Cessna 182S/182T/T182T Aircrafts Electrical Wiring Diagrams Manual

ATextron Company Wiring Diagram Ma nual. MODEL 182S, 182T SERIAL NUMBERS 18280001 AND ON AND MODEL T182T SERIAL NUMBERS T18208001 AND ON 0) Member of GAMA. COPYRIGHT © 1997 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 1 82SWD05 3 FEBRUARY 1997 Revision 5 1 JANUARY 2007 Revision 5 Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 182/T182 WIRING DIAGRAM MANUAL RECORD OF REVISIONS DATE DATE PAGE REVISION INSERTED REMOVED NUMBER NUMBER DATE DATE PAGE INSERTED REMOVED NUMBER REVISION NUMBER Island Enterprises

MODEL 182VTi 82 WIRING DIAGRAM MANUAL CHAPTER SECTION SUBJECT Title Record of Revisions Introduction-List of Effective Pages List of Revisions Introduction Zone Numbering System Light Bulb Replacement Guide Fuse Replacement Guide Service Bulletin List Vendor Address List Engineering Approved Abbreviations List of Chapters Alphabetical Index Component Index Reference Designator Index Part Number Index NUMBER OF PAGES DATE 1 Janl1/2007 1 1 Janl1/2007 1 Janl1/2007 12 Mar 1/2004 3 Mar 1/2004 2 Mar 1/2004 1 Mar 1/2004 3 Mar 1/2004 3 Feb 13/2006 2 Mar 1/2004 1 Janl1/2007 5 Feb 13/2006 6 Feb 13/2006 37 Feb 13/2006 21 Feb 13/2006 INTRODUCTION - EFFECTIVITIES © Cessna Aircraft Company Page 1 Janl1/2007 Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 182/TI182 WIRING DIAGRAM MANUAL LIST OF REVISIONS 1. Effectivity A. This Wiring Diagram Manual covers Model 182S and 182T1 Airplanes 18280001 and ON and Model Ti182T1 Airplanes Ti18208001 and ON. NOTE: Information in this Wiring Diagram Manual is applicable to U.S. and foreign certified model 182S and 182T1 Airplanes 18280001 and ON and Model T1 82T, Airplanes T1 8208001 and ON. Information unique to a particular country is identified in the chapter(s) affected. 2. Revisions A. This Wiring Diagram Manual includes the original issue and the following listed revisions. To ensure that information in this manual is current, the revisions shall be incorporated in to the manual as they are issued. Original Issue - 3 February 1997 Revision 1 - 1 November 2000 Revision 2 - 18 June 2001 Revision 3 - 1 March 2004 Revision 4 - 13 February 2006 Revision 5 - 1 January 2007 © Cessna Aircraft Company LIST OF REVISIONS Page 1 Janl1/2007 I I Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 182/T182 WIRING DIAGRAM MANUAL INTRODUCTION 1. Coverage A. The Wiring Diagram Manuai is prepared in accordance with Air Transport Association Specification 100 for Manufacturer's Technical Data. B. The information in this publication is based on data available at the time of publication and is updated, supplemented, and automatically amended by all information issued in Service News Letters, Service Bulletins, Special Service Projects, 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 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. 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. Inspection, maintenance and parts requirements for Supplemental Type Certification (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. D. This manual has been prepared to assist personnel in maintaining wiring and electrical/electronic components in this airplane and provides the necessary information required to troubleshoot, remove and replace components or repair systems. E. Information beyond the scope of this manual may be found in the Maintenance Manual, Illustrated Parts Catalog and Structural Repair Manual. For technical assistance concerning this manual, contact Cessna Aircraft Company, Propeller Aircraft Product Support. F. Technical Publications available from suppliers of various components and systems, which are not covered in this manual, must be utilized as required for maintenance of those components. INTRODUCTION Page 1 c Cessna Aircraft Company Mar 1/2004 Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 182/Ti182 WIRING DIAGRAM MANUAL G. Publications for this model are available in paper, aerofiche and CD-ROM versions. For information concerning the different versions and availability of these publications, contact Cessna Aircraft Company, Propeller Aircraft Product Support. (1) Paper versions are available as individual publications. (2) Aerofiche versions are available as individual publications. Aerofiche versions are a copy of the paper version of the manual. (3) Maintenance Manual, Illustrated Parts Catalog, Wiring Diagram Manual and Structural Repair Manual CD-ROM versions are grouped together on a CD-ROM. Refer to the CD-ROM introduction for information about items marked as (Paper version of this manual only.). 2. Effectivity A. This Wiring Diagram Manual covers 182 series 1997 & on. NOTE: Information in this Wiring Diagram Manual is applicable to U.S. and foreign certified models. Information unique to a particular country is identified in the chapter(s) affected. 3. List of Effective Pages(Paper version of this manual only.) A. A list of effective pages is provided with each wiring diagram manual chapter. All pages in the chapter are listed in sequence with the most recent revision date for each page. 4. Temporary Revision(Paper version of this manual only.) A. Additional information which becomes available will be provided through temporary revision. This service is used to provide, without delay, new information which will assist in maintaining safe and efficient flight/ground operations. The temporary revisions are normally incorporated in the wiring diagram manual at the next revision, and then becomes a permanent part of the manual. 5. Revision Filing Instructions A. Regular Revision. (Paper version of this manual only.) (1) Refer to the List of Effective pages of each chapter while inserting a revision. (2) Pages changed by the revision will be indicated by the revision date on the page and on the List of Effective pages for that chapter. The revised page replaces the existing page in the manual. (3) New pages added to the manual are indicated by "Added" on the List of Effective pages. Pages are inserted in the manual in sequence by chapter/section/subject and page number. (4) Existing pages no longer needed in the manual are indicated by "Deleted" on the List of Effective pages. These pages are to be removed and discarded. When a page has been deleted by a revision, the List of Effective pages for subsequent revisions does not list the page. B. Temporary Revisions: (Paper version of this manual only.) (1) File temporary revisions in the applicable chapter in accordance with filing instructions that appear on the title page. (2) Temporary revisions should be removed from the manual only when replaced by a revision to the manual or by instructions noted on the superseding temporary revision. 6. RevisIon Indicators A. Additions, deletions or revisions to text in an existing section will be identified by a revision bar in the left margin of the page adjacent to the change. Applicable to the List of Revisions page, Introduction, Chapter 20, and Chapter 91 only. B. When technical changes cause unchanged text to appear on a different page/pages, a revision bar will be placed in the margin opposite the page number of all affected pages. These pages will be updated to the current revision date. Applicable to the List of Revisions page, Introduction, Chapter 20, and Chapter 91 only. INTRODUCTION Page 2 C Cessna Aircraft Company Mar 1/2004 Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 182/182 WIRING DIAGRAM MANUAL C. When extensive technical changes are made to text in an existing section that requires complete retype of copy, revision bars will appear full length of the text. Applicable to the List of Revisions page, Introduction, Chapter 20, and Chapter 91 only. D. Revisions to parts listing pages are identified by an "Ru in the right margin of the text pages. 7. ManuallUsage A. Purpose. (1) This Wiring Diagram Manual has been prepared by Cessna Aircraft Company to assist customer personnel in locating, tracing and repairing of aircraft wiring and components. The wiring diagram manual may also be used to assist in ordering replaceable wiring components and in identifying new and reclaimed parts. It is not approved for any other purpose. B. Effectivity. (1) Due to limited space on the parts list, the effectivity is listed under the title and includes the model number. Effectivity within the top effectivity is listed in a parts column and does not include the model number of a serial. EXAMPLE: 80001 - 80004 would Indicate the part listed Is applicable to serial numbers 18280001 thru 18280004. 8001 - 8004 would indicate the part listed Is applicable to serial numbers T18208001 - T118208004. .1 (2) Airplane effectivity is indicated in the parts list by a ten-character alphanumeric code. The first five characters indicate the first applicability and the last five characters indicate the last applicability on an unbroken sequence of assigned airplanes. When an item is applicable to all airplanes, the column shall be left blank. (3) Avionic configurations are standard avionics package, NAV I option, NAV 1I option, or NAV Ill. Sections of this wiring diagram manual that are unique to a specific avionics configuration are listed as STANDARD, NAV I, NAV II, or NAV Ill. C. Identification Procedures. (1) Wiring Diagram Manual Numbering. (a) Numbering of chapters, sections and subjects within the Wiring Diagram Manual is in accordance with ATA Specification 100. This same numbering system is utilized in the Illustrated Parts Catalog and Maintenance Manual to allow for easy cross- referencing between the three books. Refer to Figure 1 for an example of the numbering system. Chapter (Fuel) Subsystem (Distribution) Specific Diagram (Left Fuel Control) 28-20-01 Wiring Diagram Numbering Figure 1 (2) Wiring Diagram Page Numbering. (a) Page numbers 0 thru 100 are used to number wiring diagrams. Sheet numbers are used for diagrams that require more than one page for illustration. NOTE: Whenever a diagram is referenced to another, only the diagram number is used. Therefore, where there is more than one page of the same diagram, it is necessary to refer to the effectivity block at the top of the parts list to make certain the diagram applies to the airplane of interest. Ccessna Aircraft Company INTRODUCTION Page 3 Mar 1/2004 61984 Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 182/T182 WIRING DIAGRAM MANUAL 0. Wire Identification and Numbering. (1) In each electrical and electronic wiring circuit, the wires are identified by a number-letter code. The code is either printed, stenciled or banded on each wire segment. A wire segment is a run of wire between two points in a circuit. The number-letter code explains where the wire is used. Refer to Figure 2 for the wire identification system. * B P481-P J482 (BILK) Connector Pin Following is lower case Connector Pin Connector (or other component) Color of Wire ~~~~ Connector (or other component) Connector Pin Wiring Diagram Numbering Figure 2 (2) Thermocouple leads are banded for identification and are color coded as shown in Table 1. Table 1. Thermocouple Color Coding Color Coding Red Yellow Wire Material Alumel Chromel E. Parts List. (1) Electrical and electronic equipment used in the wiring diagrams are identified by an alphanumeric reference designator. This reference designator is used as a cross-reference to the parts list where the part number and part description are shown. The five digit Federal Supply Code may be found in the Suppliers Address List to find the suppliers name and address. (2) Most reference designators consists of two (2) alphabetical characters followed by three (3) numeric characters. (a) The first alphabetical character denotes component type. (D Cessna Aircraft Company INTRODUCTION Page 4 Mar 1/2004 B1985 Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 182YT182 WIRING DIAGRAM MANUAL Table 2. First Alphabetical Character A = Splice B = Controller C = Capacitor 0 = Diode E = Instrument F = Light G = Ground H = Circuit Breaker, Fuse, Bus Bar J Connector (Jack, Receptacle) K =Relay L =Inductor M =Servo Motor N =Logic P =Connector (Plug) a = Transistor R = Resistor S = Switch T = Thermal Element U = Unit, Module V =Solenoid Valve W =Solenoid V =Junction Block Z =Cessna Assembly (b) The second alphabetical character denotes general location in the airplane. Table 3. Second Alphabetical Character A = Aft Bulkhead B= ~~~Firewall C = Left Fuselage F = Right Fuselage G = Landing Gear H = Horizontal Stabilizer I= Instrument Panel L =Left Wing INTRODUCTION Page 5 © Cessna Aircraft Company Mar 1/2004 Island Enterprises

CESSNA AIRCRAFT COMPANY MODEL 1821182 WIRING DIAGRAM MANUAL Table 3. Second Alphabetical Character (continued) M = Left Wing Feedthru N = Nose R = Right Wing S = Right Wing Feedthru W =Tailcone V =Vertical stabilizer Z =Inside a Cessna Assembly (c) The three (3) numeric characters are sequentially assigned and do not denote location or order of occurrence. F. List of Chapters. (Paper version of this manual only.) (1) The List of Chapters includes all chapters used in the manual and includes the Aerofiche fiche and frame where each chapter starts. G. Alphabetical Indexes. (Paper version of this manual only.) (1) The Alphabetical Index lists subjects and components in this manual. (2) The Component Index lists each component and its location in the airplane. The components are cross- referenced to the reference designator and applicable chapter, section, subject where the component will be found. H. Reference Designator Index (Paper version of this manual only.) (1) The Reference Designator Index is a complete listing of all parts included in the parts list. All reference designators are cross-referenced to the part number and applicable chapter, section, subject and figure where the reference designator is used. I. Part Number Indexes. (Paper version of this manual only.) (1) The Alpha and Numeric Part Number Indexes are a complete listing of all parts included in the parts list. All part numbers are cross- referenced to the reference designator and applicable chapter, section, subject and figure where the part number is used. J. Chapter 20. (1) Chapter 20 has safety precautions and general maintenance information for wire repairs, grounding of wires, soldering, heat shrink tubing, resistors, torque values and connectors. K. Chapter 91. (1) Chapter 91 has reference information for connectors, ground locations and component locations. (a) Connector charts are provided for those connectors that contain wires for several different systems. The wire number for each wire to a pin is shown with reference to the system where the complete circuit will be found. L. How To Use This Manual. (1) All operable electrical components, such as relays, etc., are shown with the airplane on the ground, all circuits off or de-energized and no electrical power on the circuits. Switches are shown in the off or normal position unless otherwise noted. (2) The parts list may consist of two or more text lines. Make certain that all lines are observed, as the part number and part description are not always complete on the first line. (3) Some wire diagrams have too many parts to list on one page of text. In this case, identical wire diagrams are used with a different parts list for each diagram. INTRODUCTION Page 6 C Cessna Aircraft Company Mar 1/2004 Island Enterprises

Cessna 182S/182T/T182T Aircrafts Electrical Wiring Diagrams Manual

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