls for operation as applicable. Check cables for tension, routing, fraying, corrosion, and turnbuckle safety 273103 ElevatorTrimTaband Hinges-Check B 1, 3 224 condition, security, and operation. Revised 273104 Elevator Trim Tab Actuator - Examine B 1, 3 320 Jul 3/06 the free play limits. Refer to Chapter 27, Elevator Trim Control - Maintenance Practices, Trim Tab Free Play Inspection. If the free play is more than the permitted limits, lubricate the actuator and examine the free play limits again. If the free play is still more than the permitted limits, replace the actuator. Deleted 273105 Dec 1/98 273106 Elevator Trim Tab Stop Blocks - C 1 240 Inspect for damage and security. Added 273107 Elevator Trim Tab Actuator - Remove, Z 26 320 Jul 3/06 clean, examine, and lubricate the actuator. Refer to Chapter 27, Elevator Trim Control - Maintenance Practices. Revised 275001 Flaps - Check tracks, rollers, B 1,3 510, 610 Dec 1/98 and control rods for security of attachment. Check rod end bearings for corrosion. Check operation. 275002 Wing Flap Control - Check operation C 1 221 through full travel and observe Flap Position indicator for proper indication. 275003 Flap Structure, Linkage, Bellcranks, C 3 510, 610 Pulleys, and Pulley Brackets - Check for condition, operation and security. 275004 Flaps and Cables - Check cables C 3 510, 610 for proper tension, routing, fraying, corrosion, and turnbuckle safety. Check travel if cable tension requires adjustment. 5-10-01 Page 6 C Cessna Aircraft Comoanv Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Revised 275005 Flap Motor, Actuator, and Limit C 3 610 Dec 1/98 Switches - Check wiring and terminals for condition and security. Check actuator for condition and security. Revised 275006 Flap Actuator Threads - Clean and B 1, 3 610 Dec 1/98 lubricate. Refer to Chapter 12-21-03. 282001 Fuel System - Inspect plumbing B 1,3 510, 610 and components for mounting and security. Revised 282002 Fuel Tank Vent Lines and Vent Valves B 1,3 510, 610 Dec 1/98 - Check vents for obstruction and proper positioning. Check valves for operation. Revised 282003 Fuel Selector Valve - Check controls B 1, 3 224 Jun 1/00 for detent in each position, security of attachment, and for proper placarding. Revised 282004 Integral Fuel Bays - Check for B 1, 3 510, 610 Dec 1/98 evidence of leakage and condition of fuel caps, adapters, and placards. Using quick drains, ensure no contamination exists. Check quick drains for proper shut off. Deleted 282005 Aug 4/03 282006 Fuel Selector - Using quick drain, B 1,3 224 ensure no contamination exists. 282007 Fuel Strainer, Drain Valve, and B 1, 3 510, 610 Controls - Check freedom of movement, security, and proper operation. Disassemble, flush, and clean screen and bowl. Revised 282008 Fuel Quantity Indicators - Examine for F 7 220 Mar 1/05 damage and security of installation. Complete a fuel quantity calibration check. Refer to Chapter 28, Fuel Storage and Distribution - Maintenance Practices. 5-10-01 Page 7 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Revised 282009 Integral Fuel Bays - Drain the I 10 510, 610 Jan 2/06 fuel (Refer to Chapter 12, Fuel - Servicing) and purge tanks (Refer to the Single Engine Structural Repair Manual, 1996 and On). Complete an inspection of the tank interior and outlet screens and remove any foreign object debris. Complete an inspection of the tank interior surfaces for sealant deterioration and corrosion (especially in the sump areas). Revised 282010 Auxiliary (Electric) Fuel Pump - B 2, 4 120 Jun 1/00 Check pump and fittings for condition, operation, security. 311001 Instruments - Check general condition B 1, 3 220 and markings for legibility. Deleted 311002 Mar 1/05 311003 Instrument Lines, Fittings, Ducting, C 1 220 and Instrument Panel Wiring - Check for proper routing, support, and security of attachment. Revised 321001 Main Landing Gear Wheel Fairings B 2, 4 721,722 Jun 1/00 and Brake Fairings - Check for cracks, dents, and condition of paint. Revised 321002 Main Gear Spring Assemblies - B 2,4 721,722 Mar 1/05 Examine for cracks, dents, corrosion, condition of paint or other damage. Examine for chips, scratches, or other damage that lets corrosion get to the steel spring. Examine the axles for condition and security. 321003 Main Landing Gear Attachment B 2, 4 721,722 Structure - Check for damage, cracks, loose rivets, bolts and nuts and security of attachment. 322001 Nose Gear - Inspect torque links, B 2, 4 720 steering rods, and boots for condition and security of attachment. Check strut for evidence of leakage and proper extension. Check strut barrel for corrosion, pitting, and cleanliness. Check shimmy damper and/or bungees for operation, leakage, and attach points for wear and security. 322002 Nose Landing Gear Wheel Fairings B 2, 4 720 - Check for cracks, dents, and condition of paint. 5-10-01 Page 8 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER 322003 Nose Gear Fork - Inspect for cracks, C 4 720 general condition, and security of attachment. 322004 Nose Gear Attachment Structure - B 2, 4 720 Inspect for cracks, corrosion, or other damage and security of attachment. 324001 Brakes - Test toe brakes and parking B 2, 4 230 brake for proper operation. Revised 324002 Brakes, Master Cylinders, and B 2, 4 224, 230 Dec 1/98 Parking Brake - Check master cylinders and parking brake mechanism for condition and security. Check fluid level and test operation of toe and parking brake. Refer to Chapter 12-13-00 for servicing instructions. 324003 Brake Lines, Wheel Cylinders, Hoses, D 5 721, 722 Clamps, and Fittings - Check for leaks, condition, and security and hoses for bulges and deterioration. Check brake lines and hoses for proper routing and support. 324004 Tires - Check tread wear and general B 2, 4 720, 721, condition. Check for proper inflation. 722 324005 Wheels, Brake Discs, and Linings B 2, 4 721,722 - Inspect for wear, cracks, warps, dents, or other damage. Check wheel through-bolts and nuts for looseness. Revised 324006 Wheel Bearings - Clean, inspect and B 4 720, 721, Dec 1/98 lube. 722 325001 Nose Gear Steering Mechanism - C 4 720 Check for wear, security, and proper rigging. 331001 Instrument and Cabin Lights - Check B 1, 3 220, 211, operation, condition of lens, and 221 security of attachment. 334001 Navigation, Beacon, Strobe, and B 1, 3 340, 520, Landing Lights - Check operation, 620 condition of lens, and security of attachment. 341101 Static System - Inspect for security of C 3 210 installation, cleanliness, and evidence of damage. Revised 341102 Pitot and Static System - Examine in J 11 220 Jul 3/06 accordance with 14 CFR Part 91.411. 5-10-01 Page 9 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER 341103 Pitot Tube and Stall Warning Vane - A 1,2, 3, 4 510 Check for condition and obstructions and verify operation of anti-ice heat. 342101 Magnetic Compass - Inspect for C 1 225 security of installation, cleanliness, and evidence of damage. Revised 342102 Magnetic Compass - Calibrate. M 14 220 Dec 1/98 Revised 345001 Instrument Panel Mounted Avionics C 1 225 Dec 1/98 Units (Including Audio Panel, VHF Nav/Com(s), ADF, GPS, Transponder, Compass System, Multi-function Display, and Primary Flight Display) and Remote Mounted Avionics Components. Inspect for deterioration, cracks, and security of instrument panel mounts. Inspect for security of electrical connections, condition, and security of wire routing. 345002 Avionics Operating Controls - Inspect C 1 225 for security and proper operation of controls and switches and ensure that all digital segments will illuminate properly. 345003 Navigation Indicators, Controls, and C 1 220, 225 Components - Inspect for condition and security. 345004 Navigation Antennas and Cables - C 1 310 Inspect for security of attachment, connection, and condition. Added 351001 Oxygen System (if applicable) - C 1 211 Nov 1/00 Inspect masks, hoses, lines, and fittings for condition, routing, and support. Test operation and check for leaks. Added 351002 Oxygen Cylinder (if applicable) T 21 211 Nov 1/00 - Inspect for condition, check hydrostatic test date and perform hydrostatic test, if due. 371001 Vacuum System - Inspect for B 2, 4 120 condition and security. 371002 Vacuum Pumps - Check for condition B 2, 4 120 and security. Check vacuum system breather line for obstructions, condition, and security. 5-10-01 Page 10 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER 371003 Vacuum System Hoses - Inspect for B 2, 4 120 hardness, deterioration, looseness, or collapsed hoses. Revised 371004 Gyro Filter - Inspect for damage, B 2, 4 120 Dec 1/98 deterioration and contamination. Clean or replace if required. Deleted 371005 Aug 4/03 Revised 371006 Vacuum Manifold Check Valve V 22 120 Jan 2/06 - Complete a check for proper operation. (Only airplanes with dual vacuum pumps and Airborne manifolds. Refer to the Airborne Air & Fuel Products Service Letter Number 39A or latest revision, and in accordance with SB02-37-04.) Refer to Chapter 37, Vacuum System - Maintenance Practices for the removal and installation of the check valve. Added 371007 Do an inspection of the wear indicator Y 25 120 Jan 2/06 ports on the vacuum pumps described in Tempest Service Letter 004. 521001 Doors - Inspect general condition. B 1,3 210 Check latches, hinges, and seals for condition, operation, and security of attachment. 531001 Fuselage Surface - Inspect for skin B 1,3 210 damage, loose rivets, condition of paint, and check pitot-static ports and drain holes for obstruction. Inspect covers and fairings for security. 531002 Firewall Structure - Inspect for C 2 120 wrinkles, damage, cracks, sheared rivets, etc. Check cowl shock mounts for condition and security. 531003 Internal Fuselage Structure - Inspect C 1 211 bulkheads, doorposts, stringers, doublers, and skins for corrosion, cracks, buckles, and loose rivets, bolts and nuts. 5-10-01 Page 11 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER Revised 551001 Horizontal Stabilizer and Tailcone B 1, 3 320, 330 Dec 1/98 structure - Inspect bulkheads, spars, ribs, and skins, for cracks, wrinkles, loose rivets, corrosion, or other damage. Inspect horizontal stabilizer attach bolts for looseness. Retorque as necessary. Check security of inspection covers, fairings, and tips. Revised 551002 Horizontal Stabilizer and Tips - B 1, 3 320, 330 Dec 1/98 Inspect externally for skin damage and condition of paint. Revised 553001 Vertical Stabilizer Fin - Inspect B 1, 3 340 Dec 1/98 bulkheads, spars, ribs, and skins for cracks, wrinkles, loose rivets, corrosion, or other damage. Inspect vertical stabilizer attach bolts for looseness. Retorque as necessary. Check security of inspection covers, fairings, and tip. Revised 553002 Vertical Stabilizer Fin and Tailcone B 1, 3 340 Dec 1/98 - Inspect externally for skin damage and condition of paint. 561001 Windows and Windshield - Inspect B 1, 3 210 general condition. Check latches, hinges, and seals for condition, operation, and security of attachment. 571001 Wing Surfaces and Tips - Inspect B 1, 3 510, 520, for skin damage, loose rivets, and 610, 620 condition of paint. 571002 Wing Struts and Strut Fairings - Check B 1, 3 510, 610 for dents, cracks, loose screws and rivets, and condition of paint. 571003 Wing Access Plates - Check for C 3 510, 520, damage and security of installation. 610, 620 571004 Wing Spar and Wing Strut Fittings C 3 510, 520, - Check for evidence of wear. 610, 620 Check attach bolts for indications of looseness and retorque as required. 571005 Wing Structure - Inspect spars, C 3 510, 520, ribs, skins, and stringers for cracks, 610, 620 wrinkles, loose rivets, corrosion, or other damage. 611001 Spinner - Check general condition A 1, 2, 3, 4 110 and attachment. Revised 611002 Spinner and Spinner Bulkhead - B 2, 4 110 Jan 3/05 Remove spinner, wash, and inspect for cracks and fractures. 5-10-01 Page 12 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM STATUS CODE NUMBER 611003 611004 611005 611006 Added Nov 1/00 Added Dec 1/98 Revised Aug 4/03 Added Dec 15/01 Added Nov 1/00 Revised Aug 4/03 611007 612001 612002 612003 710001 710002 TASK Propeller Blades - Inspect for cracks, dents, nicks, scratches, erosion, corrosion, or other damage. Propeller Hub - Check general condition. Propeller Mounting - Check for security of installation. Propeller Mounting Bolts - Inspect mounting bolts and safety wire for signs of looseness. Retorque mounting bolts as required. Propeller Heat Slip Rings, Brushes, and Boots - Inspect for condition, and security. Perform operational check. Propeller Governor and Control - Inspect for oil and grease leaks. If leakage is evident, refer to McCauley Service Manual. Propeller Governor and Control - Check for security and operation of controls. Maximum linear freeplay is 0.050 inch. Propeller Control Cable - Non- repairable item and must be replaced at every interval or whenever maximum linear movement exceeds 0.050 inch. Refer to Chapter 61-20-00, Propeller Control Cable. Turbocharger (if applicable) Inspect turbocharger mounting brackets, ducting, linkage, and attaching parts for general condition, leakage or damage, and security of attachment. Check waste gate, actuator, controller, oil and vent lines, overboost relief valve, and compressor housing for leakage, apparent damage, security of attachment, and evidence of wear. Check waste gate return spring for condition and security. Turbocharger (if applicable) Examine the turbocharger for burned areas, bulges, or cracks. Use a flashlight and mirror in the tailpipe to examine the turbine for coking, carbonization, oil deposits, and turbine impellers for damage. INTERVAL OPERATION ZONE A C A 1,2, 3,4 2 110 110 1,2,3,4 110 C A 2 1,2,3,4 110 110 1,2,3,4 110 A C 2 15 N A C 110 120,210 1,2,3,4 120 2 120 5-10-01 Page 13 Jul 3/2006 © Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM STATUS CODE NUMBER TASK INTERVAL OPERATION ZONE Cowling and Cowl Flaps - Inspect for cracks, dents, other damage and security of cowl fasteners. Check cowl flaps for condition, security, and operation. Check cowl flap controls for freedom of movement through full travel. Engine Shock Mounts, Engine Mount Structure, and Ground Straps - Check condition, security, and alignment. Alternate Induction Air System - Check for obstructions, operation, and security. Induction System - Check security of clamps, tubes, and ducting. Inspect for evidence of leakage. Induction Airbox, Valves, Doors, and Controls - Remove air filter and inspect hinges, doors, seals, and attaching parts for wear and security. Check operation. Induction Air Filter - Remove and clean. Inspect for damage and service. Fuel line (Stainless steel tube assembly) and support clamp inspection and installation. Refer to Lycoming Service Bulletin Number 342E or later version. Engine - Inspect for evidence of oil and fuel leaks. Wash engine and check for security of accessories. Crankcase, Oil Sump, and Accessory Section - Inspect for cracks and evidence of oil leakage. Check bolts and nuts for looseness and retorque as necessary. Check crankcase breather lines for obstructions, security, and general condition. Hoses, Metal Lines, and Fittings - Inspect for signs of oil and fuel leaks. Check for abrasions, chafing, security, proper routing and support and for evidence of deterioration. A C A A 1,2,3,4 120 2 1,2,3,4 120 120 1,2,3,4 120 B 2, 4 A 2, 4 X A 24 120 120 120 1,2,3,4 120 B 2, 4 A 120 1,2,3,4 120 5-10-01 Page 14 Jul 3/2006 © Cessna Aircraft Company Revised Dec 1/98 711001 712001 716001 716002 Revised Jun 1/00 716003 716004 Added Jan 2/06 720000 722001 722002 722003 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL . REVISION ITEM TASK INTERVAL OPERATION ZONE STATUS CODE NUMBER 723001 Engine Cylinders, Rocker Box B 2, 4 120 Covers, and Pushrod Housings - Check for fin damage, cracks, oil leakage, security of attachment, and general condition. 723002 Engine Metal Lines, Hoses, Clamps, C 2 120 and Fittings - Check for leaks, condition, and security. Check for proper routing and support. 723003 Engine Baffles and Seals - Check A 1,2, 3, 4 120 condition and security of attachment. Revised 723004 Cylinder Compression - Complete B 2, 4 120 Jan 2/06 a differential compression test. If there is weak cylinder compression, refer to Chapter 71, Engine -Troubleshooting, for further procedures. 730001 Engine-Driven Fuel Pump - Check B 2, 4 120 for evidence of leakage, security of attachment, and general condition. 730002 Fuel Injection System - Check system B 2, 4 120 for security and condition. Clean fuel inlet screen, check and clean injection nozzles and screens (if evidence of contamination is found), and lubricate air throttle shaft. Added 730003 Idle and Mixture - Run the airplane B 2, 4 120 Jun 18/01 engine to determine satisfactory performance. If required, adjust the idle rpm and fuel mixture. Refer to Chapter 73, Fuel Injection Systems - Maintenance Practices. Revised 741001 Magnetos - Examine the external B 2, 4 120 Jan 2/06 condition and for correct installation and condition of the electrical leads. Complete a check of the engine timing (external timing). You must set the internal timing if the total of all external adjustments are more than 0.125 inch (3.17 mm) from the original factory position, or between each of the internal timing adjustments. Refer to Chapter 74, Ignition System - Maintenance Practices. Revised 741002 Magnetos - Clean, examine, and H 9 120 Jul 3/06 adjust as necessary. Do the 500-hour inspection in accordance with the Slick 4300/6300 Series Magneto Maintenance and Overhaul Manual. 5-10-01 Page 15 © Cessna Aircraft Company Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM STATUS CODE NUMBER 742001 742002 743001 Revised Jun 1/00 Revised Jan 2/06 Revised Dec 1/98 Added Nov 1/00 743002 761001 781001 781002 TASK Ignition Harness Check for deterioration, ar terminals. and Insulators proper routing, nd condition of Spark Plugs - Remove, clean, analyze, test, gap, and rotate top plugs to bottom and bottom plugs to top. Ignition Switch and Electrical Harness - Inspect for damage, condition, and security. Inspect and lubricate ACS brand ignition switch. Refer to Chapter 74, Ignition System - Maintenance Practices. Engine Controls and Linkage - Examine the general condition and freedom of movement through the full range. Complete a check for the proper travel, security of attachment, and for evidence of wear. Complete a check of the friction lock and vernier adjustment for proper operation. Complete a check to make sure the throttle, fuel mixture, and propeller governor arms operate through their full arc of travel. The maximum linear freeplay is 0.050 inch. Exhaust System - Inspect for cracks and security. Special check in area of heat exchanger. Refer to Chapter 78, Exhaust system - Maintenance Practices. Exhaust System (turbocharged engine) - Inspect couplings, seals, clamps, and expansion joints for cracks. Special check in area of heat exchanger. Refer to Chapter 78, Exhaust System - Maintenance Practices. Note: This inspection is specifically required for German (LBA) certification. INTERVAL OPERATION ZONE 2, 4 B B B N B A A 2,4 2, 4 15 120 120 120 224 1,2,3,4 120,225 1,2,3,4 120 1, 2, 3,4 5-10-01 © Cessna Aircraft Company 120 Page 16 Jul 3/2006 CESSNA AIRCRAFT COMPANY MODEL 182/T182 MAINTENANCE MANUAL REVISION ITEM STATUS CODE NUMBER TASK INTERVAL OPERATION ZONE Engine Oil - Drain oil sump and oil cooler. Check for metal particles or foreign material in filter, on sump drain plug, and on engine suction screen. Refer to Textron Lycoming Service Bulletin # 480C or latest revision. Replace filter, and refill with recommended grade aviation oil. Oil Cooler - Check for obstructions, leaks, and security of attachment. Starter and Electrical Connections - Check security and condition of starter, electrical connection, and cable. Bendix Drive Starter Assembly - Clean and lubricate starter drive assembly. A 1,2,3,4 120 A 1,2,3,4 120 B 2,4 A 120 1,2,3,4 120 5-10-01 Page 17 Jul 3/2006 © Cessna Aircraft Company Revised Jun 1/00 791001 792001 Revised Jun 1/00 Added Apr 1/02 801001 801002 CESSNA AIRCRAFT COMPANY MODEL 182/Ti 82 MAINTENANCE MANUAL COMPONENT TIME LIMITS 1.General A. Most components given in Chapter 5 must be examined as shown elsewhere in this chapter and repaired, overhauled, or replaced as necessary. Some components have a time or life limit and must be overhauled or replaced on or before the specified limit. B. The terms overhaul and replacement as used within this section are defined as follows: (1) Overhaul - Overhaul the item as given in 14 CFR 43.2 or replace it. (2) Replacement - Replace the item with a new item or a serviceable item that is within its service life and time limits or has been rebuilt as given in 14 CFR 43.2. C. This section (5-11 -00) gives a list of items which must be overhauled or replaced at specific time limits. Cessna-Supplied Replacement Time Limits shows those items which Cessna has found necessary to overhaul or replace at specific time limits. Supplier-Supplied Replacement Time Limits shows component time limits which have been given by an outside supplier for their products. In addition to these time limits, the components shown in this section are also examined at regular time intervals given in the Inspection Time Intervals section. If necessary, based on service use and inspection results, these components can be overhauled or replaced before their time limit is reached. 2. Cessna-Supplied Replacement Time Limits A. Equipment/Furnishings (Chapter 25). (1) 504516-401 -XXXX Restraint System, Pilot's Left Hand or Right Hand Auto Adjust - Replace every 10 years. (2) 504851-401-XXXX Restraint System, Pilot's Left Hand or Right Hand Manual Adjust - Replace every 10 years. (3) 50451 6-403-XXXX Restraint System, Aft Bench Left Hand or Right Hand Auto Adjust - Replace every 10 years. (4) 504851-403-XXXX Restraint System, Aft Bench Left Hand or Right Hand Manual Adjust - Replace every 10 years. (5) 2000031-09-201 Restraint Assembly, Pilot's Seat - Replace every 10 years. (6) 2000031-10-201 Restraint Assembly, Copilot's Seat - Replace every 10 years. (7) 2000031-11 -201 Restraint Assembly, Right Rear Seat - Replace every 10 years. (8) 2000031-12-201 Restraint Assembly, Left Rear Seat - Replace every 10 years. B. Flight Controls (Chapter 27). (1) 1260074-1 Trim Tab Actuator - Replace the trim tab actuators when the free play cannot be kept in limits by the adjustment or replacement of the rod ends, rod end bolts, screw assembly, and the lubrication of the trim tab actuator. (2) 1260074-7 Trim Tab Actuator (with dual axis autopilot) - Replace the trim tab actuators when the free play cannot be kept in limits by the adjustment or replacement of the rod ends, rod end bolts, screw assembly, and the lubrication of the trim tab actuator. C. Vacuum (Chapter 37). (1) C294502-0201 Gyro Filter - Replace at 600 hours. D. Propeller (Chapter 61). (1) 565-580-038 Propeller Control Cable - Replace at engine TBO. E. Powerplant (Chapter 71). (1) Engine Compartment Flexible Fluid-Carrying Teflon Hoses (Cessna-Installed), Except Drain Hoses - Replace every 10 years or at the engine overhaul, whichever occurs first. NOTE: This life limit is intended not to let flexible, fluid-carrying Teflon hoses in a deteriorated or damaged condition stay in service. Replace the flexible, fluid-carrying Teflon hoses in the engine compartment (Cessna-installed only) every 10 years or at the engine overhaul, whichever occurs first. This does not include drain hoses. Serviceable hoses which are beyond these limits must be put on order immediately and replaced within 30 days after the new hose is received from Cessna. 5-1 1-00 Page 1 C Cessna Aircraft Company Jul 1/2007 CESSNA AIRCRAFT COMPANY MODEL 182/Ti82 MAINTENANCE MANUAL (2) Engine Compartment Drain Hoses - Replace on condition. (3) Engine Flexi