CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL

30.00.00 List of Effective Pages 30.00-. 00 Record of Temporary Revisions 30.10.00 Airfoil 30.10.01 Wing and Stabilizer Deice 208 30.10.01 Wing and Stabilizer Deice 2085 30.10.02 Cargo Pod Deice Relay 30.30.00 Pitot and Static 30.30.01 Pitot and Static Heaters 208 30.30.01 Pitot and Static Heaters 2085 30.30.01 Pitot and Static Heaters-French 30.40.00 Windows, Windshields, and Doors 30.40.01 Windshield Anti-Ice 30.60.00 Propellers/Rotors 30.60.01 Propeller Deice (00001-00327, B0001-B0828) 30.60.01 Propeller Deice (00328 On, 80829 On) 30.80.01 Windshield Ice Dect Light (Opt) 31.00.00 Indicating/Recording Systems 31.00.00 List of Effective Pages 31.00.00 Record of Temporary Revisions 04/12/2007 Copyright Aircraft Technical Publishers Page 4 of 8 CS 2614 WD Section Topic 31.20.00 Independent Instruments 31.20.01 Electric Clock 31.30.00 Recorders 31.30.01 Hourmeter 31.50.00 Central Warning Systems 31.50.01 Annunciator Panel 31.50.02 Annuciator Panel Assembly (00001-00145, 80001-80179) 31.50.02 Annuciator Panel Assembly (00146-00240, B0180´•80417) 31.50.02 Annuciator Panel Assembly (00241 On, 30418 On) 31.50.03 Emergency Power Lever Warning 31.50.04 Chip Detectors 31.50.05 Beta Mode Warning 32.00.00 Landing Gear 32.00.00 List of Effective Pages 32.00.00 Record of Temporary Revisions 32.30.00 Extension and Retraction 32.30.01 Landing Gear-Amphibian 33.00.00 Lights 33.00.00 List of Effective Pages 33.00.00 Record of Temporary Revisions 33.10.00 Flight Compartment 33.10.01 Dimmable Panel Lights 33.10.01 Dimmable Panel Lights-French 33.10.01 Dimmable Panel Lights-British 33.10.02 Map Light 33.10.03 Ice Detector Light 33.20.00 Passenger Compartment 33.20.01 Cabin Lights 208 33.20.01 Cabin Lights 2088 33.20.01 Cabin Lights with Timer 208 33.20.01 Cabin Lights with Timer 2088 33.20.02 Reading Lights 208 33.20.02 Reading Lights 208B 33.20.03 Courtesy Lights 33.20.04 Seat Belt/No Smoking Sign 33.20.05 Jump Lights 33.20.06 Exit Sign-Chinese 33.40.00 Exterior 33.40.01 Landing and Taxi Lights 04/12/2007 Copyright Aircraft Technical Publishers Page 5 of 8 CS 2614 WD) Section Topic 33.40.02 Navigation and Strobe Lights 33.40.03 Flashing Beacon Light 34,00.00 Navigation 34.00.00 List of Effective Pages 34.00.00 Record of Temporary Revisions 34.10.00 Flight Environment Data 34.10.01 Airspeed Warning 34.10.02 Airspeed Warning Alarm Assy (00001-00131, 80001-80091) 34.10.02 Airspeed Warning Alarm Assy (00132 On, 80092 On) 34.10.03 Airspeed Switch (00212-00217, 80294-80306) 34.10.04 Low Airspeed Warning, Icing (Opt) (0382-0403,81088-B121) 34.10.04 Low Airspeed Warning, Icing (Opt) (0404 On,B1211 On) 34.20.00 Attitude and Direction 34.20.01 Turn Bank and Turn Coordinator Indicators 34.20.02 Attitude and Directional Gyros 34.20.02 Directional Gyro-Left 208 (00146 On) 34.20.03 Directional Gyro´•Left 208 (00146 On) 37.00.00 Vacuum 37.00.00 List of Effective Pages 37.00.00 Record of Temporary Revisions 37.20.00 Indicating 37.20.01 Low Vacuum Warning Structures 52.00.00 Doors 52.00.00 List of Effective Pages 52.00.00 Record of Temporary Revisions 52.10.00 Passenger/Crew 52.10.01 In-Flight Moveable Door 52.70.00 Door Warning 52.70.01 Door Unlocked Warning Propeller/Rotor 61.00.00 Propellers/Propulsors 61.00.00 List of Effective Pages 61.00.00 Record of Temporary Revisions 61.40.00 Indicating 04/12/2007 Copyright Aircraft Technical Publishers Page 6 of 8 CS 2614 WD Section Topic 61.40.01 Propeller Overspeed Test Power Plant 73.00.00 Engine Fuel and Control 73.00.00 List of Effective Pages 73.00.00 Record of Temporary Revisions 73.10.00 Distribution 73.10.01 Fuel Control Heater 73.30.00 Indicating 73.30.01 Fuel Flow 74.00.00 Ignition 74.00.00 List of Effective Pages 74.00.00 Record of Temporary Revisions 74.30.00 Switching 74.30.01 Ignition 77.00.00 Engine Indicating 77.00.00 List of Effective Pages 77.00.00 Record of Temporary Revisions 77.10.00 Power 77.10.01 Propeller Speed 77.10.02 Gas Generator Speed 77.10.03 Electric Torque Indicator 77.20.00 Temperature 77.20.01 Inter Turbine Temperature Indicator 77.30.01 Altair Etm (0382 On, 31087 On) 79.00.00 Oil 79.00.00 List of Effective Pages 79.00.00 Record of Temporary Revisions 79.30.00 Indicating 79.30.01 Low Oil Pressure Warning 79.30.02 Oil Temperature Indicator 91.00.00 Charts 91.00.00 List of Effective Pages 91.00.00 Record of Temporary Revisions 91.10.01 Connector Charts 04/12/2007 Copyright Aircraft Technical Publishers Page 7 of 8 CS 2614 WD Section Topic End of Index 04/12/2007 Copyright Aircraft Technical Publishers Page 8 of 8 CS 2614 WD) IVI FGI INTRO II cessna ATextronComDanv A Textron Wiring Diagram Manual MODEL 208 SERIES CARAVAN Member of GAMA COPYRIGM. 01995 II AUGUST 1 995 CESSNA AIRCRAFT COMPANY WICHITA,KANSAS,USA 02079-7-13 REVISION 7 1 JANUARY 2007 RECORD OF REVISIONS MFG REV NO DESCRIPTION ISSUEDATE ATPREVDATE INSERTEDBY 6 See Highlights 3/1/2001 ATP/J B 7 See Highlights 1/1/07 4/18/07 ATP/GM 4/11/2007 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL RECORD OF REVISIONS REVISION DATE DATE PAGE REVISION DATE DATE PAGE NUMBER INSERTED REMOVED NUMBER NUMBER INSERTED REMOVED NUMBER CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL LIST OF REVISIONS 1. Effectivity A. The configuration of each airplane is tailored to the request of the customer. This Wiring Diagram Manual covers airplanes 20800001 and On; and airplanes 20880001 and On. NOTE: Information in this Wiring Diagram Manual is applicable to U.S. and Foreign Certified Model 208 Series airplanes. 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 into the manual as they are issued Original Issue-i August 1995 Revision 1-1May1996 Revision 2 -2 December 1996 Revision 3 -1 September 1998 Revision 4 15 October 1999 Revision 5 1 September 2000 Revision 6 -1 March 2001 Revision 7 1 January 2007 LIST OF REVISIONS Page 1 0 Cessna Aircraft Company Jan 1/2007 RECORD OF TEMPORARY REVISIONS TEMP ATP REV INSERT DATE REV REMOVE REV NO DESCRIPTION ISSUE DATE DATE BY REMOVED INCOR BY 8/18/2005 REVISION MODEL 208 SERIES CARAVAN I VVIRING DIAGRAM MAN UAL REVISION 7 1 JAN UARY 2007 D2079-7-13 This revision consists of the original manual dated 1 AUGUST 1995 and incorporates REVISION 1 thru 7. This revision replaces the existing manual in its entirety. CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL CHAPTER NUMBER SECTION OF SUBJECT PAGES DATE Title 1 Jan 1/2007 Record of Revisions 1 Introduction-list of Effective Pages 1 Jan 1/2007 List of Revisions 1 Jan 1/2007 Introduction 19 Sep 1/2000 Zone Numbering System 5 Oct 15/1999 Service Kit List 1 Jan 1/2007 Light Bulb Replacement Guide 2 Oct 15/1999 Fuse Replacement Guide 2 Oct 15/1999 Suppliers Publication 2 Sep 1/2000 Suppliers Address List 5 Sep 1/2000 List of Chapters 1 Jan 1/2007 Alphabetical Index 4 Jan 1/2007 Component Index 19 Jan 1/2007 Reference Designator Index 45 Jan 1/2007 Part Number Index 24 Jan 1/2007 INTRODUCTION- EFFECTIVITIES Page 1 0 Cessna Aircraft company Jan 1/2007 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL INTRODUCTION i. Coverage A. The Wiring Diagram Manual 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, Supplier Service Notices, Publication Changes, Revisions, Reissues and Temporary Revisions. All such amendments become part of and are specifically incorporated within this publication. Users are urged to keep abreast of the latest amendments to this publication through information available at Cessna Authorized Service Stations or through the Cessna Product Support subscription services. Cessna Service Stations have also been supplied with a group of supplier publications which provide disassembly, overhaul, and parts breakdowns for some of the various supplier equipment items. Suppliers publications are updated, supplemented, and specifically amended by supplier issued revisions and service information which may be reissued by Cessna thereby automatically amending this publication and are communicated to the field through Cessna’s Authorized Service Stations andlor 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, PURCHASED, 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 ANDIOR SELLER OF SUCH NON-CESSNA PARTS. C. This manual has been prepared to assist maintenance personnel in maintaining Model 208 airplanes. This manual provides the necessary information required to enable the mechanic to troubleshoot, remove and replace components or repair systems. NOTE: This manual has been prepared in both paper and CD-ROM versions. For CD-ROM version, refer to the CD-ROM introduction for information about items marked as (Paper version of this manual- only.). D. Information.beyond the scope of this manual may be found in the Maintenance Manual, Illustrated Parts Catalog, Structural Repair Manual and Avionics Manual. For technical assistance concerning this manual, contact Cessna Aircraft Company, Propeller Aircraft Product Support. E. Technical Publications available from the manufacturer of the various components and systems which are not covered in this manual must be utilized as required for maintenance of those components. INTRODUCTION Page 1 0 Cessna AircraA Company Sep 1/2000 CESSNA AIRCRAFT COMPANY NIODEL 208 WIRING DIAGRAM MANUAL 2. 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. A revised list of effective pages is provided for each chapter that changes with every regular wiring diagram manual revision. 3. Temporary Revision 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 regularly scheduled revision, and then becomes a permanent part of the man ual. 4. Revision Filing Instructions (Paper version of this manual only.) A. Regular Revision. (1) Refer to the List of Effective pages of each chapter while inserting a revision. (2) Figures changed by the revision will be indicated by the revision date on the pages and on the List of Effective pages for that chapter. The revised figure replaces the existing figure in the manual. (3) New figures added to the manual are indicated by "Added" on the List of Effective pages. Pages for the figure are inserted in the manual in sequence by chapter, section, subject, figure and page number. (4) Existing figures no longer needed in the manual are indicated by "Deleted" on the List of Effective pages. The pages that make up these figures are to be removed and discarded. When a figure has been deleted by a revision, the List of Effective pages for subsequent revisions does not list the figure. B. Temporary Revisions: (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. 5. Revision Bars 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. 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 providing no other revision bar appears on the page. These pages will be updated to current regular revision date. 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. D. When art in an existing diagram is revised, a pointing hand will appear in the diagram pointing to the area of revision. E. New art added to an existing section will be identified by a single pointing hand adjacent to the diagram title. F Revisions to parts listing pages are identified by an "R" in the right margin of the text pages. INTRODUCTIOPI Page 2 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL 1. Manual Usage A. Purpose. (1) The 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. Ef~ectivity. (1) Airplane effectivity is indicated in the parts list by a ten-character alphameric 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 covered by the Wiring Diagram Manual, the column shall be left blank. C. Identification Procedures. (1) Wiring Diagram Numbering. I (a) Wiring diagram numbering is in accordance with ATA Specification 100. On the Model 208 Series wiring diagrams, this number is shown as three sets of two numbers. Refer to Figure 1 for an example of wiring diagram numbering. (2) Wiring Diagram Page Numbering. (a) The page numbers 1 to 100 are used to number wiring diagrams. Sheet numbers will be used in the title block 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 to make certain the diagram applies to the airplane of interest. A2a)5 Chapter/System -~-----------28-2!-01 Subject/Unit (Fuel) (Fuel Boost Pump) Section/Subsystem (Distribution) Wiring Diagram Numberng Figure 1 D. 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 Table 2 for the wire identification system. (2) Thermocouple leads are banded for identification and are color coded as shown in Table 1. Table 1. Color Coding for Thermocouple Leads Color Coding Wire Material Green Tracer Alumel White Chromel INTRODUCTION Page 3 0 Cessna Aircraff Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL Table 1. Color Coding for Thermocouple Leads (continued) Color Coding Wire Material Yellow Constantan Red Copper Black Iron INTRODUCTION Page 4 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL Table 2. Circuit Function and Specific Circuit Code Letters A Armament H Heating, Air Conditioning, Q Fuel And Oil Ventilating and Deicing QA- Auxiliary fuel pump B-Photographic HA-Anti-icing OS-Oil Dilution HE Cabin Heater QC Engine Primer C Control Surface HC Cigar Lighter QD Main Fuel Pumps CA -Automatic Pilot HD Deice QE Fuel Valves CC Wing Flaps HE Air Conditioners CD Elevator Trim HF Cabin Ventilation R Radio RA Instrument Landing D Instrument (Other Than Flight J Ignition RE Command or Engine Instrument) JA Magneto RC Radio Direction Finding DA-Ammeter RD-VHF DB Flap Position Indicator K Engine Control RE Homing DC Clock KA Starter Control RF Marker Beacon DD-Voltmeter RG-Navigation DE Outside Air Temperature KB Propeller Synchronizer RH High Frequency DF Flight Hour Meter KC Inertial Air Separator RJ Interphone RK-UHF E-Engine Instrument L-Lighting RL Low Frequency EA Carburetor Air LA Cabin RM Frequency Modulation Temperature La instrument RP Audio System and Audio EB Fuel Quantity Gage LC Landing Amplifier and Transmitter LD Navigation RR Distance Measuring EC Cylinder Head LE Taxi Equipment (DME) Temperature LF Rotating Beacon RS -Airborne Public Address ED-Oil Pressure LG-Radio System EF-Fuel PressureEE-OilTemperature LH-Deice LJ-Fuel Selector S-Radar EG -Tachometer LK-Tail Flood Light EH Torque Meter LL Recognition Light U Miscellaneous Electronic EJ Instrument Cluster US identification Friend or EK-Turbine Inlet Temperature Foe EL-Fuel Flow M-Miscellaneous MA Cowl Flaps W Warning And Emergency WA Flare Release F-Flight Instrument FA Bank and Turn MB Electronically Operated WE Chip Detector FB Pitot Static Tube Heater Seats WC Fire Detection System and Stall Warning Heater MC Smoke Generator WD Low Fuel Level FC Stall Warning MD Spray Equipment WE Vacuum Warning System FD Speed Control System ME Cabin Pressurization WF Annunciator FE Indicator Lights Equipment WG Battery MF Chem Oxygen Indicator WH Emergency Power G Landing Gear Light VVJ Low Voltage GA -Actuator MG -Vacuum Pump WK Unlocked Door GB-Retraction GC -Warning Device (Horn) P D.C. Power X A.C. Power GD Limit Switches PA Battery Circuit GE Indicator Lights PB Generator Circuit PC External Power Source PH Anti-ice Power Source INTRODUCTION Page 5 0 Cessna Aircraff Company Sep 112000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL E. Equipment List. (1) All the electrical and electronic equipment used in the wiring diagrams are identified by an alpha- numeric reference designator. This reference designator is used as a cross-reference symbol to the equipment list where the part number and part description are shown. The five digit Federal Supply Code may be found in the Introduction to this manual or in the introduction to the Model 208 Illustrated Parts Catalog to provide a suppliers name and address. (a) Reference designators in this manual were added for convenience in using this manual. Electrical equipment in the airplane may or may not have reference designators. Refer to Table 3 for categories assigned to the basic equipment designator letters: Table 3. Equipment Designators A Ammeters AD Warning Horns ALT Alternator BATT Batteries C Capacitor CB Circuit Breaker CU Control Units D Diodes F Fuse FL Flasher H Heaters HS Heat Sink IC Integrated Circuit IND Indicators J Receptacles K Relays L Lights M Motors P Plugs Q Transistor or Darlington R Resistor S Switch SG Starter/Generator SH Shunt SL Solenoid SPKR Speaker or Warning Horn T r~mer TB Terminal Board XMTR Transmitter INTRODUCTION Page 6 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL 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. (2) The first frame(s) on each fiche has the list of chapters for location of all chapters. G. Alphabetical Index. (Paper version of this manual only.) (1) The Alphabetical Index lists all wiring diagrams in the manual. H. Reference Designator Index (1) The Reference Designator Index is a listing of all reference designators included in the parts list. All reference designators are cross referenced to the reference designator and applicable chapter, section, subject and figure where the reference designator is used. (2) Component locations are provided for most reference designators. Components that are part of another assembly, such as a diode on a circuit board, do not have a location listed. I. Part Number Index. (Paper version of this manual only.) I figure where the part number isused.are cross-referenced to the reference designator and applicable chapter, section, subject and (1) The Part Number Index is a complete listing of all parts included in the parts list. All part numbers J. Chapter 20. (1) Chapter 20 has safety precautions. I (3) included in chapter 20. (2) General maintenance information for: wire repairs, grounding of wires, soldering, heat shrink tubing, resistors, torque values, connectors and conformal coating for printed circuit boards, are Information on connectors includes: removal and installation of contacts, contact pin and socket part numbers, tools to crimp the contacts, sealing of potted type connectors and the contact arrangements, Are included in chapter 20. K. Chapter 91. (1) Chapter 91 has reference information for: connectors and component location. I (a) Connector charts are provided for those connectors that contain wires for several different systems, such as pressure bulkhead connectors. All contact pins are shown for the complete connector. The wire number for each wire to a pin is shown with reference to the system where the complete circuit will be found. (Connector maintenance practices in 20-10-04 have insert arrangement charts for connectors.) 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 Equipment List may consist of more than one line of information for a component. Make certain that all lines are observed. (a) A part number or part description may require more than one line. (b) Serial effectivity May require more than one line. (c) Special qualifying conditions, such as incorporation of-a service bulletin, are listed after the component. (d) Alternate part numbers may be listed after a component. (e) Attaching parts, such as a backshell for a connector are listed after a component. attaching parts are indented for identification. (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. I (a) Identical wire diagrams will have the same figure and sheet number, to help identify duplicate wire diagrams, although page numbers will increment. INTRODUCTION Page 7 0 Cessna Aircraff Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL I (4) Where applicable, this manual includes part numbers, zone information, supplier information,occurs.serial effectivity, qualifying conditions, alternate part numbers and attaching parts information for all components assigned a reference designator. (a) All information for a component is provided on each parts page in which the component (5) Letters or numbers are used to identify the contacts of a connector to which each wire is connected. (a) The letter or number shown on the wiring diagram is also marked on the connector. (b) A letter that is underlined indicates a lower case letter. On wiring diagrams: the letter may be printed in either lower case or capital letters, but both indicate lower case on the connector. 7. Symbols A. Refer to Figure 2 for examples of symbols used in this wiring diagram manual. 8. Manufacturer’s Names and Addresses A. Refer to the supplier list pages for manufacturer’s names and addresses. 9. Service KitslService Bulletins A. A record of Service kits/Service bulletins prepared for the Model 208 Series airplane is listed on the service kit/service bulletin pages. B. The list of service kits/service bulletins utilize five columns to summarize the information. (1) Service Kit Number The service kit number column identifies the service kit by number. Service kits are numbered consecutively starting with number one. (2) Title The title column identifies the service kit by nomenclature. It is the same title displayed on page one of the service kit. by number, that corresponds to the service kit. Service bulletins are numbered consecutively (3) Service Bulletin Number The service bulletin number column identifies the service bulletin starting with number one. (4) Service Kit Date The service kit date column indicates the date the service kit displays. (5) Manual Incorporation Date The manual incorporation date column will indicate the status of the service kit. (a) Date This indicates when the service kit information was incorporated into the manual. (b) No Effect If "No Effecr’ appears in the column, this indicates the service kit does not affect the manual. (c) Other self-explanatory statements may appear in this column (i.e., replaces, replaced, superseded, etc.). INTRODUCTION Page 8 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3944 BATTERY +-11111; BUS CAP AND STOW CAPACITOR CIRCUIT BREAKER --6-~- The switch contacts connect to an annunciator system to warn when a circuit breaker is open. T- -II 28V CURRErilTLh ’rbc~-"" Remote circuit breakers combine the functions SENSOR ’1 A21 of circuit breaker and relay. A 1 amp or 0.5 amp circuit breaker is used at pilot’s circuit breaker panel to indicate an overload and can be opened LOGIC by the pilot to disable the system. Remote circuit breakers have a visual indicator to the right of the L connector. OPEN and CLOSED labels on red and green backgrounds indicate the position of ~6blll relay contacts. CONTROL SWITCH (RELAY) Electrical Symbols Figure 2 (Sheet i) INTRODUCTION Page 9 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRATT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3945 CONNECTOR The black circle indicates contact will accept 10 gage wire. A blade triangle indicates contact will accept 12 gage wire. Unmarked contacts accept 20 gage wire. CURRENT SENSOR Current flowing in coil opens switch to indicate circuit is functioning correctly. CURRENT TRANSFORMER Current flowing in wire produces a voltage in coil. DIODE Regular Low resistance forward, high resistance reverse. I--~-- Zener Low resistance foward, high resistance reverse until a specific voltage is applied, then conducts freely. --dt Transzorb A transzorb is similar to a zener, but with higher peak current limit. Varistor High resistance either way until a specific voltage is applied, then conducts freely. Example: V47ZA1 conducts freely above 47 volts. I ~h I ILI varistor Encapsulated for moisture protection. FILTER dmb Passes direct current but opposes pulsating current; used to reduce noise in sensitive avionics equipment. FUSE/LIMITER GROUND -~II Electrical Symbols Figure 2 (Sheet 2) INTRODUCTIOPI Page 10 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL w~ HEADSET bb HEATER -rll~Lr HORN/SPEAKER \NTEGRETED C\RCU\T integrated circuits do not necessarily work on the principle of ON-OFF as a switch, instead some work on high and low voltage. Example: high might be 5.0 volts and low might be 0.5 volts. =f>- AND GATE Output is low until both inputs are high, then the output is high. IN OUT then the output islow.NANDGATE Output is high until both inputs are high, IN OUT OR GATE Output is low until either or both inputs are high, then output is high. IN OUT then output islow.NORGATE Output is high until either or both inputs are high, IN OUT --i~ when input islow.INVERTER Output is low when input is high, output is high IN OUT OPERATIONAL AMPLIFIER (OP AMP) Amplifies the differences in voltage between the two inputs. The minus input is the in- IN OUT verting input and the plus is the noninverting input. If an input is applied to the minus input, with the plus input grounded, the polarity of the output will be opposite to the input. If an input is applied to the plus input, with the minus input grounded, the polarity of the output will be the same as that of the input. TIMER Changes the output from high to low in a regular pattern. Electrical Symbols Figure 2 (Sheet 3) INTRODUCTION Page 11 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3949 LAMP -tf~ MOTOR BBSiCSymb011olmOmr RED ~MOT) Reversible Motor Direction of rotation is controlled ~L-BLK-- by ’eversing power and ground on input wires. CW II Reversible Motor Direction of rotation is controlled by applying power to either field winding input wire. CCW Nonreversible Motor- Direction of rotation is controlled MOT by design; input wires may be connected either way. power to either inputwire.NonreversibleMotor Two-speed controlled by applying Electrical Symbols Figure 2 (Sheet 4) INTRODUCTION Page 12 0 Cessna AircraA Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208’ WIRING DIAGRAM MANUAL PHONE JACK RELAY The symbol for the solenoid may be a box or a coil, the operation is identical c I I~31+II CURRENT FLOW CURRENT FLOW THE WITH POWER APPLIED INSTANT POWER IS REMOVED I =b A diode is connected across the input wires of relays and solenoid operated devices, such as valves, to protect voltage sensitive navigation and electronic equipment. The diode is reverse-biased for normal power and no current flows through the diode. Current flowing through the coil of wire produces a magnetic field to operate the relay or valve. The I ~II instant power is removed from the coil, the collapsing magnetic field produces a momentary spike of high voltage which can be several hundred volts depending on the current and the number of turns of wire in the coil. The diode is forward-biased for the power generated in the coil and the high voltage spike is dissipated through the diode. A varistor J is used in place of the diode on some relays. ANNUNCIATOR 28VDC ~LOAD An annunciator relay has a connection on the J moveable contact to indicate by a light or annunciator panel when the relay is energized. Electrical Symbols Figure 2 (Sheet 5) INTRODUCTION Page 13 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3963 The contacts of a time delay do not move to the ~>-(t energized position instantly when power is applied. I TIMF 1 For some time delay relays, the delay time is part of design of the relay. For some time delay relays, the delay time is controlled by the size of an external resistor. 1 Jumper wire gives 0.1 second delay. 160,000 OHM resistor gives 10-second delay. O~- Other resistors give delay time between 0.1 second and 10 seconds. B TIME A UCTERNAL DELAY RESISTOR RESISTOR REGULAR resistance does not change. TEMPERATURE CONTROLLED resistance changes with the temperature. VARIABLE OR ADJUSTABLE resistance changes with mechanical input. d~14, RHEOSTAT Type of variable resistor with two wires. three wires.POTENTIOMETER Type of variable resistor with Electrical Symbols Figure 2 (Sheet 6) INTRODUCTION Page 14 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3954 SOLENOID/SOLENOID VALVE NO (normally open) or NC (normally closed) by a solenoid operated valve indicates the position of the valve with no power applied to the solenoid. CLOSED BI CLOSE BI CLOSE D CLOSED MOTOR M~GI MOTOR FI ANNUNCIATOR (MOTOR ON) Al OPEN CI OPENED Al OPEN SHOWN OPEN I D OPENED SHOWN OPEN MOTOR OPERATED LIMIT SWITCHES STOP POWER WHEN LIMIT OF TRAVEL IS REACHED. SHUNT SPLICE This symbol with no sp reference designator is --I=7C a premanent splice; when identified with an sp reference designator, it is an environmental disconnect splice. ENVI RONMENTAL DISCONNECT -IE3C: ENVIRONMENTAL Electrical Symbols Figure 2 (Sheet 7) INTRODUCTION Page 15 0 Cessna Aircraff Company Sep 112000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3941 SWITCH SINGLE POLEISINGLE THROW (SPST) --´•0~- SINGLE POLE/DOUBLE THROW (SPDT) c~- may have OFF position in the center. DOUBLE POLUDOUBLE THROW (DPDT) O- may have OFF position in the center. Dashed line indicates all parts move simultaneously. 00O 4k O ROTARY OR MULTI POSITION 000 TWO POLE ROTARY On rotary or multipole switches controlled by a knob, the poles o o 0 (or decks) are indentified on wiring diagrams 14, O or shaftend.asA, B, C, with A being the part on the knob Lc’ DDD EEE CCC KKK ABC CICIC II 1111 II FT10 21 21 2 GRAYHILL 31 31 3 SIDE VIEW WITH TYPICAL TERMINAL NUMBERING REAR VIEW C Common terminals for each deck 1 thru In Switch Terminals Position EXAMPLE: AC Common terminals on deck A B1 Switch position 1 on deck B Electrical Symbols Figure 2 (Sheet 8) INTRODUCTION Page 16 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3946 O 1NO TWO STAGE Two pole, four pole or six pole switch designed le Oa 1NC so that all moveable switch contacts do not move simultaneously. OP 2NC OPPOS ITE O 2NO ´•I CENTER ~k 2 POLE TO FLAT 1NO1NC Handle position is referenced to the flat 2NO2NC side of the mounting threads. o~-p 3NC O 3NO NOTE: Some switches of this type do not have a center position. 4NC O 4NO TO FLAT CENTER" OPPOSITE 4 POLE NO NO I NO CONTACT 1 OF 2 POLE C O O’b O CONTACTS 1 AND 2 OF 4 POLE CONTACTS 1, 2 AND 3 1NO OF 6 POLE I NC I NC I NC 1NC NC NC NC CONTACT 2 OF 2 POLE (O 2NO CONTACTS 3 AND 4 OF 2NC CONTACTS 4, 5 AND 6O 6d94 POLE O 3NC3NO OF 6 POLE NO NO NO 4NC C IS THE COMMON TERMINAL NC IS THE NORMALLY CLOSED TERMINAL IO 4No NO IS THE NORMALLY OPEN TERMINAL 5C~4 5NC lo 5NO 6NC O 6NO 6 POLE Electrical Symbols Figure 2 (Sheet 9) INTRODUCTION Page 17 0 Cessna Aircraff Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3948 0- PRESSURE OPERATED TEMPERATURE OPERATED TERMINAL STRIP lo o ol TRANSFORMER Electrical Symbols Figure 2 (Sheet 10) INTRODUCTION Page 18 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A3~m TRANSISTOR Transistor contacts are identified as base, collector C and emitter. Flow of current through a transistor is controlled by the signal applied to the base. The control current (3 to 5 percent of total current) flows between base and emitter. The main flow of current (95 to 97 percent) is between collector and emitter. E Transistors may be drawn without the circle. NPN COLLECTOR CE ~-I=EMITTER MAIN BASE CURRENT FLOW PNP CONTROL SIGNAL DARLINGTON WIRE nn/lSTED SHIELDED -H- -ce Q12A20 HIGH TEMPERATUREWIRE Electrical Symbols Figure 2 (Sheet 11) INTRODUCTION Page 19 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COWIPANY MODEL 208 WIRING DIAGRAM MANUAL ZONE NUMBERING SYSTEM i. Zone Numbering System A. General (1) The Model 208 is divided into numbered zones to provide a method for locating components. The zones are identified by a three- digit number. Each digit designates a zone category: major, sub-major or subdivision. Refer to Figure 1. (2) Major Zones 100 FS 100.0 forward side of firewall and forward. 200 FS 100.0 aft side of firewall to FS308.00 (208), FS356.00 (2088). 300 FS 308.00 (208), FS 356.00 (2088) to end of airplane 400 Nacelle area forward of firewall. 500 Left wing 600 Right wing 700 Landing gear. 800 Cabin and cargo doors. 900 Cargo pod (if applicable). A3055 EXAMPLE 311 u$arzone-------l SJadvieanzane Submajor Zone Zoning Diagram Description Figure 1 (3) Submajor Zones. The second digit of the three-digit number designates a further delineation of a particular area of the major zone, i.e., zone 217, which indicates either side of the cockpit below the cockpit floor. (4) Subdivision Zones. The third digit of the three-digit number designates a further breakdown of a submajor zone. i.e., upper or lower or left or right, in order to designate a reasonably small area to facilitate location of components. Zone 217 therefore indicates the cockpit, below the cockpit floor on the left side. B. How to Find a Component Using the Zones (1) Identify the component reference designator on the wiring diagram of the particular figure. (2) Refer to the text portion of the figure and locate the reference designator. Read across to the nomenclature. The zone for that particular component is located in the nomenclature portion of the figure. (3) After locating the zone, refer to Figure 2 to locate the component in the airplane. ZONE NUMBERING SYSTEM Page 1 0 Cessna Aircraft Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A22945 231 251 255 215 (232) (252) (256) 311 211 (21 6) (312) (212) e~ 330 320 130 213 217 233 801 253 257 803 (21 4) (218) (234) (802) (254) (258) (804) 208 FUSELAGE ZONES 231 251 255 215 (232) (252) (256) 311 211 (216) (312) (212) n 330 320 130 213 217 233 801 253 257 803 (214) (218) (234) (802) (254) (258) (804) 2088 FUSELAGE ZONES 240 243 242 122 244 i:__ 121 241 2610XM03 2610X3M)3 2610X3Mn Airplane Zones Figure 2 (Sheet 1) ZONE NUMBERING SYSTEM Page 2 0 Cessna Aircraft Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A22945 341 TRIM TAB 371 (372) 343 340 STABILIZER 373 (374) ELNATOR 375 (376) 208 AND 2088 HORIZONTAL STABILIZER 208 AND 2088 EMPENNAGE 511 (611) 501 wS35.0 I WSss.o (601) WS 155.9 WS 2!4.3 503 523 (603) (623) WS 308.0 O O Oo i o d I ~Ci;´• O 0 O 0\0 O O O O I O 0_0~ 575 (675) 525 527 521 WS228.0 551 571 (625) (627) (621) (651) (571) 208 AND 2088 LEFT AND RIGHT WING ZONES 2810X1W9 2610X1011 261MM)8 Airplane Zones Figure 2 (Sheet 2) ZONE NUMBERING SYSTEM Page 3 0 Cessna Aircraff Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAFA MANUAL A2294f 803 (804) 531 801 (631) (802) .9 701 907 Q 905 (908) 921 922 903 923 (906) 721 901 (904) (722) (902) 209 CARGO POD, DOORS AND LANDING GEAR 531 803 801 (631)~ 1 ~804) (802) 907 701’ -f I J~O 905 (908) 924 (906) 901 921 922 923 903 721 (902) (904) (722) 208B CARGO POD, DOORS AND LANDING GEAR 152 151 m PI~ ,-1- ~D, .D :I ii -~t---*C-----IIIC4-5 :I Il /I j´• II 18 ,-i i (PBI~ I ,i T’ a~8 ’I II ii ´•i´• J1‘~\ I .CI1 I I i g ~u o i og ii ii 26102005 2~101001 FORWARD SIDE OF FIFIEWALL (FS 100.00) 26133007 Figure 2 (Sheet 3) Airplane Zones ZONE NUMBERING SYSfEM Page 4 0 Cessna Aircraff Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL A22339 227 222 223 228 221 220 224 B 8’ 0’ O I~j qJ O L_J eee~;] g 13 .8. ~bdo 0. 226 INSTRUMENT PANEL AND CENTER PEDESTAL 201 202 203 204 FIREWALL LOOKING FORWARD 261881014 28182015 2613)(3007 Airplane Zones Figure 2 (Sheet 4) ZONE NUMBERI~G SYSTEM Page 5 0 Cessna Aircran Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL SERVICE BULLETIN LIST 1. General A. Refer to the Model 208 Illustrated Parts Catalog for the current Model 208 Service Bulletin List. SERVICE BULLETIN LIST Page 1 0 Cessna Aircraft Company Jan 1/2007 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL LIGHT BULB REPLACEMENT GUIDE 1. Light Bulb Replacement Guide A. The following table may be used for light bulb replacement. The reference designator identifies the light on it’s associated wire diagram. For lights that have no reference designator, the column is left blank. REFERENCE DESIGNA- AIRPLANE BULB LIGHT TOR ZONE QUANTITY BULB PART NUMBER EXTERIOR Anti-collision, Right L37 575 01 040-0043 Beacon (Flashing) L38 340 01 C17312-1 Courtesy, Left L26 511 01 MS15584-15 Courtesy, Right L27 611 01 MS?5584-15 Ice Detect L21 231 01 A7079824 Landing, Left L32 503 01 4553 Landing, Right L33 603 01 4553 Navigation, Left Wing L36 675 01 1\l1S25309-7512 Navigation, Right Wing L37 575 01 1\11825309-7512 Navigation, Tail L35 330 01 C622001 Taxi, Left L31 503 01 4646 Taxi, Right L34 603 01 4646 INTERIOR (CABIN) Jump Light (Amber) L29 255 01 1\11825231-313 Jump Light (Green) L30 255 01 1\11825231-313 Jump Light (Red) L28 255 01 MS25231-313 Passenger Reading L25 08 1495 (20800001- 00207) Passenger Reading L25 08 1308 (20800208 8 On) Passenger Reading (2088 L25 08 1308 Passenger Airplanes) Post Light, Primary L43 211 7 MS25327-328 Operators Console Post Light, Secondary L45 256 1 1\11825327-328 Operators Console Reading Light, Primary L44 211 1 1385 Operators Console Reading Light, Secondary L46 211 1 1385 Operators Console INTERIOR (FLIGHT COMPARTMENT) LIGHT BULB REPLACEMENT GUIDE Page 1 0 Cessna Aircraft Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE DESIGNA- AIRPLANE BULB LIGHT TOR ZONE QUANTITY BULB PART NUMBER Annunciator Panel CU1 221 46 N1825237-327 Annunciator Panel, CU1 221 02 1\11825237-8918 Ignition On Anti-collision, Left L36 675 01 040-0043 Circuit Breaker Panel On L8 220 01 1820 Glareshield Circuit Breaker Panel L8 220 01 1\11825231-313 Under Instrument Panel Compass L4 221 1 1\11825237-327 Dome Light, Cabin 118 251/252 01 N1835478-307 (Second Forward) Dome Light, Cargo Door L24 255 01 1\/1835478-307 Dome Light, Forward L22 251 01 1~1S35478-307 Cabin Dome Light, Passenger L23 256 01 1\11835478-307 Door Engine Instruments L3 221 08 MS25237-327 Engine Instruments L17 221 01 MS25237-327 (French Airplanes) Flood, Leff L13 231 02 1308 Flood, Right L9 232 02 1308 Left Instrument Panel L2 220 01 MS25237-327 (Fixed) Left Instrument Panel L1 222 01 1\11825237-327 (Removable) Movable Door In Transit L40 223 1 1\11825237-327 OAT Gauge L14 231 1 MS25237-327 Overhead Panel L10 231/232 01 MS25237-327 Overhead Panel L12 231/232 2 MS25237-327 Pedestal L6 226 02 MS25231-1819 Pedestal Flood Light L11 231/232 02 1308 Pilots Map L20 227 01 24RB Pilots Switch Panel L7 220 01 N1825237-327 Right Digital Clock L19 224 01 1\/1825231-1819 Right Instrument Panel L15 224 01 1\11825237-327 Switch Panel L5 220 01 MS25237-327 Vacuum, Low L39 224 01 CM6839 LIGHT BULB REPLACEMENT GUIDE Page 2 0 Cessna Aircraft Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL FUSE REPLACEMENT GUIDE 1. Fuse Replacement Guide A. The following table may be used for fuse and fuse limiter replacement. The reference designator identifies the fuse on its associated wire diagram. AIRPLANE PART NAME CIRCUIT LOCATION ZONE NUMBER F1´• Circuit Breaker Electric Power Box 121 ANL40 Panel F14 Standby Alternator Power Box 121 275005 Alternator Shunt Alternate 276005 F15 Standby Alternator Power Box 121 275005 Alternator Shunt Altemate 276005 F16 Standby Alternator Power Box 121 275005 Alternator Shunt Alternate 276005 F17 Standby Alternator Power Box 121 275005 Alternator Shunt Alternate 276005 F18 Circuit Breaker Alternator Power Box 121 AN L40 Panel F19 Circuit Breaker Alternator Power Box 121 AN L40 Panel F2 Circuit Breaker Electric Power Box 121 AN L40 Panel F20 Circuit Breaker Alternator Power Box 121 ANL40 Panel F21 FLIP Door and Relay Box 121 AN L-60 Pallet Control F22 Primary Relay Box 121 ANL-60 Operators Console F23 FLIR Pallet Motor At M13 pallet motor. 255 S2565-5 F24 FLIR Pallet Motor At M13 pallet motor. 255 S2565-5 F3 Circuit Breaker Electric Power Box 121 ANL40 Panel F4 Circuit Breaker Electric Power Box 121 ANL40 Panel P5 Circuit Breaker Electric Power Box 121 AN L40 Panel F6 Circuit Breaker Electric Power Box 121 AN L40 Panel FUSE REPLACEMENTGUIDE papal 0 Cessna Aircraft Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL AIRPLANE PART NAME CIRCUIT LOCATION ZONE NUMBER F7 Circuit Breaker Electric Power Box 121 ANL40 Panel F8 Circuit Breaker Electric Power Box 121 ANL40 Panel F9 Circuit Breaker Electric Power Box 121 ANL40 Panel FUSE REPLACEMENTGUIDE Page2 0 Cessna Aircraft Company Oct 15/1999 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL SUPPLIER PUBLICATION LIST 1. General A. Outlined below is a list of manufacturers publications of which most are available from the Cessna Aircraft Company. NOTE: Publications with AF after the part number signify aerofiche. Chapter 21 Air Conditioning Item Publication Title Manufacturer Vent Blower 33E82 Blower Assembly FL Aerospace Corp. Supplier PN 33E83-2 Component Maintenance Manual Janitrol Aero Div. (Vent Blower) with Illustrated Parts 4200 Surface Rd, List Columbus, OH Publication PN 37E66-1-13 Chapter 24 Electrical Power Item Publication Title Manufacturer Battery Battery Instruction Manual Marathon Power Technologies Co. Supplier PN 30994-001 (NICAD) Marathon Battery Service 8301 Imperial Dr. Manual Waco, TX 76712-6588 Publication PN BA89-9/92-13 Battery Gill Battery Service Manual Teledyne Battery Products Supplier PN G6381E Publication PN GSM682-13 Teledyne Co, Inc. 840 W. Brockton Ave.P.O. Box 431 Redlands, CA DC to DC Power Converter Removalllnstallation Manual KGS Electronics, Inc. Supplier PN RG40 Model RG40 Regulated DC to 418A E. Live Oak Ave. DC Converter (FAA TSO-C71 Arcadia, CA 91006-5690 Approved) Publication PN 837066 Chapter 30 Ice and Rain Protection Item Publication Title Manufacturer Propeller Deice Brush Block Propeller Deice System Brush BF Goodrich Supplier PN 3E2090-1 Block Assembly Overhaul Manual Aerospace Div. and Illustrated Parts Catalog Engineered Polymer Products Publication PN 68-04-714K-13 150 Division Dr. Wilmington, NC 28401 Propeller Deice Propeller Deice System BF Goodrich Supplier PN 3E2205-4 Maintenance Manual Aerospace Div. Publication PN 68-04-712D-13 Engineered Polymer Products 150 Division Dr. Wilmington, NC 28401 Propeller Deice McCauley Electrothermal Deice Cessna Aircraft Co. Cessna PN 9910587-202 Systems Service Parts Manual McCauley Accessory Div. Supplier PN P7036368-0154 Publication PN 830415-1-13 3535 McCauley Dr. Vandalia, OH SUPPLIER PUBLICATION LIST Page 1 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL Chapter 61 Propellers Item Publication Title Manufacturer Propeller Spinner Spinner Assembly Maintenance TRW Hartzell Propeller Supplier PN D4898P D4899 Instruction Guide Division of TRW Inc. Publication PN -127-13 1800 Covington Ave. Pique, OH Propeller McCauley C700 Propeller Service Cessna Aircraft Co. Cessna PN 9910587-2-01 Manual McCauley Accessory Div. Supplier PN P7036368-01 Publication PN 8103012-13 3535 McCauley Dr. Vandalia, OH Propeller Composite Blade Inspection, TRW Hartzell Propeller Supplier PN HC-B3MN3/ Repair, and Overhaul Instructions Division of TRW Inc. M10083 Publication PN 135C-13 1800 Covington Ave, Piqua, OH Chapter 71 Powerplant Item Publication Title Manufacturer Engine Pratt 8 Whitney PT6A-34/ Pratt 8 Whitney Canada Inc. Cessna PN 9910579-1 34AG/348/36/11 4/116/135M35A 100 Marie-Victorin Blvd. Supplier PN PTGA114 Maintenance Manual Longueuil, Quebec, Canada Publication PN 3021242-13 J4G ?A? Engine Pratt 8 Whitney PT6A-34/ Pratt 8 Whitney Canada Inc. Cessna PN 9910579-1 34AG/34B/36/11 4/116/135/135A 100 Marie-Victorin Blvd. Supplier PN PTGA114 Illustrated Parts Catalog Longueuil, Quebec, Canada Publication PN 3021244-13 J4G 1Al Chapter 80 Starting Item Publication Title Manufacturer Generator Control Unit Assembly Lear Siegler 51539-012 DC Lucas Aerospace Supplier PN 51539-012N Generator Control Unit Overhaul Power Equipment Corp. Manual With Illustrated Parts List 777 Lena Drive Publication PN -51539-012-13 Aurora, OH 44202 Starter/ Generator 200SGL Starter/ Generator Unit Aircraft Parts Corp. Supplier PN 200SGL119Q-XL Overhaul Manual with Illustrated 160 Finn Ct. Parts List (208) Farmingdale, NY Publication PN -TM105A5/92-13 Starterl Generator Lear Siegler 23081 DC Lucas Aerospace Supplier PN 23081-22 Starter/Generator Overhaul Power Equipment Division Manual With Illustrated Parts List 777 Lena Drive Publication PN -23081-023-3-13 Aurora, OH 44202 Starterl Generator Lucas Aerospace DC Generators Lucas Aerospace Supplier PN 23081-22 and Starter-Generators Power Equipment Division Maintenance Manual 777 Lena Drive Publication PN Aurora, OH 44202 SUPPLIER PUBLICATION LIST Page 2 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL SUPPLIER ADDRESS LIST 00779 AMP,INC. 09052 SAFTAMERICA,INC. 2800 Fulling Mill Azalea Industrial Park P.O. Box 3608 711lndustrial Blvd. Harrisburg, PA Valdosta, GA 01295 TEXAS INSTRUMENTS, INC 09353 C AND K COMPONENTS INC. SEMICONDUCTOR GROUP 15 Riverdale Ave. M/S 3684 Newton, MA 02158-1082 13500 N. Central Expy. PO. Box 655303 Dallas, TX 02289 HI-G CO., INC. 09445 DUKES,INC. SUBDIVISION OF NYTRONICS, INC. 9060 Winnetka Ave. 101 Locust St. Northridge, CA 91324-3293 Hartford, CT 06096 03481 B.F. GOODRICH CO. 09790 EATONCORP. AEROSPACE DIV. ENGINEERED VALVE AND ACTUATOR DIV. POLYMERS PRODUCTS 2338 Alaska Ave. 150 Division Dr. El Segundo, CA 90245-11896 W~lmington, NC 28401 04655 GTE PRODUCTS CORP. OAJJO B.F GOODRICH CO. COMMUNICATIONS SYSTEMS DIV. AEROSPACE DE-ICING SYSTEMS 77 A St. 1555 CORPORATE WOODS Pkwy. Needham Heights, MA PO. Box 1277 Uniontown, OH 44685 04713 MOTOROLA, INC. SEMICONDUC- 0B9E8 ENVIRO SYSTEMS INC. TOR PROD SECTOR 4000 Hwy. 99 North 5005 E. McDowell Rd. PO. Box 1260 Phoenix, AZ Seminole, OK 74868 06177 PNEUDRAULICS, INC. 15605 EATON CORP. OP 8 TECH CTR 8575 Helms Ave. 4201 N. 27th St. Rancho Cucarnonga, CA Milwaukee, WI 53216 08717 THESLOANCO. 16017 K.G.S.ELECTRONICS, INC. 7704 San Fernando Rd. 418A E. Live Oak Ave. Sun Valley, CA 91352-4350 Arcadia, CA 91006-5690 08806 GENERAL ELECTRIC CO. 17744 GULTON INDUSTRIES, INC. MINIATURE LAMP DEFT. LIGHTING LUMINATOR DIV. BUSINESS GROUP 1200 E. Piano Parkway Nela Park Piano, TX 75074 Cleveland, OH 44112 08808 GENERAL ELECTRIC CO. 22373 ALLIED-SIGNAL INC. LAMP GLASS AND COMPONENTS ELECTRONIC 8 AVIONIC SYSTEMS DEFT. 23500 W 105th St. 24400 Highland Rd. 1 Technology Center Richmond Heights, OH Olathe, KS 66061 SUPPLIER ADDRESS LIST Page 1 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL 22526 DU PONT E I DE NEMOURS AND 31435 LUCAS AEROSPACE POWER CO. INC. EQUIPMENT CORP. DU PONT ELECTRONICS DEFT. 777 Lena Dr. 515 Fishing Creek Rd. Aurora, OH 44202 New Cumberland, PA 23939 CAPTOR CORP., THE 31669 PICO ELECTRONICS, INC. 5040 S. County Rd. 25A 453 Dr.rth Mac Questen Pkwy. Tipp City, OH 45371 Mount Vernon, NY 10552-2608 24444 GENERAL SEMICONDUCTOR 32245 AEROSPACE OPTICS, INC. INDUSTRIES, INC. 3201 Sandy Ln. SUBDIVISION OF SQUARE D CO. Forth Worth, TX 76112 2001 W 10th PI. Tempe, AZ 24446 GENERAL ELECTRIC CO. 32970 AIRCRAFT PARTS CORP. 3135 Easton Turnpike 160 Finn Ct. Fairfield, CT Farmingdale, NY 26433 PARKER-HANNIFIN CORP. 32997 BOURNS,INC. AIRBORNE DIV. TRIMPOT DIV. 711 Taylor St. 1200 Columbia Ave. P.O. Box 4032 Riverside, CA 92507-2114 Elyria, OH 44036 27014 NATIONAL SEMICONDUCTOR 34163 AEROSPACE SYSTEMS AND CORP. COMPONENTS, INC. 2900 Semiconductor Dr. 1620 S. Broadmoor Santa Clara, CA Wichita, KS 67218 27191 CUTLER-HAMMER,INC. 36540 LISLECORP. POWER DISTRIBUTION AND 807 E. Main St. CONTROL DIV. Clarinda, IA Milwaukee, WI 27192 EATONCORP. 37942 NORTHAMERICAN CAPACITORCO. SPECIFIC INDUSTRY CONTROL MALLORY DIV. DIV. Indianapolis Rd. Hwy. 240 4265 N. 30th St. PO. Box 273 Milwaukee, WI Indianapolis, IN 46135 27193 EATON CORP. AEROSPACE/ 51589 ST-SEMICON INC. COMMERCIAL CONTROLS DIV. 415 College Ave. Milwaukee, WI Bloomington, N 27264 MOLEX,INC. 54071 COMMERCIAL AIRCRAFT 2222 Wellington Ct. PRODUCTS INC. Lisle, IL 60532-1613 2569 W Pawnee Wichita, KS 31433 KEMET ELECTRONICS CORP. PO. Box 5928 Greenville, SC 29606 SUPPLIER ADDRESS LIST Page 2 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL 57041 SPECOINC. 64817 ELECTRODELTAINC. 5 Merril Industrial Dr. 999 Cherokee Tr. P.O. Box 1930 PO. Box 8 Hampton, MA White Oak, TX 75693 58614 COMMUNICATIONS INSTRUMENTS, 69275 TEC FAR MFG. INC. INC. 11600 Tuxford St. Highway 74 East Sun Valley, CA 91352 P.O. Box 520 Fairview, NC 28730 58880 ARMTECINDUSTRIES, INC. 71468 ITTCANNON SUBDIVISION OF BESTOBEL PLC DIV. OF ITT CORP. 10 Ammon Dr. 666 E. Dyer Rd. Manchester, NH 03103-7406 Santa Ana, CA 58918 AEROSPACE CONTROL PRODUCTS 71590 CRL COMPONENTS., INC. INC. 228 Kenyon Rd. W 1314 W 76th St. Ft. Dodge, IA 50501-5639 Davenport, IA 5Y111 ICE CORP. 72914 FL AEROSPACE CORP. 240 Levee Dive GRIMES DIV. Manhattan, KS 66502 550 Rt. 55 P.O. Box 247 Urbana, OH 61349 AMETEC INC. U.S. GAUGE DIV. 74025 MARATHON BA~TERY CO. 900 Clymer Ave. 8301 Imperial Dr. Sellersville, PA Waco,TXP.O. Box 8233 61725 ITT COMPONENTS 75915 LITTLEFUSE TRACOR, INC. DIV OF ITT CORP. SUBDIVISION. OF TRACOR, INC. 1201 E. Mo Fadden 800 E. N.W. Hwy. Santa Anna, CA Des Plaines, IL 60016 62219 GENELCOINC. 76374 MECHANICAL PRODUCTS, INC. 11649 Chairman Dr. No. 16 SUBDIVISION OF SPRECKLES Dallas, TX INDUSTRIES, INC. 1824 River St. P.O. Box 729 Jackson, MI 49204-1755 63017 CONCORDE BATTERY CORP. 76854 OAK SWITCH SYSTEMS, INC. 2009 San Bernardino Rd. AN OAK INDUSTRIES INC. CO. West Covina, CA 91970 100 S. Main St. PO. Box 517 Crystal Lake, IL 60014 63426 NKK SWITCHES OF AMERICA, INC. 14415 N. Scottsdale Rd. No. 600 Scottsdale, AZ 85260 63829 SANDEN INTERNATIONAVUSA/INC. 10710 Sanden Dr. Dallas, TX SUPPLIER ADDRESS LIST Page 3 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL 77342 AMF,INC. POTTERANDBRUMFIELD 91929 HONEYWELL,INC. DIV. MICRO SWITCH DIV. 200 Richland Creek Dr. 11 W Spring St. Princeton, IN 47671-0001 Freeport, IL 61032 78488 STACKPOLE CORP., THE 93790 CORNELL-DUBILIER ELECTRONICS 201 Stackpole St. 1605 E. Rodney French Blvd. St. Marys, PA PO. Box 8-967 New Bedford, MA 81640 EATONCORP. 93929 WARREN G-V AEROSPACE AND COMMERCIAL UNIT OF GENERAL SIGNAL CORP. CONTROLS DIV. 1 Apollo Dr. 2250 Whitfield Ave. E Whippany, NJ 07981 Sarasota, FL 34243-9703 82647 TEXASINSTRUMENTS, INC. 96182 EATONCORP CONTROL PRODUCTS DIV. AEROSPACE AND COMMERCIAL 34 Forest St. CONTROLS MSC PRODUCTS DIV. Mail Station 12-33 1640 Monrovia Ave. Attleboro, MA 02703 Costa Mesa, CA 92627-4405 83326 SAFE FLIGHT INSTRUMENT CORP. 97484 TECHNICAL DEVELOPMENTCO New King St. 24 E. Glenolden Ave. PO. Box 550 Glenolden, PA 19036-2107 White Plains, NY 10602 83564 WEMAC 98087 ITTCORP. DIV. OF PURITAN-BENNETT ITT AEROSPACE CONTROLS ITT Fountain Valley, CA 92708-7004 28150 Industry Dr. 18475 Pacific St. N EO-DYN E Valencia, CA 91355-0000 84375 TELEDYNE BATTERY PRODUCTS D1510 KISSLING HEINRICH GMBH UND TELEDYNE INC. CO. CO. KG. 840 W Brockton Ave. FEINMECHANIK U P.O. Box 431 ELEKTROTECHNIK Redlands, CA IM Bohnland 16 7277 Wildberg 5 Germany 86887 SIGMA TEK, INC. FRIG FRIGETTE CORP. 1001 Industrial Rd. Ft. Worth, TX Augusta, KS 67010 89513 FL AEROSPACE CORP. JANITROL MCCI MID-CONTINENT CONTROLS, INC. AERO DIV. 207 S. Buckner 4200 Surface Rd. Derby, KS 67037 Columbus, OH 43228 8N273 AERO-MACH LABORATORIES, INC. 633 E. Harry Wichita, KS SUPPLIER ADDRESS LIST Page 4 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL MODN MODERN MOTORS, INC. 785 N. Freedom St. Ravenna, OH 44266 U6335 HAWKER ENERGY PRODUCTS, LTD. Stephenson St. Newport, Swent, UK NP9 OXJ SUPPLIER ADDRESS LIST Page 5 0 Cessna Aircraft Company Sep 1/2000 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL LIST OF CHAPTERS CHAPTER EFFECTIVE DATE 20 Standard Practices Airframe Jan 1/2007 21 Air Conditioning Mar 1/2001 24 Electrical Power Jan 1/2007 26 Fire Protection Sep 1/2000 27 Flight Controls Sep 1/2000 28 Fuel Jan 1/2007 30 Ice and Rain Protection Jan 1/2007 31 Indicating Recording Systems Jan 1/2007 32 Landing Gear Jan 1/2007 33 Lights Jan 1/2007 34 Navigation Jan 1/2007 37 Vacuum Oct 15/1999 52 Doors Sep 1/2000 61 Propeller Mar 1/2001 73 Engine Fuel And Control Sep 1/2000 74 Ignition Oct 15/1999 77 Engine Indicating Jan 1/2007 79 Oil Oct 15/1999 91 Charts Jan 1/2007 Represents date of each chapter’s List of Effective Pages which is applicable to manual revision date. LIST OF CHAPTERS Page 1 Q Cessna AircraA Company Jan 1/2007 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL NOMENCLATURE CH SEC SUBJ FIG A AIR CONDITIONER 208 21-50-01-01 AIR CONDITIONER 2088 PASSENGER 21-50-01-02 AIRSPEED SWITCH 34-1 AIRSPEED WARNING .........,._._.. 34-10-01 AIRSPEED WARNING ALARM ASSEMBLY 34-10-02-01 AIRSPEED WARNING ALARM ASSEMBLY 34-1002~2 ALTAIR ETM ANNUNCIATOR PANEL 31-50-01-01 ANNUNCIATOR PANELASSEMBLY 31-50-02-01 ANNUNCIATOR PANEL ASSEMBLY 31-50-02-02 ANNUNCIATOR PANELASSEMBLY 31-50-02-03 ATTITUDE AND DIRECTIONAL GYROS 34-20-02-01 AUXILIARY FUEL PUMP 208 2&20-01-01 AUXILIARY FUEL PUMP 2088 2&20-01-02 B BATTERY CIRCUIT BATTERY CIRCUIT ................_ ................_ BATTERY CIRCUIT ................_ BATTERY TEMPERATURE WARNING 24-34-03-01 BETA MODE WARNING 31-50-05-01 BONDING AND GROUNDINGMMANNTNNANC PRACTICES 20-10-02 C CABIN HEATER CABIN LIGHTS 208 CABIN LIGHTS 2088 CABIN LIGHTS WITH TIMER 208 33-20-01-03 CABIN LIGHTS WITH TIMER 2088 33-20-01-04 CABIN VENTILATION BLOWERS WITHOUT AIR CONDITIONING 21-20-01-01 CARGO POD DEICE RELAY 30-10-02-01 CHIP DETECTORS COAX CABLE CONNECTORS-MAINTENANCE PRACTICES ........._._._ 20-10-05 CONFORMAL COATING FOR PRINTED CIRCUIT BOARDS 20-10-12 CONNECTORS COURTESY LIGHTS 33-20-03-01 D DIMMABLE PANEL LIGHTS 33-10-01-01 DIMMABLE PANEL LIGHTS-BRITISH 33-10-01-03 DIMMABLE PANEL LIGHTS-FRENCH 1 33-10-01-02 DIRECTIONAL GYRO-LEFT 208 34-20-031)1 DOOR POST CABLE ASSEMBLY 208 .........____ 24-61-01-01 DOOR POST CABLE ASSEMBLY 208 .........____ 24-61-01-02 DOOR POST CABLE ASSEMBLY 208 24-61-01-03 DOOR POST CABLE ASSEMBLY 208 24-61-01-04 DOOR POST CABLE ASSEMBLY 208 24-61-01-05 DOOR POST CABLE ASSEMBLY 2088 24-61-02-01 DOOR POST CABLE ASSEMBLY 2088 24-61-02-02 DOOR POST CABLE ASSEMBLY 2088 24-61-02-03 DOOR POST CABLE ASSEMBLY 2088 24-61-02-04 DOOR POST CABLE ASSEMBLY 2088 24-61-02-05 DOOR UNLOCKED WARNING .........____ 52-70-01-01 ALPHABETICAL INDEX Page 1 0 Cessna Aircraft Com pany Jan 1/2007 CESSNA AIRCRAFT COMPANY NIODEL 208 WIRING DIAGRAM MANUAL NOMENCLATURE CH SEC SUBJ FIG E ELECTRIC CLOCK ELECTRIC TORQUE INDICATOR 77-10-03-01 ELECTRICAL CONNECTORS-MAINTENANCE PRACTICES 20-1 0-04 ELECTRICAL SAFETY PRECAUTIONS 20-10-00 ELEVATOR TRIM 208 27-30-02-01 EMERGENCY POWER LEVER WARNING 31-50-03-01 EXIT SIGN-CHINESE 33-20-06-01 EXTERNAL POWER 24-40-01-01 EXTERNAL POWER 24-40-01-02 EXTERNAL POWER 24-40-02-01 EXTERNAL POWER 24-40-02-02 F FIRE DETECTION FIRE WARNING ALARM ASSEMBLY 26-10-02-01 FIRE WARNING ALARM ASSEMBLY 26-10-02-02 FLAP CONTROL FLASHING BEACON LIGHT 33-40-03-01 FUEL CONTROL HEATER 73-10-01-01 FUEL FLOW FUEL QUANTITY FUEL SELECT OFF WARNING 208 28-42-01-01 FUEL SELECT OFF WARNING 2088 28-42-01-01 FUEL SELECT OFF WARNING RELAY ASSEMBLY 2670088-1 2&42-02-01 FUEL TOTALIZER G GAS GENERATOR SPEED 77-10-02-01 GENERATOR OVERHEAT WARNING 24-30-03-01 H HEAT SHRINKABLE TUBING-MAINTENANCE PRACTICES 20-10-07 HOURMETER ICE DETECTOR LIGHT 33-10-03-01 IGNITION IN-FLIGHT MOVEABLE DOOR 52-10-01-01 INTER TURBINE TEMPERATURE INDICATOR 77-20-01-01 J JUMP LIGHTS L LANDING AND TAXI LIGHTS 33-40-01-01 LANDING GEAR-AMPHIBIAN 32-30-01-01 LOW AIRSPEED WARNING, ICING(OPT) 34-10-04-01 LOW AIRSPEED WARNING, ICING (OPT) 34-10-04-02 LOW FUEL LEVEL WARNING 2&41-01-01 LOW FUEL LEVEL WARNING-WING TANKS 28-41-02-01 LOW OIL PRESSURE WARNING 79-30-01-01 LOW VACUUM WARNING 24-30-04-01 37-20-01-01 LOW VOLTAGE WARNING ALPHABETICAL INDEX Page 2 0 Cessna Aircraft Company Jan 1/2007 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL NOMENCLATURE CH SEC SUBJ FIG M MAP LIGHT ........._.,._._ N NAVIGATION AND STROBE LIGHTS ........._._._._ 33-40-02-01 O OIL TEMPERATURE INDICATOR 7930-02-01 P PITOT AND STATIC HEATERS 208 30-30-01-01 PITOT AND STATIC HEATERS 2088 30-30-01-02 PITOT AND STATIC HEATERS-FRENCH 30-30-01-03 POWER DISTRIBUTION ........._,__ .........__,_ 24-60-01-01 POWER DISTRIBUTION 24-60-01-02 POWER DISTRIBUTION 24-60-01-03 POWER DISTRIBUTION 24-60-01-04 PROPELLER DEICE 30-60-01-01 PROPELLER DEICE 30-60-01-02 PROPELLER OVERSPEED TEST .........____ 61-40-01-01 PROPELLER SPEED 77-1 R READING LIGHTS 208 .........___., ........._._._._ 33-20-02-01 READING LIGHTS 2088 ........._ 33-20-02-02 RESISTORS-MAINTENANCE PRACTICES 20-10-08 S SEALING OF ELECTRICAL CONNECTORS 20-10-10 SEAT BELTINO SMOKING SIGN 33-20-04-01 SOLDERING-MAINTENANCE PRACTICES 20-10-03 SPLICES AND TERMINALS ........._._._._ ........._._._._ 20-10-06 STALL WARNING STALL WARNING STANDBY ALTERNATOR 24-36-01-01 STANDBY ALTERNATOR 24-36-01-02 STANDBY ALTERNATOR ........._._._._ ........._._._._ 24-36-01-03 STANDBY ALTERNATOR 24-36-01-04 STANDBY ALTERNATOR 24-36-02-01 STANDBY ALTERNATOR 24-3802´•02 STANDBY ALTERNATOR OVERHEAT WARNING 24-36-03-01 STARTEWGENERATOR .........____ .........____ 24-30-01-01 STARTEWGENERATOR .........____ 24-30-01-02 STARTEWGENERATOR .........____ 24-30-01-03 STARTERIGENERATOR 24-30-01-04 STARTEWGENERATOR 24-30-01-05 STARTER/GENERATOR 24-30-01-06 STARTER/GENERATOR .........____ 24-30-02-01 STARTEWGENERATOR 24-30-02-02 T TORQUE VALUES FOR THREADED FASTENERS .........____ .........____ 20-10-09 TURN 8 BANK AND TURN COORDINATOR INDICATORS 34-20-01-01 ALPHABETICAL INDEX Page 3 0 Cessna Aircraff Company Jan 1/2007 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL NOMENCLATURE CH SEC SUBJ FIG V VOLT-AMMETER VOLT-AMMETER WITH STANDBY ALTERNATOR 24-37-02-01 VOLT-AMMETER WITH STANDBY ALTERNATOR 24-37-03-01 VOLT-AMMETER WITH STANDBY ALTERNATOR 24-37-03-02 W WINDSHIELD ANTI-ICE 30-40-01-01 WINDSHIELD ICE DETECT LIGHT (OPT) 30-80-01-01 WING AND STABILIZER DEICE 208 30-10-01-01 WING AND STABILIZER DEICE 2088 30-10-01-02 WIRING-MAINTENANCE PRACTICES 20-10-01 ALPHABETICAL INDEX Page 4 0 Cessna Aircraft Company Jan 1/2007 CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR A ACTUATOR ELECTRIC ELEVATOR TRIM In control pedestal. M3 AiARM ASSEMBLY AIRSPEED Above pilot’s seat. AD3 ALARM ASSEMBLY FIRE Above Pilot’s seat. AD2 ALARM ASSEMBLY STALL WARNING Above pilot’s seat. AD1 ALTERNATOR STANDBY On rear of engine. ALT1 ALTERNATOR STANDBY On rear of engine. ALT1 AMMETER LEFT PITOT HEATER On pilot’s instrument panel. A2 AMMETER RIGHT PITOT HEATER On Copilot’s instrument panel. A3 ANNUNCIATOR PANEL At top of instrumentpanel. CU1 ANNUNCIATOR PANEL At top of instrument panel. CUI ATTITUDE GYRO On copilot’s instrument panel. IND11 ATTITUDE GYRO On copilot’s instrument panel. INDIS B BATTERY LEAD ACID Forward side of firewall right of engine. BATT1 BATTERY OPTIONAL NICAD. Forward side of firewall right of engine. BATT1 BATTERY SEALED LEAD ACID 40AH Forward side of firewall right of engine. BATT1 BLOWER FRESH AIR VENT In inboard end of left wing. M5 BLOWER FRESH AIR VENT In inboard end of right wing. M4 BLOWER AFT EVAPORATOR In forward end of tailcone. M6 BLOWER LEFT EVAPORATOR In inboard end of left wing. M8 BLOWER RIGHT EVAPORATOR In inboard end of right wing. M7 C CAPACITOR Mounted withwire clamp on forward end of standby alternator. C1 CAPACITOR In annunciator panel assembly on instrument panel. C1 CHIP DETECTOR ACCESSORY GEARBOX On bottom of engine. XMTRIG CHIP DETECTOR REDUCTION GEARBOX On bottom of engine. XMTR17 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB62 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB72. CIRCUIT BREAKER Circuit breaker panel in cockpit. CB73 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB75 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB76 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB90 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB91 CIRCUIT BREAKER ADF 1 Circuit breaker panel in cockpit. CB66 CIRCUIT BREAKER AFT VENT BLOWER Circuit breaker panel in cockpit. CB307 CIRCUIT BREAKER AIR CONDITIONING COMPRESSOR Circuit breaker panel in cockpit. CB210 CIRCUIT BREAKER AIR CONDITIONING CONT Circuit breaker panel in cockpit. CB210 CIRCUIT BREAKER AIR SPEED WARNING Circuit breaker panel in cockpit. CB405 CIRCUIT BREAKER ANNUNCIATOR PANEL Circuit breaker panel in cockpit. CB~08 CIRCUIT BREAKER ANNUNCIATOR PANEL Circuit breaker panel in cockpit. CB208 CIRCUIT BREAKER ANTI CYCLE SWITCH In electrical power box on forward side of firewall left of CB71 engine.´• CIRCUIT BREAKER AUDIO AMPLIFIER Circuit breaker panel in cockpit. CB81 CIRCUIT BREAKER AUDIOIMARKER Circuit breaker panel in cockpit. CB69 CIRCUIT BREAKER AUTO PILOT RELAY Circuit breaker panel in cockpit. CB71 CIRCUIT BREAKER AUTOPILOT ACTUATOR Circuit breaker panel in cockpit. CB70 CIRCUIT BREAKER AUTOPILOT FLIGHT DIRECTOR Circuit breaker panel in cockpit. CB93 CIRCUIT BREAKER AUXILIARY FUEL PUMP Circuit breaker panel in cockpit. CB205 COM’PONENT INDEX Page 1 Jan 1/2007 O Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR CIRCUIT BREAKER AVIONICS FAN Circuit breaker panel in cockpit. CBSO CIRCUIT BREAKER BATTERY RELAY In electrical power box on forward side of firewall left of CB72 engine. CIRCUIT BREAKER BEACON LIGHT Circuit breaker panel in cockpit. CB504 CIRCUIT BREAKER BLEED AIR HEAT Circuit breaker panel in cockpit. CB306 CIRCUIT BREAKER BUS 1 POWER Circuit breaker panel in cockpit. CB101 CIRCUIT BREAKER BUS 1 POWER Circuit breaker panel in cockpit. CB301 CIRCUIT BREAKER BUS i POWER Circuit breaker panel in cockpit. CB501 CIRCUIT BREAKER BUS 2 POWER Circuit breaker panel in cockpit. CB201 CIRCUIT BREAKER BUS 2 POWER Circuit breaker panel in cockpit. CB401 CIRCUIT BREAKER BUS 2 POWER Circuit breaker panel in cockpit. CB601 CIRCUIT BREAKER CABIN LIGHTS In electrical power box on forward side of firewall left of engine. CBAOG CIRCUIT BREAKER CDI Circuit breaker panel in cockpit. CB97 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB62 CIRCUIT BREAKER Circuit breaker panel in cockpit. CB72 CIRCUIT BREAKER CLOCK In electrical power box on forward side of firewall left of engine. CB75 CIRCUIT BREAKER COMPASS Circuit breaker panel in cockpit. CB99 CIRCUIT BREAKER DE-ICE BOOT Circuit breaker panel in cockpit. CB407 CIRCUIT BREAKER DME Circuit breaker panel in cockpit. CB77 CIRCUIT BREAKER ELEVATOR TRIM Circuit breaker panel in cockpit. CB61 CIRCUIT BREAKER ELEVATOR TRIM Circuit breaker panel in cockpit. CB610 CIRCUIT BREAKER ENCODING ALTIMETER Circuit breaker panel in cockpit. CB60 CIRCUIT BREAKER FIRE DETECT Circuit breaker panel in cockpit. CB302 CIRCUIT BREAKER FLAP MOTOR Circuit breaker panel in cockpit. CB103 CIRCUIT BREAKER FUEL CONTROL HEATER Circuit breaker panel in cockpit. CB206 CIRCUIT BREAKER FUEL FLOW Circuit breaker panel in cockpit. CB403 CIRCUIT BREAKER FUEL SELECT WARNING Circuit breaker panel in cockpit. CB111 CIRCUIT BREAKER FUEL TOTALIZER Circuit breaker panel in cockpit. CB303 CIRCUIT BREAKER GENERATOR CONTROL Circuit breaker panel in cockpit. CB109 CIRCUIT BREAKER GENERATOR FIELD Circuit breaker panel in cockpit. CB110 CIRCUIT BREAKER GENERATOR RELAY SENSE In electrical power box on forward side of firewall CB70 left of engine. CIRCUIT BREAKER GLIDESLOPE 1 Circuit breaker panel in cockpit. CB65 CIRCUIT BREAKER GYRO SLAVE Circuit breaker panel in cockpit. CB68 CIRCUIT BREAKER HF RECEIVER Circuit breaker panel in cockpit. CB87 CIRCUIT BREAKER HF TRANSMITTER Circuit breaker panel in cockpit. CB85 CIRCUIT BREAKER HF TRANSMITTER Circuit breaker panel in cockpit. CB86 CIRCUIT BREAKER HSI 1 Circuit breaker panel in cockpit. CB67 CIRCUIT BREAKER IGNITION Circuit breaker panel in cockpit. CB105 CIRCUIT BREAKER INSTRUMENT LIGHTS Circuit breaker panel in cockpit. CB506 CIRCUIT BREAKER INVERTER 1 Circuit breaker panel in cockpit. CB95 CIRCUIT BREAKER INVERTER 2 Circuit breaker panel in cockpit. CB96 CIRCUIT BREAKER ITT GAGE- Circuit breaker panel in cockpit. CB402 CIRCUIT BREAKER LEFT DIRECTIONAL GYRO Circuit breaker panel in cockpit. CB508 CIRCUIT BREAKER LEFT FUEL QUANTITY Circuit breaker panel in cockpit. CB304 CIRCUIT BREAKER LEFT LANDING LIGHT Circuit breaker panel in cockpit. ,CB502 CIRCUIT BREAKER LEFT PITOT HEAT Circuit breaker panel in cockpit. CB308 CIRCUIT BREAKER LEFT TURN BANK INDICATOR Circuit breaker panel in cockpit. CB107 CIRCUIT BREAKER LEFT VENT BLOWER Circuit breaker panel in cockpit. CB203 CIRCUIT BREAKER LORAN GPS Circuit breaker panel in cockpit. CB84 CIRCUIT BREAKER MAP LIGHT Circuit breaker panel in cockpit. CB505 CIRCUIT BREAKER NAV 1 Circuit breaker panel in cockpit. CB63 COM PON ENT IN DEX Page 2 Jan 1/2007 O Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR CIRCUIT BREAKER NAVIGATION LIGHTS Circuit breaker panel in cockpit. CB604 CIRCUIT BREAKER OIL TEMPERATURE Circuit breaker panel in cockpit. CB305 CIRCUIT BREAKER PROP ANTI-ICE CONT Circuit breaker panel in cockpit. CB510 CIRCUIT BREAKER PROPELLER ANTI-ICE Circuit breaker panel in cockpit. CB409 CIRCUIT BREAKER PROPELLER ANTI-ICE Circuit breaker panel in cockpit. CB410 CIRCUIT BREAKER PROPELLER OVERSPEED Circuit breaker panel in cockpit. CB406 CIRCUIT BREAKER RADAR CONTROL Circuit breaker panel in cockpit. CB88 CIRCUIT BREAKER RADIO ALTIMETER Circuit breaker panel in cockpit. CB79 CIRCUIT BREAKER RADO AND FLOOD LIGHTS Circuit breaker panel in cockpit. CB605 CIRCUIT BREAKER READING LIGHTS Circuit breaker panel in cockpit. CB606 CIRCUIT BREAKER RIGHT ATTITUDE GYRO Circuit breaker panel in cockpit. CB608 CIRCUIT BREAKER RIGHT CLOCK In electrical power box on forward side of firewall left of engine. CB2 CIRCUIT BREAKER RIGHT DIRECTIONAL GYRO Circuit breaker panel in cockpit. CB609 CIRCUIT BREAKER RIGHT FUEL QUANTITY Circuit breaker panel in cockpit. CB404 CIRCUIT BREAKER RIGHT LANDING LIGHT Circuit breaker panel in cockpit. CB602 CIRCUIT BREAKER RIGHT PITOT HEAT Circuit breaker panel in cockpit. CB408 CIRCUIT BREAKER RIGHT TURN BANK INDICATOR Circuit breaker panel in cockpit. CB207 CIRCUIT BREAKER RIGHT VENT BLOWER Circuit breaker panel in cockpit. CB204 CIRCUIT BREAKER RMI Circuit breaker panel in cockpit. CB92 CIRCUIT BREAKER RNAV Circuit breaker panel in cockpit. CB78 CIRCUIT BREAKER SEAT BELT SIGN Circuit breaker panel in cockpit. CB607 CIRCUIT BREAKER STALL WARNING Circuit breaker panel in cockpit. CB209 CIRCUIT BREAKER STANDBY ALTERNATOR In standby altemator relay box on forward side of CB73 firewall left of engine. CIRCUIT BREAKER STANDBY FLAP MOTOR Circuit breaker panel in cockpit. CB104 CIRCUIT BREAKER STANDBY POWER Circuit breaker panel in cockpit. CB102 CIRCUIT BREAKER STANDBY POWER Circuit breaker panel in cockpit. CB202 CIRCUIT BREAKER START CONTROL Circuit breaker panel in cockpit. CB106 CIRCUIT BREAKER STORM SCOPE Circuit breaker panel in cockpit. CB83 CIRCUIT BREAKER STROBE LIGHT Circuit breaker panel in cockpit. CB503 CIRCUIT BREAKER TAXI LIGHT Circuit breaker panel in cockpit. CB603 CIRCUIT BREAKER TORQUE IND Circuit breaker panel in cockpit. CB410 CIRCUIT BREAKER TORQUE INDICATOR Circuit breaker panel in cockpit. CB510 CIRCUIT BREAKER TRANSPONDER i Circuit breaker panel in cockpit. CB64 CIRCUIT BREAKER TRANSPONDER 2 Circuit breaker panel in cockpit. CB74 CIRCUIT BREAKER VERTICAL GYRO Circuit breaker panel in cockpit. CB98 CIRCUIT BREAKER WINDSHIELD ANTI-ICE Circuit breaker panel in cockpit. CB309 CIRCUIT BREAKER WINDSHIELD ANTI-ICE Circuit breaker panel in cockpit. CB310 CIRCUIT BREAKER WING ICE DETECTION LIGHT Circuit breaker panel in cockpit. CB507 CIRCUIT BREAKER YAW GYRO Circuit breaker panel in cockpit. CB100 CIRCUIT BREAKER AUDIO AMPLIFIER Circuit breaker panel in cockpit. CB81 CIRCUIT BREAKER AUTOPILOT CONTROL Circuit breaker panel in cockpit. CB71 CIRCUIT BREAKER BEACON LIGHT Circuit breaker panel in cockpit. CB504 CIRCUIT BREAKER DE-ICE BOOT Circuit breaker panel in cockpit. CB407 CIRCUIT BREAKER PROP ANIT-ICE Circuit breaker panel in cockpit. CB509 CIRCUIT BREAKER PUMP 2 Circuit breaker panel in cockpit. CB510 CIRCUIT BREAKER RADAR Circuit breaker panel in cockpit. CB89 CIRCUIT BREAKER READING LIGHTS Circuit breaker panel in cockpit. CB606 CLOCK On pilot’s instrument panel. IND18 CLUTCH AIR CONDITIONER COMPRESSOR On engine. Mg COMPASS In compass above instrument panel. L4 COMPRESSOR AIR CONDITIONER On engine. Mg COMPONENT INDEX Page 3 Jan 1/2007 O Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR CONNECTOR Connects to fuel Row transmitter on aft end of engine. J5 CONNECTOR Connects to propeller deice varistor on forward side of firewall at top and center of J200 firewall. CONNECTOR Connects to propeller deice varistor on forward side of firewali at top and center of J214 firewall. CONNECTOR Connects to propeller deice varistor on forward side of firewall at top and center of P215 firewall. CONNECTOR Connects to propeller deice varistor on forward side of firewall at top and center of P300 firewall. CONNECTOR Amphibian gear pump power disconnect at forward side of circuit breaker panel. J300 CONNECTOR Amphibian gear pump power disconnect at forward side of circuit breaker panel. J301 CONNECTOR Amphibian gear pump power disconnect at forward side of circuit breaker panel. P300 CONNECTOR Amphibian gear pump power disconnect at forward side of circuit breaker panel. P301 CONNECTOR Circuit breaker panel disconnect on forward side of circuit breaker panel. J10 CONNECTOR Circuit breaker panel disconnect on forward side of circuit breaker panel. J37 CONNECTOR Circuit breaker panel disconnect on forward side of circuit breaker panel. J74 CONNECTOR Circuit breaker panel disconnect on forward side of circuit breaker panel. P10 CONNECTOR Circuit breaker panel ~disconnect on forward side of circuit breaker panel. P74 CONNECTOR Connects to accessory gearbox chip detector on bottom of engine. J86 CONNECTOR Connects to aR air conditioner blower in forward end of tailcone. J117 CONNECTOR Connects to aft air conditioner blower in forward end of tailcone. P1 17 CONNECTOR Connects to aff air conditioner blower switch on pilot’s switch panel. J115 CONNECTOR Connects to aft air conditioner blower switch on pilot’s switch panel. P115 CONNECTOR Connects to aircraft battery. Pi77 CONNECTOR Connects to airspeed alarm assembly above pilot’s seat. P?34 CONNECTOR Connects to airspeed waming switch on aft side of firewall forward of pilot’s P18 instrument panel. CONNECTOR Connects to amphibian gear select indicator on instrument panel. P167 CONNECTOR Connects to annunciator panel assembly on instrument panel. PK24 CONNECTOR Connects to attitude gym on copilot’s instrument panel. J88 CONNECTOR Connects to auxiliary fuel pump relay below cabin center Roorboards aff of pilot seats. J121 CONNECTOR Connects to auxiliary fuel pump relay below cabin center fioorboards aff of pilot seats. J122 CONNECTOR Connects to auxiliary fuel pump relay below cabin center Roort,oards aft of pilot seats. P121 CONNECTOR Connects to auxiliary fuel pump relay below cabin center floorboards aff of pilot seats. Pi22 CONNECTOR Connects to battery temperature sensor on NICAD aircraff battery. J75 CONNECTOR Connects to bleed air control valve on engine support on right side of engine. J39 CONNECTOR Connects to bleed air switches on top of bleed air duct below aft end of engine. J45 CONNECTOR Connects to bleed air switches on top of bleed air duct below aft end of engine. P45 CONNECTOR Connects to bleed air temperature switch on right side of bleed air duct below aft end J46 of engine. CONNECTOR Connects to cabin light timer on sidewall forward of circuit breaker panel. J60 CONNECTOR Connects to cargo pod and landing gear deice relay on inboard end of left wing below P182 deice timer. CONNECTOR Connects to circuit breaker panel and lower instrument panel light dimmer control on J148 bottom of instrument panel. CONNECTOR Connects to circuit breaker panel and lower instrument panel light dimmer control on P148 bottom of instrument panel. CONNECTOR Connects to circuit breaker panel. P37 CONNECTOR Connects to cockpit flood light diode assembly in cockpit overhead panel. J51 CONNECTOR Connects to cockpit flood light diode assembly in cockpit overhead panel. J52 CONNECTOR Connects to cockpit Rood light diode assembly in cockpit overhead panel. P51 CONNECTOR Connects to cockpit Rood light diode assembly in cockpit overhead panel. P52 CONNECTOR Connects to deice timer on inboard end of left wing aff of front spar. J13 COMPONENT INDEX Page 4 Jan 112007 O Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR CONNECTOR Connects to digital clock on copilot’s instrument panel. 579 CONNECTOR Connects to digital clock on copilot’s instrument panel. P79 CONNECTOR Connects to digital clock on pilot’s instrument panel. J80 CONNECTOR Connects to digital clock on pilot’s instrument panel. P80 CONNECTOR Connects to directional gym on copilot’s instrument panel. J89 CONNECTOR Connects to directional gym on pilot’s instrument panel. J83 CONNECTOR Connects to dome light above passenger door. J109 CONNECTOR Connects to dome light above passenger door. P109 CONNECTOR Connects to electric elevator trim actuator in control pedestal. PK16 CONNECTOR Connects to electric elevator trim relay in control pedestal. J140 CONNECTOR Connects to electric power box at left end of Rrewall forward of circuit breaker panel. P7 CONNECTOR Connects to electric power box at left end of firewall forward of circuit breaker panel. PZ25 CONNECTOR Connects to emergency power waming switch in power console at bottom of throttle J306 lever. CONNECTOR Connects to emergency power warning switch in power console at bottom of throttle P306 lever. CONNECTOR Connects to engine torque indicator at top of instrument panel. J100 CONNECTOR Connects to engine torque transmitter on right engine support. J211 CONNECTOR Connects to fire alarm assembly above pilot’s seat. P135 CONNECTOR Connects to fire warning control on aft side of firewall forward of pilot’s instrument J19 panel. CONNECTOR Connects to fire warning control on aft side of firewall forward of pilot’s instrument P19 panel. CONNECTOR Connects to flap motors in top right area of cabin. J156 CONNECTOR Connects to flap motors in top right area of cabin. J178 CONNECTOR Connects to flap motors in top right area of cabin. P156 CONNECTOR Connects to flap motors in top right area of cabin. P178 CONNECTOR Connects to flashing beacon on top of vertical tail. J85 CONNECTOR Connects to flashing beacon on top of vertical tail. P85 CONNECTOR Connects to forward dome light, 208. Connects to aft light of two dome lights in J108 forward part of cabin, 2088. CONNECTOR Connects to forward dome light, 208. Connects to aft light of two dome lights in P108 forward part of cabin, 2088. CONNECTOR Connects to forward light of two dome lights in forward part of cabin, 2088. J103 CONNECTOR Connects to forward light of two dome lights in forward part of cabin, 2088. P103 CONNECTOR Connects to fuel control heater on aft end of engine. J28 CONNECTOR Connects to fuel flow indicator at top of instrument panel. J6 CONNECTOR Connects to fuel select off waming relay assembly in sidewall forward of circuit J210 breaker panel. CONNECTOR Connects to fuel totalizer signal conditioner of forward side of right instrument panel. J97 CONNECTOR Connects to gas generator percent speed indicator at top of instrument panel. J135 CONNECTOR Connects to gearbox chip detector on bottom of engine. J87 CONNECTOR Connects to ge?erator control unit on left sidewall forward of circuit breaker panel. P24 CONNECTOR Connects to ground block on a bracket at left side of firewall forward of instrument J66 panel. CONNECTOR Connects to ground block on bracket at left side of firewall forward of instrument J9 panel. CONNECTOR Connects to hourmeter on right side of instrument panel. ´•J305 CONNECTOR Connects to hourmeter on right side of instrument panel. P305 CONNECTOR Connects to ignition exciter on right engine support. J27 CONNECTOR Connects to inter turbine temperature indicator at top of instrument panel. J30 CONNECTOR Connects to jump light switch. J191 CONNECTOR Connects to jump light switch. P191 COh()PONENT INDEX Page 5 Jan 1/2007 O Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR CONNECTOR Connects to jump lights. J192 CONNECTOR Connects to jump lights. P192 CONNECTOR Connects to left flood and left flight panel light dimmer control on bottom of instrument J144 panel. CONNECTOR Connects to left flood and left flight panel light dimmer control on bottom of instrument P144 panel. CONNECTOR Connects to left fuel quantity indicator at top of instrument panel. J36 CONNECTOR Connects to low oil pressure switch on aft side of firewall forward of engine J155 instruments. CONNECTOR Connects to low oil pressure switch on aff side of firewall forward of engine P155 instruments. CONNECTOR Connects to low vacuum warning light on instrument panel. J1 CONNECTOR Connects to low vacuum warning light on instrument panel. P1 CONNECTOR Connects to moveable door IN TRANSIT light. J94 CONNECTOR Connects to moveable door IN TRANSIT light. P94 CONNECTOR Connects to moveable door motor. J91 CONNECTOR Connects to moveable door motor. P91 CONNECTOR Connects to moveable door relay assembly. J96 CONNECTOR Connects to moveable door relay assembly. P96 CONNECTOR Connects to oil temperature indicator at top of instrument panel. Jib CONNECTOR Connects to oil temperature transmitter on aft end of engine. Ji4 CONNECTOR Connects to ovemeat switch on starter/generator. J150 CONNECTOR Connects to overheat switch on starter/generator. P150 CONNECTOR Connects to percent RPM transmitter on aff end of engine. J134 CONNECTOR Connects to pitot tube heater on left wing. P405 CONNECTOR Connects to pitot tube heater on right wing. P406 CONNECTOR Connects to propeller deice timer on sidewall forward of circuit breaker panel. P43 CONNECTOR Connects to propeller overspeed test valve on left side of engine at forward end. J20 CONNECTOR Connects to propeller RPM indicator at top of instrument panel. J34 CONNECTOR Connects to propeller tachometer generator on right side of engine at forward end. -J33 CONNECTOR Connects to radio and engine instruments light dimmer control on bottom of J143 instrument panel. CONNECTOR Connects to radio and engine instruments light dimmer control on bottom of P143 instrument panel. CONNECTOR Connects to right flood and right flight panel light dimmer control on bottom of Ji45 instrument panel. CONNECTOR Connects to right flood and right flight panel light dimmer control on bottom of P145 instrument panel. CONNECTOR Connects to right fuel quantity indicator at top of instrument panel. J35 CONNECTOR Connects to speed sensor on starter/generator. P25 CONNECTOR Connects to standby alternator control unit on sidewall forward of circuit breaker J81 panel. CONNECTOR Connects to standby alternator ovemeat warning light on pilot’s switch panel. P1100 CONNECTOR Connects to standby alternator relay box on forward side of firewall left of engine. P82 CONNECTOR Connects to strobe light power supplylnavigation light in left wing tip. Pi 11 CONNECTOR Connects to strobe light power supply/navigation light in right wing tip. P110 CONNECTOR Connects to transistor/heat sink light dimmer in sidewall forward of circuit breaker P146 panel. CONNECTOR Connects to transistorlheat sink light dimmer in sidewall forward of circuit breaker P147 panel. CONNECTOR Connects to transistor/heat sink light dimmer in sidewall outboard of circuit breaker P142 panel. COMPONENT INDEX Page 6 Jan 1/2007 O Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR CONNECTOR Connects to turn and bank indicator (or optional turn coordinator) on copilot’s J125 instrument panel. CONNECTOR Connects to tum and bank indicator (or optional turn coordinator) on pilot’s instrument J29 panel. CONNECTOR Connects to volt-ammeter select switch on instrument panel. J26 CONNECTOR Disconnect for door post wire bundle forward of circuit breaker panel. J176 CONNECTOR Disconnect for door post wire bundle forward of circuit breaker panel. J201 CONNECTOR Disconnect for door post wire bundle forward of circuit breaker panel. J61 CONNECTOR Disconnect for door post wire bundle forward of circuit breaker panel. J62 CONNECTOR Disconnect for door post wire bundle forward of ci~uit breaker panel. P176 CONNECTOR Disconnect for door post wire bundle forward of circuit breaker panel. P201 CONNECTOR Disconnect for door post wire bundle forward of circuit breaker panel. P61 CONNECTOR Disconnect for door post wire bundle forward of circuit breaker panel. P62 CONNECTOR Disconnect for vertical tail in top of tailcone forward of canted bulkhead, supplies J84 power to Rashing beacon. CONNECTOR Disconnect for vertical tail in top of tailcone forward of canted bulkhead, supplies P84 power to Rashing beacon. CONNECTOR Door post wire bundle disconnect forward of circuit breaker panel. J54 CONNECTOR Door post wire bundle disconnect forward of circuit breaker panel. P54 CONNECTOR Flap power disconnect above pilot’s door, joins cabin overhead wiring to door post J153 wire bundle. CONNECTOR For air conditioner compressor on engine support. 5104 CONNECTOR For air conditioner compressor on engine support. P104 CONNECTOR For air conditioner pressure switch in engine compartment near receiver/dryer. J3 CONNECTOR For air conditioner pressure switch in engine compartment near receiver/dryer. P3 CONNECTOR For auxiliary fuel pump relay and pressure switch below cabin center Roorboards aff Ji20 of pilot seats. CONNECTOR For auxiliary fuel pump relay and pressure switch below cabin center Roorboards aR P120 of pilot seats. CONNECTOR For beacon light flasher in top of tailcone forward of canted bulkhead. J106- CONNECTOR For beacon light Rasher in top of tailcone forward of canted bulkhead. P106 CONNECTOR For cabin ventilation blower in fresh air duct in leading edge of left wing at inboard J165 end. CONNECTOR For cabin ventilation blower in fresh air duct in leading edge of leff wing at inboard P165 end. CONNECTOR For cabin ventilation blower in fresh air duct in leading edge of n’ght wing at inboard 5164 end. CONNECTOR For cabin ventilation blower in fresh air duct in leading edge of right wing at inboard P164 end. CONNECTOR For cargo pod and landing gear deice relay on inboard end of left wing below deice J182 timer. CONNECTOR For cargo pod deice relay forward of circuit breaker panel. J181 CONNECTOR For cargo pod deice relay forward of circuit breaker panel. P181 CONNECTOR For compass light at top of instrument panel. J172 CONNECTOR For compass light at top of instrument panel. P1 72 CONNECTOR For copilot’s flight instrument panel post lights. J173 CONNECTOR For copilot’s flight instrument panel post lights. P173 CONNECTOR For courtesy light above pilot’s door. J136 CONNECTOR For courtesy light above pilot’s door. P136 CONNECTOR For courtesy light above right cockpit door. J137 CONNECTOR For courtesy light above right cockpit door. P137 CONNECTOR For fire warning muting relay on support bracket for control pedestal. P138 CONNECTOR For fire warning muting relay on support bracket for control pedestal. J138 COMPONENT INDEX Page 7 Jan 1/2007 O Cessna Aircraft Company CESSNA AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR CONNECTOR For float position switches on amphibian gear P304 CONNECTOR For float position switches on amphibian gear. J304 CONNECTOR For fuel select off waming hom above pilot’s door. J149 CONNECTOR For fuel select off warning horn above pilot’s door. J168 CONNECTOR For fuel select off waming horn above pilot’s door. P149 CONNECTOR For fuel select off warning hom above pilot’s door. Pi68 CONNECTOR For leff air conditioner blower between forward and aft wing spars in inboard end of J119 wing. CONNECTOR For left air conditioner blower between forward and aft wing spars in inboard end of P119 wing. CONNECTOR For left pitot heater ammeter on pilot’s instrument panel. J202 CONNECTOR For left pitot heater ammeter on pilot’s instrument panel. J204 CONNECTOR For left pitot heater ammeter on pilot’s instrument panel. P202 CONNECTOR For left pitot heater ammeter on pilot’s instrument panel. P204 CONNECTOR For light in Attitude Gym on copilot’s instrument panel. J26 CONNECTOR For light in Attitude Gyro on copilot’s instrument panel. P26 CONNECTOR For Pumps On Amphibian Gear. J302 CONNECTOR For pumps on amphibian gear. P302 CONNECTOR For reservoir tank low fuel switch in auxiliary fuel pump area below cabin center J124 floorboards aft of pilot seats. CONNECTOR For reservoir tank low fuel switch in auxiliary fuel pump area below cabin center P124 Roorboards aft of pilot seats. CONNECTOR For right air conditioner blower between forward and aft wing spars in inboard end of Ji 18 wing. CONNECTOR For right air conditioner blower between forward and aft wing spars in inboard end of Pii8 wing. CONNECTOR For right pitot heater ammeter on pilot’s instrument panel. J205 CONNECTOR For right pitot heater ammeter on pilot’s instrument panel. J206 CONNECTOR For right pitot heater ammeter on pilot’s instrument panel. P205 CONNECTOR For right pitot heater ammeter on pilot’s instrument panel. P206 CONNECTOR For SEAT BELT/NO SMOKING sign in forward end of cabin. J57 CONNECTOR For SEAT BELT/NO SMOKING sign in forward end of cabin. P57 CONNECTOR For stall warning detector in leading edge of left wing near base of pitot tube. J230 CONNECTOR For stall waming detector in leading edge of left wing near base of pitot tube. P230 CONNECTOR For stall warning horn above pilot’s door. J58 CONNECTOR For stall warning horn above pilot’s door. P58 CONNECTOR For standby alternator overneat switch on engine support at alternator. J308 CONNECTOR For standby alternator overneat switch on engine support at alternator. P308 CONNECTOR For standby alternator power on forward side of circuit breaker panel. J183 CONNECTOR For standby alternator power on forward side of circuit breaker panel. J184 CONNECTOR For standby alternator power on forward side of circuit breaker panel. Ji85 CONNECTOR For standby alternator power on forward side of circuit breaker´•panel. Pi83 CONNECTOR For standby alternator power on forward side of circuit breaker panel. Pi84 CONNECTOR For standby alternator power on forward side of circuit breaker panel. P185 CONNECTOR Fuel tank feedthru connector for left wing fuel tank float switch between forward and J70 aff wing spars on inboard end of CONNECTOR Fuel tank feedthru connector for right wing fuel tank float switch between forward and J93 aft wing spars on inboard end of wing fuel tank. CONNECTOR In electric power box on forward side of firewall left of engine. J212 CONNECTOR In electric power box on forward side of frrewall left of engine. J213 CONNECTOR In electric power box on forward side of firewall left of engine. P212 CONNECTOR In electric power box on forward side of firewall left of engine. P213 CONNECTOR Moveable door power disconnect at forward side of circuit breaker panel. J95 COMPONENT INDEX Page 8 Jan 1/2007 O Cessna Aircraft Company CESSNA.AIRCRAFT COMPANY MODEL 208 WIRING DIAGRAM MANUAL REFERENCE NOMENCLATURE- LOCATION DESIGNATOR P95 CONNECTOR Moveable door power disconnect at forward side of circuit breaker panel. CONNECTOR Panel lights disconnect for removable section of instrument panel. J158 CONNECTOR Panel lights disconnect for removable section of instrument panel. J159 CONNECTOR Panel lights disconnect for removable section of instrument panel. J171 CONNECTOR Panel lights disconnect for removable section of instrument panel. Pi58 CONNECTOR Panel lights disconnect for removable section of instrument panel. P?59 CONNECTOR Panel lights disconnect for removable section of instrument panel. Pi71 CONNECTOR Part of electric power box of forward side of firewall left of engine. JZ25 CONNECTOR Part of electric power box on forward side of firewall left of engine. J7 CONNECTOR Part of fuel select off waming relay assembly in sidewall forward of circuit breaker P210 panel. CONNECTOR Part of standby alternator relay box on forward side of firewall left of engine. J82 CONNECTOR Part of transistorlheat sink light dimmer in sidewall forward of circuit breaker panel. J146 CONNECTOR Part of transistorlheat sink light dimmer in sidewall forward of circuit breaker panel. 5147 CONNECTOR Part of transistor/heat sink light dimmer in sidewall outboard of circuit breaker panel J142 CONNECTOR Pilot’s control wheel disconnect at bottom of instrument panel. JZ12 CONNECTOR Pilot’s control wheel disconnect at bottom of instrument panel. PZ12 CONNECTOR Pilot’s overhead panel disconnect. J169 CONNECTOR Pilot’s over