Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
LIST OF REVISIONS
1.
Effectivity
A.
This Wiring Diagram Manual covers Model 182S and 182T, Airplanes 18280001 and ON and Model T182T, Airplanes
T18208001 and ON.
NOTE:
2.
Revisions
A.
3.
Information in this Wiring Diagram Manual is applicable to U.S. and foreign certified model 182S
and 182T, Airplanes 18280001 and ON and Model T182T, Airplanes T18208001 and ON. Information
unique to a particular country is identified in the chapter(s) affected.
This Wiring Diagram Manual includes the original issue and the following listed revisions. To ensure that information in this
manual is current, the revisions shall be incorporated in to the manual as they are issued.
Original Issue - 3 February 1997
Revision 1 - 1 November 2000
Revision 2 - 18 June 2001
Revision 3 - 1 March 2004
Revision 4 - 13 February 2006
Revision 5 - 1 January 2007
Revision 6 - 1 January 2008
Revision 7 - 1 March 2010
Revision 8 - 1 January 2016
Revision 9 - 1 January 2017
Export Compliance
A.
This publication contains technical data and is subject to U.S. export regulations. This information has been exported from
the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited.
ECCN: 9E991
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 1 of 1
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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INTRODUCTION
1.
General
A.
B.
C.
2.
The information in this publication is based on data available at the time of publication and is updated, supplemented, and
automatically amended by service letters, service bulletins, publication revisions, reissues, instructions for continued
airworthiness (ICA) supplements, and temporary revision, which are issued through subscription services available from
Cessna Customer Services. All such amendments become parts of and are specifically incorporated within this
publication. The latest changes to this publication are given through the Cessna Customer Service subscription services
and/or Citation Service Centers and Citation Service Stations.
The information in this manual has been written for Cessna approved parts. If non-Cessna approved parts are installed,
refer to the manufacturers and/or seller's publications for inspection intervals, replacement time limits, methods of
inspections, life limits, etc.
Inspection, maintenance and parts requirements for Supplemental Type Certification (STC) installations are not included in
this manual. When an STC installation is incorporated on the airplane, those portions of the airplane affected by the
installation must be inspected in accordance with the inspection program published by the owner of the STC. Since STC
installations may change systems interface, operating characteristics and component loads or stresses on adjacent
structures, Cessna provided inspection criteria may not be valid for airplanes with STC installations.
How to Get Customer Assistance
A.
Customer Service
CESSNA CUSTOMER SERVICE
Mailing Address
One Citation Lane
Wichita, KS 67209
(1) If you need assistance with a general support question, publication information, subscriptions, or maintenance
programs visit our website at CessnaSupport.com or contact:
CESSNA CUSTOMER SERVICE
Phone Numbers
Fax
Email Address
316-517-5800
1-800-4Cessna option 2 (1-800-423-7762)
316-517-5802
Customercare@txtav.com
(2) For complex troubleshooting problems or structural repair or support visit CessnaSupport.com.
3.
Coverage
A.
B.
C.
D.
E.
4.
This Cessna Wiring Diagram Manual is prepared with information given by the ATA (Air Transport Association)
Specification Number 2200 for Manufacturer's Technical Data.
Additional information not given in this manual can be found in the Maintenance Manual, Illustrated Parts Catalog,
Structural Repair Manual, Component Maintenance Manual, Nondestructive Testing Manual and Illustrated Tool and
Equipment Manual. For technical aid applicable to this manual, contact Cessna Customer Service.
This manual has been prepared to assist maintenance personnel. This manual provides the necessary information
required to enable the mechanic to troubleshoot, remove and replace components or repair systems.
Technical Publications available from the manufacturers of the various components and systems, which are not covered in
this manual, must be utilized as required for maintenance of those components.
Publications for this model are available in paper and as electronic media. The paper publications are available as
individual publications such as the Maintenance Manual, Parts Catalog, etc. The electronic media service publications are
available in a DVD, download, online and mobile application library that contain multiple books together. These
publications are kept up to date through routine revisions.
Effectivity
A.
This Wiring Diagram Manual covers 182 series 1997 & on.
NOTE:
Information in this Wiring Diagram Manual is applicable to U.S. and foreign certified models.
Copyright © Textron Aviation Inc.
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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5.
Information unique to a particular country is identified in the chapter(s) affected.
List of Effective Pages (Paper version of this manual only.)
A.
6.
Instructions for Continued Airworthiness (ICA)
A.
B.
C.
7.
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.
Wiring Diagram Manual
(1) The instructions provided in the maintenance manual are the principal instructions for continued airworthiness, the
information provided in the wiring diagram manual is also ICA. The wiring diagram manual may be revised to add
changes to the ICAs or to add additional ICAs when changes to the airplane type design require changes to these
instructions. When a revision to this manual is not possible within the time constraints for these ICAs, the instructions
may be transmitted with a temporary revision or with an ICA supplement. Temporary revisions will be incorporated in
the next revision to this manual and ICA supplements will also be incorporated in the next revision unless these
instructions require restricted distribution.
Temporary Revisions
(1) Temporary revisions may be produced to transmit supplemental instructions for continued airworthiness when a
revision to the wiring diagram manual is not possible within the time constraints for these ICAs. They consist of
figures which replace the existing paper and will temporally supersede the electronic data. Temporary revisions will
be included on the next electronic release cycle. Temporary revisions are numbered consecutively in the ATA chapter
assignment.
(2) Paper Version of the Wiring Diagram Manual
(a) Paper temporary revisions will be distributed on yellow paper. File the temporary revision cover sheet after the
title page of the chapter to which it applies and substitute or add the remaining pages in the paper manual.
(3) Electronic Version of the Wiring Diagram Manual
(a) The cover sheet will be located in the wiring diagram manual electronic library at the beginning of the chapter to
which it applies and the changed or added figures will be located in the appropriate location by ATA.
ICA Supplements
(1) ICA supplements may be produced to transmit supplemental instructions for continued airworthiness when a revision
to the affected manuals is not possible within the time constraints for these ICAs. ICA supplements will provide
supplemental instructions for one or more ICA manual and is to be used in conjunction with the affected manuals
(maintenance manual, wiring diagram manual, etc.) until those instructions are incorporated into the manuals. ICA
supplements are numbered consecutively by model in the ATA chapter assignment. All wiring diagram figures that
are revised or added will be located in Appendix B of the ICA supplement.
(2) Refer to the ICA Supplement List to determine the incorporation status for each manual affected.
Revision Filing Instructions (Paper Version of this Manual Only)
A.
B.
Regular Revision.
(Paper version of this manual only.)
(1) Refer to the List of Effective pages of each chapter while inserting a revision.
(2) Pages changed by the revision will be indicated by the revision date on the page and on the List of Effective pages
for that chapter. The revised page replaces the existing page in the manual.
(3) New pages added to the manual are indicated by "Added" on the List of Effective pages. Pages are inserted in the
manual in sequence by chapter/section/subject and page number.
(4) Existing pages no longer needed in the manual are indicated by "Deleted" on the List of Effective pages. These
pages are to be removed and discarded. When a page has been deleted by a revision, the List of Effective pages for
subsequent revisions does not list the page.
Temporary Revisions:
(Paper version of this manual only.)
(1) File temporary revisions in the applicable chapter in accordance with filing instructions that appear on the title page.
(2) Temporary revisions should be removed from the manual only when replaced by a revision to the manual or by
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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instructions noted on the superseding temporary revision.
8.
Identifying Revised Material
A.
B.
9.
Regular Revision
(1) Text Pages
(a) Additions, deletions or revisions to text pages in an existing section will be identified by a revision bar in the left
margin of the page adjacent to the change. The current revision date for that section will show in the lower right
corner of the section, below the page number.
(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 the current regular revision date.
(c) When large technical changes are made to text in a section, a revision bar will be shown the full length of the text.
(2) Wiring Diagram Figures
(a) Revisions to wiring diagram figures are identified by the revision date in the lower right corner below the page
number. The revised information is listed in the effective pages as added, revised or deleted.
(3) Parts Lists
(a) Revisions to parts list pages are identified by an "R" in the right margin of the parts list and the revision date in
the lower right corner below the page number.
Electronic Manual
(1) Text
(a) Additions or revisions to text in a section will have a teal background to show the revised text. The current
revision number for the manual will show in parenthesis in the upper right corner of the page adjacent to the title
of the manual. The revision number for that section will show in parenthesis in the upper left corner of the page
adjacent to the chapter-section-subject.
(2) Parts Lists and Wiring Diagram Figures
(a) Revisions to a parts list are identified by an "R" in the right margin of the parts list. The current revision number
for the manual will show in parenthesis in the upper right corner of the parts list adjacent to the title of the manual.
The revision number for that parts list and figure will show in parenthesis in the upper left corner of the page
adjacent to the chapter-section-subject.
Manual Usage
A.
B.
Purpose.
(1) This Wiring Diagram Manual has been prepared by Cessna Aircraft Company to assist customer personnel in
locating, tracing and repairing of aircraft wiring and components. The wiring diagram manual may also be used to
assist in ordering replaceable wiring components and in identifying new and reclaimed parts. It is not approved for
any other purpose.
Effectivity.
(1) Due to limited space on the parts list, the effectivity is listed under the title and includes the model number. Effectivity
within the top effectivity is listed in a parts column and does not include the model number of a serial.
EXAMPLE: 80001 - 80004 would indicate the part listed is applicable to serial numbers 18280001 thru
18280004. 8001 - 8004 would indicate the part listed is applicable to serial numbers T18208001
- T18208004.
C.
(2) Airplane effectivity is indicated in the parts list by a ten-character alphanumeric code. The first five characters indicate
the first applicability and the last five characters indicate the last applicability on an unbroken sequence of assigned
airplanes. When an item is applicable to all airplanes, the column shall be left blank.
(3) Avionic configurations are standard avionics package, NAV I option, NAV II option, or NAV III. Sections of this wiring
diagram manual that are unique to a specific avionics configuration are listed as STANDARD, NAV I, NAV II, or NAV
III.
Identification Procedures.
(1) Wiring Diagram Manual Numbering.
(a) Numbering of chapters, sections and subjects within the Wiring Diagram Manual is in accordance with ATA
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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Specification 100. This same numbering system is utilized in the Illustrated Parts Catalog and Maintenance
Manual to allow for easy cross- referencing between the three books. Refer to Figure 1 for an example of the
numbering system.
A2005
Chapter/System
(Fuel)
28−21−01
Subject/Unit
(Fuel Boost Pump)
Section/Subsystem
(Distribution)
Figure 1
(2) Wiring Diagram Page Numbering.
(a) Page numbers 0 thru 100 are used to number wiring diagrams. Sheet numbers are used for diagrams that
require more than one page for illustration.
NOTE:
D.
Whenever a diagram is referenced to another, only the diagram number is used.
Therefore, where there is more than one page of the same diagram, it is necessary to refer
to the effectivity block at the top of the parts list to make certain the diagram applies to the
airplane of interest.
Wire Identification and Numbering.
(1) In each electrical and electronic wiring circuit, the wires are identified by a number-letter code. The code is either
printed, stenciled or banded on each wire segment. A wire segment is a run of wire between two points in a circuit.
The number-letter code explains where the wire is used. Refer to Figure 2 for the wire identification system.
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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Figure 2
(2) Thermocouple leads are banded for identification and are color coded as shown in Table 1.
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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Table 1. Thermocouple Color Coding
E.
Color Coding
Wire Material
Red
Alumel
Yellow
Chromel
Parts List.
(1) Electrical and electronic equipment used in the wiring diagrams are identified by an alphanumeric reference
designator. This reference designator is used as a cross-reference to the parts list where the part number and part
description are shown. The five digit Federal Supply Code may be found in the Suppliers Address List to find the
suppliers name and address.
(2) Most reference designators consists of two (2) alphabetical characters followed by three (3) numeric characters.
(a) The first alphabetical character denotes component type.
Table 2. First Alphabetical Character
A=
Splice
B=
Controller
C=
Capacitor
D=
Diode
E=
Instrument
F=
Light
G=
Ground
H=
Circuit Breaker, Fuse, Bus Bar
J=
Connector (Jack, Receptacle)
K=
Relay
L=
Inductor
M=
Servo Motor
N=
Logic
P=
Connector (Plug)
Q=
Transistor
R=
Resistor
S=
Switch
T=
Thermal Element
U=
Unit, Module
V=
Solenoid Valve
W=
Solenoid
V=
Junction Block
Z=
Cessna Assembly
(b) The second alphabetical character denotes general location in the airplane.
Table 3. Second Alphabetical Character
A=
Aft Bulkhead
B=
Firewall
C=
Left Fuselage
F=
Right Fuselage
G=
Landing Gear
H=
Horizontal Stabilizer
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I=
L=
M=
N=
R=
S=
W=
V=
Z=
F.
G.
H.
I.
J.
K.
L.
Instrument Panel
Left Wing
Left Wing Feedthru
Nose
Right Wing
Right Wing Feedthru
Tailcone
Vertical stabilizer
Inside a Cessna Assembly
(c) The three (3) numeric characters are sequentially assigned and do not denote location or order of occurrence.
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.
Alphabetical Indexes.
(Paper version of this manual only.)
(1) The Alphabetical Index lists subjects and components in this manual.
(2) The Component Index lists each component and its location in the airplane. The components are cross- referenced to
the reference designator and applicable chapter, section, subject where the component will be found.
Reference Designator Index
(Paper version of this manual only.)
(1) The Reference Designator Index is a complete listing of all parts included in the parts list. All reference designators
are cross-referenced to the part number and applicable chapter, section, subject and figure where the reference
designator is used.
Part Number Indexes.
(Paper version of this manual only.)
(1) The Alpha and Numeric Part Number Indexes are a complete listing of all parts included in the parts list. All part
numbers are cross- referenced to the reference designator and applicable chapter, section, subject and figure where
the part number is used.
Chapter 20.
(1) Chapter 20 has safety precautions and general maintenance information for wire repairs, grounding of wires ,
soldering, heat shrink tubing, resistors, torque values and connectors.
Chapter 91.
(1) Chapter 91 has reference information for connectors, ground locations and component locations.
(a) Connector charts are provided for those connectors that contain wires for several different systems. The wire
number for each wire to a pin is shown with reference to the system where the complete circuit will be found.
How To Use This Manual.
(1) All operable electrical components, such as relays, etc., are shown with the airplane on the ground, all circuits off or
de-energized and no electrical power on the circuits. Switches are shown in the off or normal position unless
otherwise noted.
(2) The parts list may consist of two or more text lines. Make certain that all lines are observed, as the part number and
part description are not always complete on the first line.
(3) Some wire diagrams have too many parts to list on one page of text. In this case, identical wire diagrams are used
with a different parts list for each diagram.
(4) Letters or numbers are used to identify the contacts of a connector.
(a) The letter or number shown on the wiring diagram is also marked on the connector.
(b) On wire diagrams, a letter that is underlined or preceded by an asterisk indicates a lower case letter, but both
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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are identified lower case on the connector.
10. Manufacturer's Names and Addresses
A.
Refer to the Suppliers Address List page for manufacturers names and addresses.
11. Service Bulletins
A.
B.
A record of service bulletins are listed in the service bulletin list.
The list of service bulletins summarizes the following information:
(1) Service Bulletins Number - Service bulletins are numbered by ATA chapter number followed by a sequential number
with at least two digits, starting with number one (01).
(2) Service Bulletin Date - The service bulletin date is the printing date of the service bulletin.
(3) Manual Incorporation Date - This indicates how the service bulletin affects the manual:
(a) Date - This indicates when the service bulletin information was incorporated into the manual
(b) No Effect - This indicates the service bulletin does not affect the manual.
(c) Other self-explanatory statements may appear (i.e., replaces, replaced, superseded, etc.).
(4) Title - The title identifies the service bulletin by nomenclature, it is the same title on page one of the service bulletin.
12. Symbols
A.
Refer to Electrical Symbols Figure 3. for examples of symbols used in this wiring diagram manual.
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Figure 3 : Sheet 1 : Electrical Symbols
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Figure 3 : Sheet 2 : Electrical Symbols
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Figure 3 : Sheet 3 : Electrical Symbols
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Figure 3 : Sheet 4 : Electrical Symbols
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Figure 3 : Sheet 5 : Electrical Symbols
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ZONE NUMBERING SYSTEM
1.
Zoning Diagrams - Description
A.
General
(1) Numbered zones provide a method for locating components. The zones are identified by a three-digit number. Each
digit designates a zone category: major, submajor or subdivision. Refer to Figure 1.
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Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
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Figure 1
B.
(2) Major Zones
100 - Forward side of firewall and forward.
200 - Aft side of firewall to forward side of aft bulkhead.
300 - Aft side of aft bulkhead to end of airplane
500 - Left wing
600 - Right wing
700 - Landing gear.
(3) Submajor Zones. The second digit of the three-digit number designates a further delineation of a particular area of
the major zone.
(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.
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.
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Figure 2 : Sheet 1 : Airplane Zones
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Figure 2 : Sheet 2 : Airplane Zones
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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.
LIGHT
AIRCRAFT IDENTIFICATION
BEACON
CENTER PEDESTAL
COMPASS
COPILOT DOME
GLARESHIELD
GREEN
LANDING
LANDING
LED
LED
LEFT COURTESY
LEFT NAVIGATION (RED)
LEFT NAVIGATION (RED)
LEFT STROBE
LEFT STROBE
LOWER PEDESTAL
PILOT DOME
PILOT'S DOME LED
PILOT'S DOME LED
REAR DOME
REAR DOME LED
REAR DOME LED
RIGHT COURTESY
RIGHT NAVIGATION (GREEN)
RIGHT NAVIGATION (GREEN)
RIGHT STROBE
RIGHT STROBE
TAXI
TAXI
UPPER PEDESTAL
REFERENCE
DESIGNATOR
FI008
FV002
FI005
FC001
FC003
FI002
FI011
FL002
FL002
FF004
FC012
FL004
FL006
FL003
FL005
FL007
FI004
FC002
FC006
FC006
FC005
FC007
FC007
FR002
FR004
FR001
FR005
FR003
FL001
FL001
FI003
AIRPLANE
ZONE
BULB
QUANTITY
BULB PART NUMBER
340
210
340
211
211
211
211
01
01
01
01
01
01
01
01
01
01
01
01
01
01
01
01
01
02
01
01
01
01
01
01
01
01
01
01
01
01
01
01
S3284-1
721-1074-002
02-0350433-01
S1899-4
MS25237-327
4595-1
7300248-2
S2800-679
34-0750692-00
34-0750692-00
1864
1864
MS15584-8
01-0770082-12
C622001-0201
C622003-0101
01-0770818-00
MS25231-1829
4595-1
RL6870-1
RL6870-1
4596-1
RL3870-1
RL3870-1
MS15584-8
01-0770082-13
C622001-0201
01-0770818-00
C622003-0101
34-0750707-00
34-0750707-00
MS25231-1829
520
520
510
520
520
520
520
211
211
211
211
211
211
211
610
620
620
620
620
520
520
211
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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.
NAME
CIRCUIT
LOCATION
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AIRPLANE ZONE
PART NUMBER
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SERVICE BULLETIN LIST
1.
General
A.
The Service Bulletin List provides the service bulletin number, title and date. If a service bulletin has been revised, the
revision number is listed. If a service bulletin has been included in this manual, the manual revision date is given.
Service
Bulletin
SB08-11-01
SB02-11-01
Revision
Service Bulletin Title
Service Bulletin Included In
Date
Manual
1
May 26/2008
Jan 21/2002
No Effect
No Effect
SB07-11-01
SB06-11-01
SSP04-11-01
SB97-11-02
SB03-11-02
SB07-11-02
1
Jun 25/2007
Mar 27/2006
Feb 2/2004
Jul 1/1997
Jan 21/2002
Oct 22/2007
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
SB08-11-02
SSP04-11-02
1
Pilot's Operating Handbook and Checklist Revisions
Pilot's Operating Handbook and Pilot's Checklist
Revisions
Electronic Pilot's Checklist Availability
Pilot's Operating Handbook Revisions
Airplane Identification Data Plate Inspection/Replacement
Pilot's Operating Handbook Revision
Pilot's Operating Handbook Revision
Pilot's Operating Handbook - AmSafe Aviation Inflatable
Restraints
Electronic Pilot's Checklist
Pilot's Operating Handbook and Pilot's Operating
Handbook Supplement 3 Revision
Pilot's Operating Handbook Revisions
German Pilot's Operating Handbook and Pilot's Checklist
Revisions
NAV III Pilot's Checklist
Pilot's Operating Handbook and Checklist Revisions
Autopilot Limitation Placard Installation and Control Cable
Tension Inspection
AP Limitations Placard Installation/Control Cable Tension
Inspection
Muffler Inspection Placard Installation
Altimeter Certification Logbook Entry Verification
Pilot's Operating Handbook and Pilot's Checklist
Revisions
Brazilian POH Revision
Brazilian Pilot's Operating Handbook Revision
Firewall Sealant Replacement
Fresh Air Vent Replacement
Garmin Autopilot GSM 85 Servo Gearboxes Inspection
Honeywell KAP 140 Autopilot System Modification
KAP-140 Dual Axis Autopilot Modification
KC 140 Autopilot Computer Inspection
Autopilot Circuit Breaker Extension Cap Installation
Honeywell KS270C Pitch Servo and KS271C Roll Servo
Tach Generator Modification
Honeywell KAP 140 Autopilot System Modification
Trim Servo Cable Chain Inspection
Aug 18/2008
Jul 5/2004
No Effect
No Effect
Jul 29/2005
Sep 27/1999
No Effect
No Effect
Aug 30/2004
May 4/1998
Sep 21/1998
No Effect
No Effect
No Effect
Sep 21/1998
No Effect
Aug 24/1998
Dec 15/1997
Dec 26/2000
No Effect
No Effect
No Effect
Oct 12/1998
Oct 12/1998
Dec 31/1998
Mar 15/1999
Jun 4/2007
Feb 14/2000
May 18/1998
Sep 16/2002
Sep 13/2004
Apr 24/2006
No Effect
No Effect
No Effect
No Effect
No Effect
Apr 5/2004
No Effect
No Effect
No Effect
No Effect
Nov 25/2002
Dec 5/2005
No Effect
No Effect
SB05-11-02
SB99-11-02
SB04-11-03
SB98-11-03
SB97-11-03
1
SB00-11-03
1
SB98-11-04
SB97-11-05
SB00-11-05
SB00-11-07
SB98-11-07
SB98-20-01
SB99-21-01
SB07-22-01
SB00-22-01
SB98-22-01
SSP02-22-01
SB04-22-01
SB06-22-01
1
SB02-22-01
SB05-22-01
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 1 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
SB10-22-01
SB97-22-01
SB07-22-02
SB98-22-02
SB05-22-02
SB03-23-01
SB04-23-01
SB98-24-01
SB04-24-01
SB03-24-01
SB05-24-01
2
SB99-24-01
SB06-24-01
SB00-24-01
SB02-24-01
SEB-24-01
SSP06-24-01
SB11-24-02
SB03-24-02
SEB-24-02
SB00-24-02
SB97-24-02
SB06-24-02
SB99-24-02
SB06-24-03
SB09-24-03
SB06-24-04
SB06-24-05
SB04-25-01
SB02-25-01
SB98-25-01
SB01-25-01
SB07-25-01
1
4
Removal of the Autopilot Flight Control System (AFCS)
Placard
Bendix/King Autopilot Flight Computer Modification
GFC-700 Autopilot Flight Control System (AFCS) Placard
Installation
KAP-140 Dual Axis Autopilot Limitation
Honeywell KAP-140 Autopilot Software Modification
Honeywell KMA 26 Audio Panel Modification
Garmin GIA 63 Inspection/Modification
Alternator Replacement
Alternator Control Unit Inspection/Replacement
Alternator Replacement
MC01-3A Main Electrical Power Junction Box Circuit
Breakers Inspection
Electrical Power System Modification
Electrical Ground Strap Inspection
Main Power Junction Box Circuit Breaker Retrofit Kit
Installation
Electrical Power System Modification
Transmittal of Lamar Technologies LLC Service
Information Letters LSI-019 Revision A and LSI-021
(Mandatory Inspection and Compliance)
95 Ampere Alternator Installation
Avionics Switch Inspection and Replacement
MC01-3A Main Electrical Power Junction Box Modification
Transmittal of Lamar Technologies LLC Service
Information Letters LSI-019 Revision A and LSI-021
(Mandatory Inspection and Compliance Upon Initial
Replacment of the X61-0007 Alternator Contactor with the
X61-0029 Alternator Contractor)
Electrical Panel Wiring Modifications
Electrical Wire Bundle Routing Inspection and Modification
60 Ampere Alternator Rotor Replacement
Circuit Panel Assembly Cover Installation
60 Ampere Alternator Brush Replacement
Alternator Ring Terminal Inspection/Replacement and
Field/Stator Connector Inspection
Circuit Breaker Inspection
Circuit Breaker Panel Assembly Inspection
Crew Seat Recline Modification
Pilot and Copilot Shoulder Harness Guide Removal
Pilot and Copilot Seatback Inspection/Modification
Glareshield Shroud Installation
Inflatable Seat Restraints Wiring Connector Strain Relief
Installation
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Mar 15/2010
No Effect
Oct 6/1997
Nov 21/2007
No Effect
No Effect
Feb 1/1999
Dec 5/2005
Jul 28/2003
Sep 13/2004
Mar 30/1998
Mar 1/2004
Jul 28/2003
Jan 31/2005
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Mar 15/1999
May 8/2006
Mar 13/2000
No Effect
No Effect
No Effect
Mar 15/1999
Oct 7/2014
No Effect
No Effect
Nov 20/2006
Jul 22/2011
Oct 13/2003
Oct 27/2014
No Effect
No Effect
No Effect
No Effect
Jun 5/2000
Dec 22/1997
Dec 26/2006
Dec 27/1999
Dec 18/2006
Oct 26/2009
Nov 1/2000
No Effect
No Effect
No Effect
No Effect
No Effect
Dec 26/2006
Dec 26/2006
Dec 26/2006
Apr 29/2002
Jun 1/1998
Dec 24/2001
Jan 29/2007
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Page 2 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
SB10-25-01
SB08-25-01
SB05-25-01
SB09-25-01
SB99-25-01
SB05-25-02
SB04-25-02
SB98-25-02
SSP99-25-02
1
SB07-25-02
SEB-25-02
SB07-25-03
2
1
1
1
2
SB04-25-04
SB07-25-04
SB07-25-05
SB97-26-01
SSP09-27-01
SB00-27-01
SSP05-27-01
SB08-27-01
SB07-27-01
SB04-27-01
SSP03-27-01
SB03-27-01
SB99-27-01
SEB-27-01
SB06-27-01
SB00-27-02
SB03-27-02
SB11-27-03
SB98-27-04
SB98-27-06
SB98-28-01
1
1
2
2
1
1
SSP05-28-01
SB03-28-01
SSP08-28-01
SB05-28-01
SB99-28-01
AmSafe Aviation Inflatable Restraint Connector Cover
Installation
CO Detector Inspection
Inflatable Seat Belt Restraint Installation Inspection
Crew Seat Height Adjustment Nut Inspection
Emergency Locator Transmitter (ELT) Operational Test
Inflatable Seat Restraints Installation
Crew Seat Back Cylinder Lock Installation Modification
Pilot and Copilot Seat Roller Bushing Inspection
Crew and Passenger Seat Restraint Systems
Replacement
Crew Seat Base Inspection and Modification
Armsafe EMA Installation Modification
Garmin G1000 Arrival and Departure Procedures
Software Alert
Crew Seat Back Cylinder Lock Installation Crew Seat
Back Cylinder Lock Control Inspection/Adjustment
Seat Base/Back Attach Fitting Modification
AmSafe Inflatable Restraints Hose Plug Inspection
Fire Extinguisher Mounting Bracket Inspection
Rudder Pedal Cotter Pin Inspection
Lower Forward Elevator Control Cable Pulley Brackets
Inspection
Flight Controls Inspection
Copilot Rudder Pedal Pin Inspection
Elevator Trim Tab Actuator Assembly Inspection
Elevator Rivet Inspection
Elevator Control Cable Turnbuckles Inspection
Flap Actuator Motor Inspection
Control Yoke Pivot Bolt Inspection/Replacement
Control-Column Internal Glide Attach-Screw Installation
Flap Aft Roller Bearing Installation Modification
Aileron Control Cable Quadrant Inspection/Modification
Flap Control Bracket Attach Bolts Replacement
Flap Motor Housing Inspection
Control Column Internal Slide Attach Screw Inspection
Flight Control Cables and Travel Inspection
Engine Fuel Pressure Transducer Inspection and
Replacement
Fuel Quantity Sending Unit Inspection
Fuel Cap Lanyard Removal
Fuel Level Sensor Inspection
Fuel Strainer Gasket Inspection
Wing Fuel Tank Vent Check Valve Inspection
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Jan 11/2010
No Effect
Mar 10/2008
Mar 7/2005
Feb 23/2009
Dec 27/1999
Feb 13/2013
Jun 5/2006
Sep 14/1998
Sep 27/1999
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Apr 23/2007
Oct 27/2014
Mar 12/2007
No Effect
No Effect
No Effect
Oct 11/2004
No Effect
Apr 23/2007
Nov 19/2007
Dec 22/1997
Jun 15/2009
Aug 28/2000
No Effect
No Effect
No Effect
No Effect
No Effect
Mar 4/2005
Jan 28/2008
May 12/2007
Sep 13/2004
Nov 10/2003
Sep 29/2003
Jul 12/1999
Apr 20/2012
Apr 10/2006
Nov 06/2000
Dec 22/2003
Jun 21/2011
Nov 11/1998
Jun 15/1998
Mar 2/1998
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Jan 17/2005
Oct 27/2003
Sep 1/2008
Jan 17/2005
Apr 26/1999
No Effect
No Effect
No Effect
No Effect
No Effect
Page 3 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
SB02-28-01
SB08-28-01
SB04-28-02
SB11-28-02
SB97-28-02
SB01-28-04
SB06-32-01
SB99-32-01
SB03-32-01
SEB-32-01
SB09-32-02
SEB-32-02
SB02-33-01
SB05-33-01
1
1
SB97-33-01
SB97-34-01
SB03-34-01
1
SB06-34-01
SB02-34-01
SB00-34-01
SB98-34-01
SSP04-34-01
SB07-34-01
SB99-34-01
SB11-34-01
SEB-34-01
SB01-34-01
SB04-34-01
SB05-34-01
SB06-34-02
SB07-34-02
SSP04-34-02
SB08-34-02
SB05-34-02
SB04-34-02
SB97-34-02
SB03-34-02
1
1
2
1
1
1
1
1
1
1
Fuel Line Inspection
Fuel Lines Guard Installation
Fuel Strainer Installation Inspection
Fuel Hose Inspection
Fuel System Under Wing Vent Inspection and Adjustment
Fuel Quantity Level Sender/Transmitter Inspection
Brake Master Cylinder Covers Inspection
Brake Pad Torque Plate Inspection
Nose Landing Gear Wheel Fairing Modification
Break Line Inspection
Brake Lines Inspection
Nose Gear Strut Tube Assembly
Light Dimming Resistors Inspection/Modification
High Intensity Discharge (HID) Landing and Taxi Light
Installation
Light Dimming Module Resistor Installation Inspection
KLN 89B Navigation System Approach Restriction
Honeywell KS 270C, KS 271C and KS 272C Servo
Friction Inspection
Honeywell KT 73 Mode S Transponder Installation
Goodrich WX-500 Weather Mapping Sensor Modification
Pitot Tube Heater Assembly Insulation Installation
KLN 89B GPS Navigation System IFR Non-Precision
Approach Limitation
Garmin GIA 63 Outside Cover Replacement
Garmin G1000 NAV III Avionics ChartView Option
KLN 89B GPS Navigation System Modification
Garmin G1000 System Software Upgrade to 0563.21 for
Airplanes Equipped with Nav III and WAAS
Garmin G1000 Enhanced Search and Rescue Enablement
COM Antenna Replacement
Marker Beacon Placard Installation
Garmin G1000 System Software Upgrade
Garmin G1000 System Software Upgrade
Garmin G1000 System Software Upgrade to Version
563.03
Marker Beacon Placard Installation
Alternate Static Source Selector Valve Inspection
Garmin GMA 1347 Audio Panel Modifications
Vertical Navigation Placard Installation
Alternate Static Source Valve Inspection
Altimeter Inspection
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Dec 16/2002
Jan 28/2008
May 10/2004
May 24/2011
Nov 17/1997
Oct 1/2001
Sep 25/2006
May 10/1999
Sep 29/2003
Jun 21/2012
Aug 31/2009
Jan 14/2013
Dec 14/1998
May 9/2005
No Effect
No Effect
No Effect
No Effect
No Effect
Apr 5/2004
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Dec 14/1998
Jul 2/1997
Oct 27/2003
No Effect
No Effect
No Effect
Feb 27/2006
Nov 25/2002
Apr 10/2000
Aug 3/1998
No Effect
Apr 5/2004
No Effect
No Effect
Jul 19/2004
Oct 19/2009
Apr 24/2000
Feb 15/2011
No Effect
No Effect
No Effect
No Effect
Mar 22/2012
Sep 3/2001
Nov 22/2004
Jan 31/2005
Nov 6/2006
Aug 13/2007
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Dec 1/2004
Oct 6/2008
Feb 14/2005
Dec 27/2004
Dec 22/1997
Feb 16/2004
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Page 4 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
SEB-34-02
SB05-34-03
SB07-34-03
SB08-34-03
2
1
1
SEB-34-03
SB06-34-03
1
SB06-34-04
SEB-34-04
SB08-34-04
SB07-34-04
1
SB05-34-04
SB05-34-05
SB07-34-05
SB09-34-05
SB07-34-06
SB05-34-06
SB09-34-06
SB09-34-07
SB07-34-07
SB05-34-07
SB09-34-08
SB07-34-08
SB05-34-08
SB09-34-09
SB05-34-09
SB05-34-10
SB05-34-11
Garmin G1000 System Software Upgrade to Version
0563.26 for Airplanes Equipped with Nav III (WAASEnabled Instalation Only)
Garmin GIA 63 Integrated Avionics Unit Modification
Traffic Advisory System (TAS) Installation
Forward Looking Terrain Avoidance (FLTA) Alert Over the
Open Ocean/Sea
Garmin G1000 System Software Upgrade to Version
0563.26 for Airplanes Equipped with Nav III (non-WAAS
Instalation Only)
Enablement of Garmin G1000 Terrain Awareness Warning
System Class-B (TAWS-B)
Automatic Direction Finder (ADF) and Distance
Measuring Equipment (DME) Installation
EVS Installation
Garmin G1000 GDC-74A Air Data Computer Inspection
Garmin G1000 NAV III FliteCharts and SafeTaxi
Availability
Garmin GIA 63 Integrated Avionics Unit Modification
Garmin G1000 System Software Upgrade
Garmin G1000 Search and Rescue Enablement
Garmin G1000 System Software Upgrade to 563.14 for
Airplanes Equipped with NAV III and GFC 700 AFCS
Autopilot
Garmin G1000 GRS-77 Attitude and Heading Reference
System (AHRS) Inspection/Replacement
Garmin G1000 System Software UpgradeGarmin G1000
GDL-69A Weather and Digital Audio Entertainment
Interface Installation
Garmin G1000 System Software Upgrade to 563.14 for
Airplanes Equipped with NAV III and Honeywell KAP-140
Autopilot
Garmin G1000 Synthetic Vision Technology (SVT)
Installation
Garmin G1000 GPS/WAAS Installation
Garmin G1000 Obstacle and Terrain Avoidance System
Database Update
ADF Bezel Inspection
Garmin G1000 GTX 33 Transponder
Inspection/Replacement
Garmin G1000 System Software Upgrade
GDU 104X CRS/BARO Knob Inspection
Garmin G1000 GDL-69A Weather and Digital Audio
Entertainment Interface Installation
Aft Avionics and Electrical Wire Bundle Inspection
Garmin GIA 63 Integrated Avionics Unit Outside Cover
Replacement
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Mar 13/ 2013
No Effect
Feb 14/2005
Aug 13/2007
May 26/2008
No Effect
No Effect
No Effect
Mar 27/ 2012
No Effect
Jul 23/2007
No Effect
Oct 23/2006
No Effect
Aug 23/2012
Jul 28/2008
Jul 23/2007
No Effect
No Effect
No Effect
Apr 25/2005
Jul 29/2005
Nov 5/2007
Jun 22/2009
No Effect
No Effect
No Effect
No Effect
Nov 19/2007
No Effect
Jul 29/2005
No Effect
Jun 22/2009
No Effect
Jun 22/2009
No Effect
Apr 26/2011
Sep 26/2005
No Effect
No Effect
Aug 10/2009
Dec 17/2007
No Effect
No Effect
Sep 26/2005
Nov 9/2009
Sep 26/2005
No Effect
No Effect
No Effect
Nov 21/2005
Nov 21/2005
No Effect
No Effect
Page 5 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
SB05-34-12
SB03-37-01
SB98-37-01
SB99-37-01
SB00-37-01
1
SB05-37-01
SB02-37-01
SB04-37-02
SB02-37-02
SB02-37-03
SB02-37-04
SB06-52-01
SB04-52-01
SB02-52-01
SSP97-53-01
SB99-53-01
SB00-53-01
SSP09-53-01
SB06-53-01
SB02-53-01
SB07-53-01
SB03-53-01
SB05-53-02
SB04-53-02
SB99-53-02
SB03-53-03
SB04-53-03
SB99-55-01
SB02-55-01
SB98-55-03
SB05-57-01
SSP08-57-01
SSP04-57-02
SB06-71-01
SB05-71-01
SB07-71-01
1
1
1
1
1
1
1
Garmin G1000 Display Unit (GDU) 1040 Cover Glass
Delamination
Vacuum Manifold Inspection/Replacement
Airborne Vacuum Pump Inspection
Vacuum Hose Modification
Vacuum System Air Filter Element
Inspection/Replacement
Vacuum Pump Inspection/Replacement
Vacuum System Reducer Fitting Replacement
Dry Vacuum Pump and Coupling Replacement
Requirements
Dry Vacuum Pump and Coupling Replacement
Requirements
Vacuum System Reducer Fitting Replacement
Airborne Air and Fuel Products Check Valve Manifold
Inspection
Cabin Door Modification
Security Lock Installation
Cabin Door Handle Replacement
Lower Forward Doorpost Fastener Installation
Firewall Doubler Inspection and Engine Cowl Shock Mount
Installation
Center Cabin Rivet Inspection/Installation
Tunnel Bulkhead Rivet Inspection
Fuselage Stringer Rivet Inspection
Fuselage Ballast Weight Installation
Firewall Sealant Inspection
Aft Cabin Stringer Inspection
Tunnel Bulkhead Rivet Inspection
Firewall Doubler Flange Modification and Shock Mount
Inspection
Tailcone Skin Installation Inspection
Nose Landing Gear Fairing Attachment Inspection
Forward Door Post Bulkhead Washer Inspection
Horizontal Stabilizer Abrasion Boot Installation
Elevator Rivet Installation
Horizontal Stabilizer Forward Inboard Rib to Spar Gap
Inspection
Wing Trailing Edge Rib Inspection
Wing Tip Closeout Installation Inspection
Wing Rib Inspection/Modification
Engine Crankshaft Retirement
Engine Crankshaft Replacement
Engine Compartment Fuel Hoses Security Inspection
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Dec 5/2005
No Effect
Nov 10/2003
Mar 8/1999
Dec 27/1999
Aug 14/2000
No Effect
No Effect
No Effect
No Effect
Nov 7/2005
Jan 21/2002
Feb 18/2002
No Effect
No Effect
No Effect
Feb 18/2002
No Effect
Feb 18/2002
Oct 28/2002
No Effect
No Effect
Mar 27/2006
Jun 28/2004
Jan 21/2002
Nov 30/1998
Mar 8/1999
No Effect
No Effect
No Effect
No Effect
No Effect
Aug 14/2000
Jun 15/2009
Apr 16/2007
Sep 2/2002
Feb 12/2007
May 26/2003
Sep 12/2005
Apr 11/2005
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Apr 26/1999
May 15/2004
Oct 11/2004
Apr 16/1999
Oct 14/2002
Nov 30/1998
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Oct 10/2005
May 19/2008
Aug 30/2004
May 8/2006
Jul 18/2005
Mar 16/2007
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Page 6 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
SSP97-71-01
SB04-71-01
SB99-71-01
SB97-71-01
SB04-71-02
SB11-71-02
SB98-71-02
SB06-71-02
SB03-71-02
SB99-71-02
SB07-71-02
SB07-71-03
SB01-71-03
SB02-71-03
SB02-71-04
SB07-71-04
SB02-71-05
SB99-71-05
SB03-73-01
SB08-73-01
SB00-73-01
SSP11-73-01
SB99-73-01
SB01-73-01
SB04-73-01
2
1
2
1
1
2
1
1
2
SB05-73-01
SB10-73-02
SB99-73-02
SB08-74-01
SB01-74-01
SB07-77-01
SB97-78-01
SB97-78-02
SB98-78-02
SB98-78-03
SSP98-78-03
SB00-79-01
SB07-79-01
1
1
1
Engine Crankcase Overboard Breather Tube Modification
Engine Cowl Flap Rivet Inspection
Engine Piston Pin Plug Wear Inspection
Alternate Air Door Hinge Assembly Replacement
Engine Starter Inspection/Replacement
Fuel Drain Valve Adapter Replacement
Engine Air Filter Replacement
Engine Compartment Fuel Hoses Security Inspection
Fuel Injection Servo Inspection
Engine Oil Filler Tube to Engine Mount Clearance
Pressurized Magneto Pressure Test
Cylinder Stud Hole Inspection
Engine Turbocharger Mounting Bracket Bolt Replacement
Engine Crankshaft Gear Retaining Bolt Replacement
Engine Induction System Fuel Overboard Drain Relocation
Incorrect Cylinder Assemblies Shipped with Cylinder Kits
Engine Oil Pump Plug Inspection
Engine Valve Seat Inspection
Throttle Arm Retention Inspection
Engine Fuel Injector Servo Hex Plug Inspection
Engine Fuel Injection Lines and Support Clamps
Inspection
T182T Engine Driven Fuel Pump
Engine Fuel Manifold Spring Replacement
Engine Driven Fuel Pump Inspection
Engine Fuel Injection Lines and Support Clamps
Inspection
Engine Driven Fuel Pump Inspection
Engine Fuel Injection Lines and Support Clamps
Inspection
Engine Fuel Injector Unit Inspection
Unison Industries Slick 4200/4300/6200/6300 Magnetos
Inspection
Ignition Switch Center Ground Terminal Inspection
Tachometer Sending Unit Replacement
Engine Exhaust Riser Retention Nut Torque
Engine Exhaust Muffler Inspection
Engine Exhaust Muffler Pressure Test and Ball Joint
Inspection
Engine Exhaust Muffler Replacement
Engine Exhaust Muffler Replacement
Engine Low Oil Pressure Switch Replacement
Engine Oil Pressure Switch Replacement
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Oct 20/1997
Apr 26/2004
Jul 12/1999
Jul 27/1998
Nov 8/2004
Jun 9/2011
Jul 27/1998
Jun 19/2006
May 26/2003
Jul 12/1999
Apr 23/2007
Aug 27/2007
Aug 20/2001
May 10/2004
Nov 25/2004
Nov 19/2007
Feb 3/2003
Oct 25/1999
Nov 4/2003
Mar 30/2009
Dec 24/2001
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
No Effect
Jun 7/2011
Sep 30/2002
Oct 17/2005
Aug 30/2004
No Effect
No Effect
No Effect
No Effect
Mar 7/2005
Aug 17/2010
No Effect
No Effect
Feb 1/1999
Apr 20/2009
No Effect
No Effect
Jun 25/2001
Jun 18/2007
Aug 11/1997
Feb 2/1998
Dec 14/1998
No Effect
No Effect
No Effect
No Effect
No Effect
Dec 14/1998
Feb 2/1998
Feb 21/2000
Jan 29/2007
No Effect
No Effect
No Effect
No Effect
Page 7 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
SB07-80-01
SB11-81-01
SB10-81-01
1
Sky-Tec Starter Installation
Engine Turbocharger Housing Inspection
Engine Turbocharger Inspection
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
May 18/2010
Jan 12/2011
Jun 15/2010
No Effect
No Effect
No Effect
Page 8 of 8
Print Date: Mon Jul 02 05:08:38 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 8)
ICA SUPPLEMENT LIST
ICA Supplement Number
Title
ICA-172-28-00001 Revision
A
ICA-172-33-00001 Revision
A
ICA-182-34-00001
Single Engine Restart Fuel Quantity Indication System ICA
Supplement
Whelen Model 71368 Landing, Taxi, & Recognition Light
System ICA
G1000 Synthetic Vision Technology Option ICA
Supplement
ICA-182-34-00003 Revision Garmin GTS 800 ICA Supplement
B
ICA-206-34-00003 Revision Max Viz EVS-600 Enhanced Vision System ICA
A
Supplement
ICA-T182-35-00001
ICA Supplement - Precise Flight Oxygen Equipment
Revision B
ICA-T182T-61-0001
Model T182T Propeller Low Pitch Stop Modification
Revision C
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
ICA Supplement
Date
Manual
Incorporation
Date
Jan 30/2009
No Effect
Jul 13/2010
Nov 1/2012
Mar 6/2009
No Effect
Feb 22/2012
No Effect
Jan 11/2011
Nov 1/2012
Oct 9/2008
No Effect
Dec 13/2006
No Effect
Page 1 of 1
Print Date: Mon Jul 02 05:08:40 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
SUPPLIER ADDRESS LIST
00779
TYCO ELECTRONICS CORP.
2800 Fulling Mill
M/X 38-77
Middletown, PA 17057
CONXALL CORP.
601 East Wildwood Ave.
Villa Park, IL 60181-2762
RAYCHEM CORP.
DIV. TYCO ELECTRONICS
300 Constitution Dr.
Menlo Park, CA 94025-1111
HOFFMAN ENGINEERING CORP.
8 Riverbend Dr.
P.O. Box 4430
Stamford, CT 06907
GLENAIR, INC.
1211 Air Way
Glendale, CA 91201-2405
C AND K COMPONENTS INC.
15 Riverdale Ave.
Newton, MA 02158-1082
13511
AMPHENOL CADRE DIV.
BUNKER RAMO CORP.
Los Gatos, CA 95030
1F242
PETSCHE A.E. CO., INC.
2112 W. Division
Arlington, TX 76012
SKY-TEC
350 Howard Clemmons Rd.
Granbury, TX 76048
HEADS UP TECHNOLOGIES INC.
2033 Chennault
Suite 100
Carrollton, TX 75006-5097
TEMPREL INC.
206 Air Industrial Dr.
P.O. Box 308
Boyne City, MI 49712
GARMIN INTERNATIONAL, INC.
1200 East 151st St.
Olathe, KS 66062-3426
WHELEN ENGINEERING CO., INC.
Rt. 145 Winthrop Road
Chester, CT 06412
22863
11139
THE DEUTSCH CO.
ENGINEERED CONNECTING DEVICES
36033 Whittier Ave.
Hemet, CA 92545
29907
2B785
ALCOR AVIATION, INC.
12043 Colwick
San Antonio, TX 78216
65702
023K3
06090
06097
06324
09353
0GZF3
0MXP2
0TRC3
10402
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
1MTQ9
1WH29
MAX-VIZ INC. DBA
16165 SW. 72nd Ave.
Portland, OR 97224
1XE65
BIRK AEROSYSTEMS CORP.
7522 Slater Ave. 116
Huntington Beach, CA 92647
HONEYWELL INTERNATIONAL, INC.
AEROSPACE ELECTRONIC SYSTEMS
23500 W. 105th St.
1 Technology Center
Olathe, KS 66061
KAVILCO CORP.
14501 Los Angeles Ave.
Moorpark, CA 93021
22373
25583
27264
28198
L-3 COMMUNICATIONS AVIONICS SYSTEMS,
INC.
5353 52nd St. S.E.
Grand Rapids, MI 49512-9704
MOLEX, INC.
2222 Wellington Ct.
Lisle, IL 60532-1613
POSITRONIC INDUSTRIES, INC.
423 N Campbell St.
P.O. Box 8247
Springfield, MO 65806-1007
OMEGA ENGINEERING, INC.
One Omega Dr..
P.O. Box 4047
Stamford, CT 06907
PRECISION AIRMOTIVE CORP.
Snohomish County Airport
3200 100th St. SW Suite E
Everett, WA 98204
Page 1 of 3
Print Date: Mon Jul 02 05:08:41 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
32890
LUMINESCENT SYSTEMS, INC.
4 Lucent Drive
Lebanon, NH 03766-1439
65907
33497
PRECISION WINDING, INC.
109 S. Knight
Wichita, KS 67213
71379
37942
NORTH AMERICAN CAPACITOR CO.
MALLORY DIV.
Indianapolis Rd. Hwy. 240
P.O. Box 273
Indianapolis, IN 46135
LAMAR TECHNOLOGY, INC.
14900 40th Ave. NE.
Marysville, WA 98271
71400
AMPHENOL CORP.
AMPHENOL AEROSPACE PYLE-NATIONAL
CONNECTORS
40-60 Delaware Ave.
Sidney, NY 13838-1395
HYPERTRONICS CORP.
16 Brent Dr.
Hudson, MA 01749-2904
77342
51351
COMANT INDUSTRIES, INC.
12920 Park St.
Santa Fe Springs, CA 93022
80205
53669
DELPHI CO.NNECTION SYSTEMS
1 Vanderbilt
Irvine, CA 92618-2011
MID-CONTINENT INSTRUMENT CO., INC.
7706 E. Osie St.
Wichita, KS 67207
DAVTRON, INC.
427 Hillcrest Way
Redwood City, CA 94062-4012
ASTROTECH CORP.
10201 N. 21st St.
Phoenix, AZ 85021-1886
81343
MILITARY SPECIFICATIONS
PROMULGATED BY MILITARY DEPT.S/
AGENCIES
98410
3RCD2
49367
50541
59742
63131
63836
81349
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
76374
77820
AEROSPACE DISPLAY
SYSTEM, INC.
2321 Topaz Dr.
Hatfield, PA 19440-1936
CESSNA AIRCRAFT CO.
DEPT 870 PC
1 Cessna Blvd.
Wichita, KS 67277-7704
COOPER BUSSMAN, INC.
114 Old State Rd.
P.O. Box 14460
St. Louis, MO 63021-5942
EATON AEROSPACE, LLC
POWER & LOAD MANAGEMENT SYSTEMS
2250 Whitefield Ave.
Sarasota, FL 34243-3962
TYCO ELECTRONICS CORP.
2800 Fulling Mill Rd.
P.O. BOX 3608
Harrisburg, PA 17105
AMPHENOL CORP.
AMPHENOL AEROSPACE
40-60 Delaware St.
Sidney, NY 13838-1395
NATIONAL AEROSPACE STANDARDS
COMMITTEE AEROSPACE INDUSTRIES
ASSOCIATION OF AMERICA INC.
ASSOCIATION OF AMERICA INC.
1250 Eye St. NW.
Washington, DC 20005
SOCIETY OF AUTOMOTIVE ENGINEERS
400 Commonwealth Dr.
Warrendale, PA 15096
MOLEX ETC INC.
SUB OF MOLEX INC.
4650 62ND Ave. N
Pinellas Park, FL 33565
Page 2 of 3
Print Date: Mon Jul 02 05:08:41 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
81640
82389
82647
83564
88044
91637
93768
96182
96906
EATON CORP.
AEROSPACE AND COMMERCIAL CONTROL
DIV
2250 Whitfield Ave. E
Sarasota, FL 34243-9703
SWITCHCRAFT, INC.
SUBDIVISION OF RAYTHEON
5555 N. Elstron Ave.
Chicago, IL 60630-1314
SENSATA TECHNOLOGIES INC.
529 Pleasant St.
Attleboro, MA 02703-2421
NELLCOR PURITAN BENNETT SYSTEM CO.
18475 Pacific St.
Fountain Valley, CA 92708-7004
AERONAUTICAL STANDARDS GROUP
DEPT OF NAVY AND AIR FORCE
Washington, DC
DALE ELECTRONICS, INC.
1122 23rd St.
P.O. Box 609
Columbus, NE 68601-3632
GORDON CLAUD S CO. DBA WATLOW
GORDON
5710 KENOSHA St.
Richmond, IL 60071
EATON CORP.
AEROSPACE AND COMMERCIAL CONTROLS
MSC PRODUCTS DIV.
1640 Monrovia Ave.
Costa Mesa, CA 92627-4405
MILITARY STANDARDS
PROMULGATED BY MILITARY DEPT. UNDER
AUTHORITY OF DEFENSE
Washington, DC
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
BASC
BIRK AEROSYSTEMS CORP.
7522 Slater Ave.
Huntington Beach, CA 92647
S5416
NEW JAPAN RADIO CO., LTD.
MITSUYA TORANOMON BLDG. 22-14
TORANOMON 1 CHOME MINATO-KU
TOKYO, JAPAN 105
TROLL AVIONICS INC.
3481 W. Fifth St.
Oxnard, CA 93030
TRAI
Page 3 of 3
Print Date: Mon Jul 02 05:08:41 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
LIST OF CHAPTERS
CHAPTER
EFFECTIVE DATE *
20
Standard Practices - Airframe
Jan 1/2016
21
Air Conditioning
Mar 1/2004
22
Auto Flight
Jan 1/2016
23
Communications
Jan 1/2016
24
Electrical Power
Jan 1/2017
25
Equipment/Furnishings
Jan 1/2007
27
Flight Controls
Jan 1/2016
28
Fuel
Mar 1/2010
30
Ice and Rain Protection
Jan 1/2016
31
Indicating Recording Systems
Jan 1/2016
33
Lights
Jan 1/2017
34
Navigation
Jan 1/2017
37
Vacuum
Mar 1/2004
73
Engine Fuel And Control
Jan 1/2016
74
Ignition
Mar 1/2010
77
Engine Indicating
Jan 1/2016
79
Oil
Mar 1/2004
91
Charts
Jan 1/2017
* Represents date of each chapter's List of Effective Pages which is applicable to manual revision date.
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 1 of 1
Print Date: Mon Jul 02 05:08:43 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
REFERENCE DESIGNATOR INDEX
A1
SPLICE
AC900
SPLICE
ACU
CONTROL UNIT, ALTERNATOR
ACU
CONTROL UNIT, ALTERNATOR
AF300
SPLICE
AF301
SPLICE
AF302
SPLICE
AF303
SPLICE
AF304
SPLICE
AF305
SPLICE
AF306
SPLICE
AI304
SPLICE
AL001
CONNECTOR, LEFT STROBE POWER SUPPLY GROUND DISCONNECT
AT300
SPLICE
CN001
CAPACITOR, ALTERNATOR
CN002
CAPACITOR
On MN001 alternator located in nose on engine.
CZ001
CAPACITOR, DIMMING ASSEMBLY
CZ002
CAPACITOR, DIMMING ASSEMBLY
CZ003
CAPACITOR, DIMMING ASSEMBLY
CZ004
CAPACITOR, DIMMING ASSEMBLY
CZ005
CAPACITOR, DIMMING ASSEMBLY
D1
TRANSZORB
Left and right fuel quantity signal conditioner assembly.
81318 & ON
8232 & ON
D2
TRANSZORB
Left and right fuel quantity signal conditioner assembly.
81318 & ON
8232 & ON
DI001
DIODE
DI002
DIODE
DI004
DIODE, ZENER
DI005
DIODE
DI006
DIODE
DI007
DIODE
DI100
DIODE, CIRCUIT BREAKER PANEL
Copyright © Textron Aviation Inc.
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Page 1 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
DI101
DIODE, CIRCUIT BREAKER PANEL
DI300
DIODE, CIRCUIT BREAKER PANEL
DT600
DIODE
DT601
DIODE
EI001
INDICATOR, OIL TEMPERATURE/PRESSURE
EI002
CLOCK
EI003
INDICATOR, HOURMETER
EI004
INDICATOR, TURN COORDINATOR
EI005
INDICATOR, TACHOMETER
EI006
INDICATOR, VERTICAL SPEED
EI007
INDICATOR, DIRECTIONAL GYRO
EI009
INDICATOR, HORIZONTAL GYRO
EI010
INDICATOR, ALTIMETER
EI010
INDICATOR, ALTIMETER
EI011
INDICATOR, FUEL QUANTITY
EI011
INDICATOR, FUEL QUANTITY
EI012
INDICATOR, AMMETER/VACUUM
EI014
INDICATOR, EGT/CHT
EI014
INDICATOR, EGT/CHT
EI014
INDICATOR, EGT/CHT
EI014
PROBE, EGT/CHT
EI015
INDICATOR, MANIFOLD PRESSURE/FUEL FLOW
Located on lower middle of left instrument panel.
EI016
INDICATOR, TIT/CHT
EI017
PROBE, EGT/CHT
EI019
CLOCK
EI019
CLOCK
EI020
INDICATOR, MANIFOLD PRESSURE/FUEL FLOW
EI021
ANNUNCIATOR, PROPELLER DEICE
EI025
INDICATOR, AIRSPEED
EI026
INDICATOR, TACHOMETER
EI028
INDICATOR, ALTIMETER
EI028
INDICATOR, ALTIMETER
EI029
INDICATOR, HOURMETER
F1
FUSE
F1
FUSE
F1
FUSE
F2
FUSE
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 2 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
F2
FUSE
F2
FUSE
F3
FUSE
F3
FUSE
F4
FUSE, CLOCK
FC001
LAMP, COMPASS
FC002
LIGHT ASSEMBLY, PILOT DOME
On forward center of overhead console.
FC002
LIGHT ASSEMBLY, LED PILOT DOME
On forward center of overhead console.
FC003
LIGHT ASSEMBLY, COPILOT DOME
On forward right side of overhead console.
FC004
LIGHT, OXYGEN GAGE
FC005
LIGHT ASSEMBLY, REAR DOME
On aft end of overhead console.
FC005
LIGHT ASSEMBLY, LED REAR DOME
On aft end of overhead console.
FC006
LIGHT, PILOT DOME LED
On forward center of overhead console.
FC007
LIGHT, REAR DOME LED
On aft center of overhead console.
FC012
LIGHT ASSEMBLY, LED PILOT FLOOD
FC014
LIGHT, PEDESTAL FUEL SELECT
FC015
LIGHT, PEDESTAL TRIM
FF004
LIGHT ASSEMBLY, LED COPILOT FLOOD
FI002
LIGHT ASSEMBLY, GLARESHIELD
On glareshield.
FI003
LIGHT ASSEMBLY, UPPER PEDESTAL
In top of pedestal.
FI004
LIGHT ASSEMBLY, LOWER PEDESTAL
In lower pedestal.
FI004
LIGHT ASSEMBLY, LOWER PEDESTAL
Located in lower pedestal.
FI005
LIGHT, CENTER PEDESTAL
In center pedestal.
FI007
ANNUNCIATOR PANEL, LED LIGHT ASSEMBLY
On glareshield.
FI008
LIGHT ASSEMBLY, AIRCRAFT IDENTIFICATION
Copyright © Textron Aviation Inc.
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Page 3 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
FI011
LED, GREEN
FL001
LIGHT ASSEMBLY, TAXI
Located on left outboard leading edge of left wing.
FL001
LIGHT ASSEMBLY, TAXI
Located on left outboard leading edge of left wing.
FL002
LIGHT ASSEMBLY, LANDING
Located on left outboard leading edge of left wing.
FL002
LIGHT ASSEMBLY, LANDING
Located on left outboard leading edge of left wing.
FL003
LIGHT ASSEMBLY, LEFT NAVIGATION (RED)
In left wing tip.
FL005
LIGHT ASSEMBLY, LEFT STROBE
In left wing tip.
FL006
LIGHT ASSEMBLY, LEFT NAVIGATION (RED)
Located in left wing tip.
FL007
LIGHT ASSEMBLY, LEFT STROBE
In left wing tip.
FL008
HID LIGHT ASSEMBLY, LANDING
Located on left outboard leading edge of left wing.
FL009
HID LIGHT ASSEMBLY, TAXI
Located on left outboard leading edge of left wing.
FL010
LIGHT ASSEMBLY, LEFT NAVIGATION (RED)
FL011
LIGHT, LH COURTESY
FR001
LIGHT ASSEMBLY, RIGHT NAVIGATION (GREEN)
In right wing tip.
FR003
LIGHT ASSEMBLY, RIGHT STROBE
In right wing tip.
FR004
LIGHT ASSEMBLY, RIGHT NAVIGATION (GREEN)
Located in right wing tip.
FR005
LIGHT ASSEMBLY, RIGHT STROBE
In right wing tip.
FR006
LIGHT, GREEN POSITION
FR007
LIGHT, RH COURTESY
FV001
LIGHT ASSEMBLY
In tail stinger.
FV002
LIGHT ASSEMBLY, BEACON
In top of vertical tail.
FV004
LIGHT ASSEMBLY, BEACON
Copyright © Textron Aviation Inc.
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Page 4 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
In top of vertical tail.
FV006
LIGHT, GREEN POSITION
FV007
TAIL POS LIGHT-LED
GC002
TERMINAL
GF011
GROUND
GI001
GROUND BLOCK
Located on outboard side behind instrument panel.
GL001
GROUND
Ground for left FL005 strobe light assembly located in left wing tip.
GL010
GROUND
Ground for left courtesy light located in left wing tip.
GL010
GROUND, LEFT STROBE POWER SUPPLY DISCONNECT
Ground for left strobe light power supply in left wing tip.
GL100
GROUND STUD
Ground for audio control panel.
GN002
GROUND STUD
GN004
GROUND
GN005
GROUND, MAGNETO
GN008
GROUND
GR002
GROUND, RIGHT STROBE POWER SUPPLY DISCONNECT
Ground for right FR003 strobe light assembly located in right wing tip.
GR010
GROUND
Ground for right courtesy light located in right wing tip.
GS100
GROUND
Located on the back of the wing leveler computer rack.
GS300
GROUND, WING LEVELER
Located near roll servo actuator.
GS301
GROUND
Ground is located on the back of the autopilot computer rack.
GS302
GROUND
Ground is located on the pitch servo mounting rack.
GS303
GROUND
Ground is located on the pitch trim servo mounting rack.
GS309
GROUND
GS901
GROUND
GS902
GROUND SCREW
GV001
GROUND
GV004
GROUND
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Page 5 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
HC900
FUSE
HI001
CIRCUIT BREAKER
In electrical circuit breaker panel.
HI002
CIRCUIT BREAKER
HI003
CIRCUIT BREAKER
In electrical circuit breaker panel.
HI004
CIRCUIT BREAKER, BEACON LIGHT
In electrical circuit breaker panel.
HI005
CIRCUIT BREAKER, STROBE LIGHTS
In electrical circuit breaker panel.
HI006
CIRCUIT BREAKER
HI007
CIRCUIT BREAKER
HI008
CIRCUIT BREAKER
HI009
CIRCUIT BREAKER
HI010
CIRCUIT BREAKER
HI011
CIRCUIT BREAKER
HI011
CIRCUIT BREAKER
HI012
CIRCUIT BREAKER
HI013
CIRCUIT BREAKER
In electrical circuit breaker panel.
HI015
CIRCUIT BREAKER
In electrical circuit breaker panel.
HI022
CIRCUIT BREAKER
HI023
CIRCUIT BREAKER
HI024
CIRCUIT BREAKER
HI025
CIRCUIT BREAKER
HI026
CIRCUIT BREAKER
HI027
CIRCUIT BREAKER
HI028
CIRCUIT BREAKER
HI029
CIRCUIT BREAKER
HI030
CIRCUIT BREAKER
HI031
CIRCUIT BREAKER
HI032
CIRCUIT BREAKER
HI034
CIRCUIT BREAKER
HI035
CIRCUIT BREAKER
HI036
CIRCUIT BREAKER
HI037
CIRCUIT BREAKER
HI038
CIRCUIT BREAKER
Copyright © Textron Aviation Inc.
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Page 6 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
HI039
CIRCUIT BREAKER
HI040
CIRCUIT BREAKER
HI041
CIRCUIT BREAKER
HI042
CIRCUIT BREAKER
HI043
CIRCUIT BREAKER
HI045
CIRCUIT BREAKER
HI047
CIRCUIT BREAKER
HI048
CIRCUIT BREAKER
HI049
CIRCUIT BREAKER
HI050
CIRCUIT BREAKER
HI051
CIRCUIT BREAKER
HI052
CIRCUIT BREAKER
HI056
CIRCUIT BREAKER, CABIN LIGHTS/POWER
HI065
CIRCUIT BREAKER, LANDING LIGHT
HI066
CIRCUIT BREAKER, RECOGNITION TAXI LIGHT
HI067
CIRCUIT BREAKER
HI068
CIRCUIT BREAKER
HI069
CIRCUIT BREAKER
HI070
CIRUCIT BREAKER
HI073
FUSE
HI100
CIRCUIT BREAKER
HI101
CIRCUIT BREAKER
HI102
CIRCUIT BREAKER
HI103
CIRCUIT BREAKER
HI104
CIRCUIT BREAKER
HI105
CIRCUIT BREAKER, WING LEVELER
In avionics circuit breaker panel.
HI106
CIRCUIT BREAKER
In avionics circuit breaker panel.
HI900
CIRCUIT BREAKER
HI901
CIRCUIT BREAKER
HI902
CIRCUIT BREAKER
HI903
CIRCUIT BREAKER
HI904
CIRCUIT BREAKER
HI905
CIRCUIT BREAKER
HI906
CIRCUIT BREAKER
HI911
CIRCUIT BREAKER
HI915
CIRCUIT BREAKER
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 7 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
HI916
CIRCUIT BREAKER
HI940
FUSE
J1
CONNECTOR, STROBE DISCONNECT
Connect to UL001 and UR001 strobe power supply.
J1
CONNECTOR, POWER JUNCTION BOX DISCONNECT
J1
CONNECTOR, LED SWITCH PANEL DISCONNECT
Connect to UI009 or UI110 LED lighted switch panel.
J1
CONNECTOR, COURTESY LIGHT DISCONNECT
Disconnect for FL004 and FR002 courtesy lights.
J1
CONNECTOR, DIMMING MODULE
J2
CONNECTOR, POWER SUPPLY DISCONNECT
Connects to FL004 and FR002 courtesy lights.
J3
CONNECTOR
J4
CONNECTOR
J5
CONNECTOR
JC001
CONNECTOR, CIRCUIT BREAKER PANEL DISCONNECT
Disconnect for electrical circuit breaker panel located behind instrument panel.
JC002
CONNECTOR, CENTER PEDESTAL DISCONNECT
Connects to FI005 center pedestal light.
JC003
CONNECTOR, LOWER PEDESTAL DISCONNECT
Connects to FI004 lower pedestal light.
JC004
CONNECTOR, UPPER PEDESTAL DISCONNECT
Connects to FI003 upper pedestal light.
JC005
CONNECTOR, DIMMING CONTROL
Disconnect for dimming control module located behind right instrument panel on outboard side.
JC007
CONNECTOR, ELECTRICAL/AVIONIC DISCONNECT
Avionics/electrical disconnect behind instrument panel.
JC008
CONNECTOR
Located in cabin below instrument panel.
JC009
CONNECTOR
JC010
CONNECTOR, CIRCUIT BREAKER PANEL DISCONNECT
Disconnect for electrical circuit breaker panel located behind instrument panel.
JC011
CONNECTOR, OVERHEAD DISCONNECT
Located behind overhead console in cabin.
JC012
CONNECTOR
JC014
CONNECTOR
JC015
CONNECTOR, ANNUNICATOR SWITCH DISCONNECT
Located behind center instrument panel.
Copyright © Textron Aviation Inc.
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Page 8 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
JC018
CONNECTOR
JC022
CONNECTOR
JC023
CONNECTOR
JC024
CONNECTOR, ELECTRICAL CIRCUIT BREAKER PANEL DISCONNECT
Located behind left instrument panel.
JC025
CONNECTOR
JC026
CONNECTOR, SWITCH PANEL DISCONNECT
Located behind left instrument panel.
JC030
CONNECTOR
JC031
CONNECTOR, ELECTRICAL/AVIONIC DISCONNECT
Located behind center instrument panel.
JC032
CONNECTOR
JC036
CONNECTOR
JC037
CONNECTOR
JC522
CAP
JC523
CONNECTOR
JF005
CONNECTOR KIT, FUEL PUMP
JF006
CONNECTOR
JI001
CONNECTOR
JI001
CONNECTOR
JI003
CONNECTOR, DIMMING MODULE DISCONNECT
Disconnect for dimming control module located behind right instrument panel on outboard side.
JI004
CONNECTOR
JI006
CONNECTOR
JI007
CONNECTOR
JI008
CONNECTOR
JI009
CONNECTOR, AIRSPEED INDICATOR
JI010
CONNECTOR, HORIZON GYRO
JI011
CONNECTOR, ALTIMETER
JI012
CONNECTOR, CENTER PANEL DISCONNECT
Disconnect for left instrument panel located behind left instrument panel.
JI012
CONNECTOR, CONTROL PANEL DISCONNECT
Disconnect for left instrument panel located behind left instrument panel.
JI013
CONNECTOR, FUEL QUANTITY INDICATOR
JI014
CONNECTOR, TACHOMETER
JI015
CONNECTOR, OIL TEMPERATURE/PRESSURE INDICATOR
JI016
CONNECTOR, VERTICAL SPEED INDICATOR
JI017
CONNECTOR, EGT/CHT
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 9 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
JI018
CONNECTOR, TIT/CHT INDICATOR
JI019
CONNECTOR, AMMETER/VACUUM INDICATOR
JI021
CONNECTOR, CLOCK
JI022
CONNECTOR, DEICE DISC
JI030
CONNECTOR, PILOT'S CONTROL WHEEL
JI031
CONNECTOR, DOME LIGHT SWITCH
JI032
CONNECTOR, POWER SUPPLY
Disconnect for UI001 power supply behind instrument panel.
JI033
CONNECTOR, MAINIFOLD PRESSURE/FUEL FLOW INDICATOR
Disconnect located behind left instrument panel.
JI034
CONNECTOR
JI035
CONNECTOR, AIRCRAFT IDENTIFICATION PLACARD DISCONNECT
Disconnect to FI008 aircraft identification placard light located behind instrument panel.
JI039
CONNECTOR
JI043
CONNECTOR
JI049
PIN
JI314
CONNECTOR
JI332
CONNECTOR
JI504
CONNECTOR
JI505
CONNECTOR
JI506
CONNECTOR, PILOT CONTROL WHEEL
JI513
CONNECTOR, CONTROL WHEEL
JI513
CONNECTOR, CONTROL WHEEL
JI514
CONNECTOR, CONTROL WHEEL
Disconnect for pilot control wheel located behind left instrument panel.
80001 - 81179
8001 & ON
JI514
CONNECTOR, CONTROL WHEEL
Disconnect for pilot control wheel located behind left instrument panel.
81180 & ON
JI515
CONNECTOR
JI901
CONNECTOR, AVIONICS COOLING FAN
Disconnect for avionics cooling fan located behind left instrument panel.
80004 & ON
8001 & ON
JI901
CONNECTOR
JI901
PIN
JL002
HOUSING, LEFT WING DISCONNECT
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 10 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
Left wing electrical disconnect located at left wing root.
JL003
CONNECTOR
JL005
CONNECTOR, LEFT STROBE POWER SUPPLY DISCONNECT
JL006
CONNECTOR, PITOT HEATER
JL007
CONNECTOR, PITOT HEATER
JL008
CONNECTOR, LEFT NAGIVATION LIGHT DISCONNECT
Connects to FL006 left navigation light in left wing tip.
JL012
CONNECTOR
JL021
CONNECTOR, STALL WARNING
JM300
CONNECTOR
JN001
CONNECTOR KIT
JN003
CONNECTOR KIT
JN004
CONNECTOR KIT, OIL PRESSURE TRANSDUCER
JN005
CONNECTOR KIT, OIL PRESSURE SWITCH
JN006
CONNECTOR, EGT PROBE
JN007
CONNECTOR, TIT PROBE
JN009
CONNECTOR
JN011
CONNECTOR
JN012
CONNECTOR
JN013
CONNECTOR
JN014
CONNECTOR
JN015
CONNECTOR
JN016
CONNECTOR
JN017
CONNECTOR
JN018
CONNECTOR
JN019
CONNECTOR
JN020
CONNECTOR
JN021
CONNECTOR
JN022
CONNECTOR
JN023
CONNECTOR
JN028
CONNECTOR
JR001
CONNECTOR, RIGHT WING DISCONNECT
Disconnect for right wing located on rib in right wing root.
JR002
CONNECTOR
JR004
CONNECTOR, RIGHT STROBE POWER SUPPLY
Disconnect for UR001 strobe power supply in right wing tip.
JR005
CONNECTOR, FLAP ACTUATOR ASSEMBLY
JR006
CONNECTOR, FLAP ACTUATOR ASSEMBY
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 11 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
JR007
CONNECTOR, FLAP MOTOR ASSEMBLY
JR010
CONNECTOR, RIGHT NAVIGATION DISCONNECT
JR011
CONNECTOR
JR013
CONNECTOR
JR022
CONNECTOR, FLAP ACTUATOR ASSY
JS300
CONNECTOR, RIGHT WING DISCONNECT
Disconnect in leading edge of right wing near wing.
JS301
HOUSING
JS900
CONNECTOR
JT005
RECEPTACLE
JT700
CONNECTOR
082331 & ON
JV001
CONNECTOR, TAIL/STINGER DISCONNECT
Disconnect for vertical tail located at base of rudder.
JV003
CONNECTOR, VERTICAL TAIL DISCONNECT
JV004
CONNECTOR, BEACON LIGHT DISCONNECT
Disconnect for FV002/FV003 flashing beacon located in vertical tail.
JV004
CONNECTOR, BEACON LIGHT DISCONNECT
Disconnect for FV002/FV003 flashing beacon located in vertical tail.
JV005
CONNECTOR, VERTICAL TAIL DISCONNECT
Vertical tail disconnect for flashing beacon located in base of vertical tail.
JV1000
CONNECTOR, NAVIGATION ANTENNA COAX
JV1002
CONNECTOR, NAVIGATION ANTENNA
JZ900
CONNECTOR
Disconnect for HI106 circuit breaker behind instrument panel on left side.
JZ905
CONNECTOR
JZ906
CONNECTOR
K1
RELAY, ALTERNATOR
K2
RELAY, START
NOT INCORPORATING SB07-80-01
K3
RELAY, EXTERNAL POWER
K4
RELAY, BATTERY
L1
LIGHT ASSEMBLY, PILOT'S CONTROL WHEEL MAP
MN001
ALTERNATOR, 60 AMP
MN001
ALTERNATOR, 95 AMP
Located in nose on engine.
MN002
STARTER
NOT INCORPORATING SB07-80-01
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 12 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
MR001
MOTOR ASSEMBLY, FLAP
MR001
MOTOR ASSEMBLY, FLAP
NZ001
PRINTED CIRCUIT BOARD, STANDBY BATTERY
P1
CONNECTOR, DIMMING MODULE
Disconnect for dimming control module located behind right instrument panel on outboard side.
P1
CONNECTOR, STROBE DISCONNECT
Disconnect for FL005 and FR003 strobe light assembly.
P1
CONNECTOR, STROBE DISCONNECT
Disconnect for FL007 and FR005 strobe light assembly.
P1
CONNECTOR, DIMMING MODULE
P2
CONNECTOR, GLARESHIELD LIGHTING
Connect to UI001 glareshield power supply located behind instrument panel.
P2
TERMINAL
Pilot dome light regulator disconnect
P3
TERMINAL
Copilot dome light regulator disconnect
P4
CONNECTOR, POWER JUNCTION BOX
PB017
CONNECTOR KIT, POWER JUNCTION BOX
PB018
CONNECTOR, POWER JUNCTION BOX
PB019
CONNECTOR KIT, POWER JUNCTION BOX
PB023
CONNECTOR KIT
PC001
CONNECTOR, CIRCUIT BREAKER PANEL DISCONNECT
Disconnect for electrical circuit breaker panel located in cabin behind instrument panel.
PC002
CONNECTOR, CENTER PEDESTAL DISCONNECT
Disconnect for center pedestal light located behind instrument panel.
PC003
CONNECTOR, PEDESTAL LIGHT DISCONNECT
Disconnect for lower pedestal light located behind instrument panel.
PC004
CONNECTOR, PEDESTAL LIGHT DISCONNECT
Disconnect for upper pedestal light located behind instrument panel.
PC005
CONNECTOR, DIMMING CONTROL MODULE DISCONNECT
Disconnect for dimming control module located behind left instrument panel on outboard side.
PC007
CONNECTOR, ELECTRICAL/AVIONIC DISCONNECT
Avionics/electrical disconnect behind instrument panel.
PC007
CONNECTOR
PC009
CONNECTOR
PC010
CONNECTOR, CIRCUIT BREAKER PANEL DISCONNECT
Circuit breaker panel disconnect located behind circuit breaker panel on left side.
PC011
CONNECTOR, OVERHEAD DISCONNECT
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 13 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
Located behind overhead console in cabin.
PC012
CONNECTOR
PC013
CONNECTOR, DEICE TIMER/MONITOR
PC014
CONNECTOR
PC015
CONNECTOR, ANNUNICATOR SWITCH DISCONNECT
Connects to SI004 annunciator test/dim switch located behind center instrument panel.
PC018
CONNECTOR, SWITCH DEICE DISCONNECT
PC022
CONNECTOR
PC023
CONNECTOR
PC024
CONNECTOR, ELECTRICAL CIRCUIT BREAKER PANEL DISCONNECT
Located behind left instrument panel.
PC025
CONNECTOR
PC026
CONNECTOR, SWITCH PANEL DISCONNECT
Located behind left instrument panel.
PC030
CONNECTOR
PC031
CONNECTOR, ELECTRICAL/AVIONIC DISCONNECT
Located behind center instrument panel.
PC033
TERMINAL
PC034
CONNECTOR KIT
PC036
CONNECTOR
PC037
CONNECTOR
PC038
CONNECTOR, PEDESTAL FUEL SELECT LIGHT
PC039
CONNECTOR, PEDESTAL TRIM LIGHT
PC1001
CONNECTOR, COMM 1 ANTENNA COAX
PC1002
CONNECTOR, COMM 2 ANTENNA COAX
PC1003
CONNECTOR, ANTENNA
PC1004
CONNECTOR, NAV/COMM COAX
PC1006
CONNECTOR, COAX
PC1007
CONNECTOR, ANTENNA COAX
PC1008
CONNECTOR, NAV/COMM 1 COAX
PC1009
CONNECTOR
PC1010
CONNECTOR
PC1012
CONNECTOR
PC1014
ANTENNA, XM
PC302
JACK, PILOT HEADSET
PC303
JACK, PILOT MIC
PC304
JACK, PILOT HANDHELD MIC
PC502
JACK, PILOT HEADSET
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 14 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PC503
JACK, PILOT MIC
PC504
JACK, PILOT HAND MICROPHONE
PC505
JACK, PASSENGER MICROPHONE
PC506
JACK, PASSENGER HEADSET
PC509
JACK, PILOT HEADSET
PC510
JACK, MICROPHONE
PC511
JACK, PILOT MICROPHONE
PC512
JACK, ENTERTAINMENT AUDIO
PC515
JACK, PASSENGER HEADSET
PC517
JACK, PASSENGER MICROPHONE
PC522
CONNECTOR
PC523
CONNECTOR
PC600
CONNECTOR KIT, KA-44B ANTENNA
PC800
CONNECTOR, ENCODING ALTIMETER
PC901
CONNECTOR, SUPPLIED WITH VENDOR KIT
Located behind instrument panel.
PF003
CONNECTOR KIT
PF004
CONNECTOR
PF006
CONNECTOR
PF1000
CONNECTOR, ANTENNA
PF1001
CONNECTOR
PF1001
CONNECTOR
PF1001
CONNECTOR
PF1002
CONNECTOR, COAX
PF1004
CONNECTOR, ANTENNA
PF1005
CONNECTOR, COAX
PF1006
CONNECTOR, COAX
PF1007
CONNECTOR, COAX
PF1008
CONNECTOR, COAX
PF1009
CONNECTOR, COAX
PF1010
CONNECTOR
PF1011
CONNECTOR, COAX
PF1013
CONNECTOR
PF1014
CONNECTOR
PF1015
CONNECTOR
PF1016
CONNECTOR
PF1017
CONNECTOR
PF302
JACK, COPILOT HEADSET
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 15 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PF303
JACK, COPILOT MICROPHONE
PF502
JACK, COPILOT HEADSET
PF503
JACK, COPILOT MICROPHONE
PF504
JACK, PASSENGER HEADSET
PF505
JACK, PASSENGER MICROPHONE
PF508
JACK, PASSENGER HEADSET
PF509
JACK, PASSENGER MICROPHONE
PF512
JACK, COPILOT HEADSET
PF513
JACK, COPILOT MICROPHONE
PF800
CONNECTOR
PF900
CONNECTOR
PF901
CONNECTOR
Located behind instrument panel.
PF902
CONNECTOR
Ground for PI307 turn coordinator located behind instrument panel.
PF903
CONNECTOR
Ground for avionics cooling fans located behind instrument panel.
PI001
CONNECTOR
PI004
CONNECTOR
PI007
CONNECTOR, DIRECTIONAL GYRO
PI008
CONNECTOR, TURN COORDINATOR
PI009
CONNECTOR, AIRSPEED INDICATOR
PI010
CONNECTOR, HORIZON GYRO
PI011
CONNECTOR, ALTIMETER
PI012
CONNECTOR, CENTER PANEL DISCONNECT
Flight Instruments disconnect located behind left instrument panel.
PI014
CONNECTOR, VERTICAL SPEED INDICATOR
PI016
CONNECTOR, TACHOMETER
PI022
CONNECTOR, DEICE DISCONNECT
PI027
CONNECTOR
PI029
TERMINAL, GLARESHIELD LIGHT REGULATOR
PI031
SOCKET
Disconnect for JI031 located behind center instrument panel.
PI035
CONNECTOR, AIRCRAFT ID PLACARD LIGHT DISCONNECT
Connects to FI008 aircraft identification placardl light.
PI036
CONNECTOR
PI037
CONNECTOR
PI038
CONNECTOR
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 16 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PI039
SOCKET
Located behind left instrument panel.
PI039A
SOCKET
Located behind left instrument panel.
PI040
CONNECTOR, LED CIRCUIT BREAKER PANEL DISCONNECT
Located behind left instrument panel.
PI041
TERMINAL, LED PANEL LIGHT REGULATOR
Located behind left instrument panel.
PI045
CONNECTOR, DIMMING MODULE DISCONNECT
Disconnect for dimming control module located behind right instrument panel on outboard side.
PI047
CONNECTOR
Console cover panel disconnect.
PI049
RECEPTACLE
PI050
SOCKET
PI1000
CONNECTOR, NAV/COMM 1
PI1001
TERMINAL, TRANSPONDER COAX
80001 - 80003
PI1001
CONNECTOR, TRANSPONDER COAX
80004 & ON
PI1002
CONNECTOR, NAV/COMM 1
PI1003
CONNECTOR, NAV COUPLER
PI1004
CONNECTOR
PI1005
CONNECTOR, COMM 1 ANTENNA
PI1006
CONNECTOR, COAX
PI1007
CONNECTOR
PI1008
CONNECTOR, ADF COAX
PI1009
CONNECTOR, NAV COUPLER
PI1010
CONNECTOR, COMM 2 ANTENNA
PI1011
CONNECTOR, GPS RECEIVER
PI1011
CONNECTOR
PART OF INSTALLATION KIT 050-03321-0000
PI1016
CONNECTOR, NAV COUPLER
PI1017
CONNECTOR, COMM 2 ANTENNA
PI1028
CONNECTOR
PI300
CONNECTOR
Disconnect for UI300 wing leveler computer located behind audio panel.
PI301
CONNECTOR, TURN COORDINATOR
Connects to UI301 turn coordinator located behind left instrument panel.
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 17 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PI302
CONNECTOR, DIRECTIONAL GYRO
Connects to UI302 directional gyro located in left instrument panel.
80004 & ON
8139 & ON
PI303
CONNECTOR, AUTOPILOT COMPUTER
Connects to UI303 autopilot computer located behind audio panel.
PI304
CONNECTOR, AUTOPILOT COMPUTER
Connects to UI303 autopilot computer located behind audio panel.
PI305
CONNECTOR, CONFIGURATION MODULE
Connects to UI305 configuration module located behind left instrument panel.
PI306
CONNECTOR, RS232 INTERFACE
Located under instrument panel.
PI307
CONNECTOR, TURN COORDINATOR
Connects to UI307 located behind left instrument panel near turn coordinator indicator.
80004 & ON
PI308
CONNECTOR, HORIZONTAL SITUATION INDICATOR
Connects to UI308 located behind left instrument panel near Horizontal Situation Indicator.
PI309
CONNECTOR, HORIZONTAL SITUATION INDICATOR
Connects to UI308 located behind left instrument panel near horizontal situation indicator.
PI310
CONNECTOR, SLAVING ACC
PI311
CONNECTOR, SLAVING ACC
PI312
CONNECTOR
PI313
CONNECTOR KIT
PI314
CONNECTOR
PI315
CONNECTOR
PI316
CONNECTOR
PI317
MODULE KIT, CONFIGURATION
PI318
CONNECTOR
PI332
CONNECTOR
PI406
CONNECTOR, KMD-540 MFD
PI407
CONNECTOR, KMD-540 MFD
PART OF KMD-540 INSTALLATION KIT 050-03605-0000
PI500
CONNECTOR, AUDIO PANEL
Connects to audio control in audio panel.
PI501
CONNECTOR, KX-155 NAV/COMM 1
PI502
CONNECTOR, KX-155 NAV/COMM 1
PI503
CONNECTOR, KX-155 NAV/COMM 2
PI507
CONNECTOR, AUDIO PANEL
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 18 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
Connects to UI507 audio panel located in audio panel.
PI508
CONNECTOR, AUDIO PANEL
Connects to UI508 audio panel located in center instrument panel.
PI509
GROUND CONNECTOR
PI510
CONNECTOR KIT, KX155A NAV/COMM
PI511
CONNECTOR, KX155A NAV/COMM
PI512
CONNECTOR, KX155A NAV/COMM
PI516
CONNECTOR KIT, AUDIO PANEL
PI517
CONNECTOR KIT, KMA-28 AUDIO PANEL
PI518
CONNECTOR, KX-155A NAV/COMM 2
PI519
CONNECTOR, KX-155 NAV/COMM 2
PI531
CONNECTOR, AUDIO PANEL DISCONNECT
Located behind center instrument panel.
PI532
CONNECTOR, AUDIO PANEL DISCONNECT
Located behind center instrument panel.
PI533
CONNECTOR, KIT
PI600
CONNECTOR
PI601
CONNECTOR, KI208 INDICATOR
PI602
CONNECTOR, KR-87 ADF
PI603
CONNECTOR, KI-227 ADF INDICATOR
PI604
CONNECTOR KIT, KI209A INDICATOR
Connects to UI604 ADF indicator located in right side of left instrument panel.
PI610
CONNECTOR KIT, KI209 INDICATOR 1
PI700
CONNECTOR, KLN-89B GPS
PI700
CONNECTOR
PART OF INSTALLATION KIT 050-03321-0000
PI701
CONNECTOR, KLN-89B GPS
PI701
CONNECTOR
PART OF INSTALLATION KIT 050-03321-0000
PI702
CONNECTOR, GPS SELECTOR
80004 - 80944
PI703
CONNECTOR, GPS SELECTOR
PI704
CONNECTOR KIT, GPS SWITCHING UNIT
PI705
CONNECTOR KIT, GPS SELECTOR
PI706
CONNECTOR
PI800
CONNECTOR KIT, TRANSPONDER
Connects to UI800 KT-76C transponder located in audio panel.
PI900
CONNECTOR
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 19 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
Connects to lighting bus located behind audio panel.
PI901
CONNECTOR
PI903
CONNECTOR
PI906
RG179 BNC CONNECTION
PL002
HOUSING, LEFT WING DISCONNECT
Connects to UL002 left fuel transmitter located at the left wing disconnect in wing root.
PL003
CONNECTOR
PL004
CONNECTOR, LEFT COURTESY LIGHT DISCONNECT
Connects to J1 left courtesy light disconnect located in left wing.
PL005
CONNECTOR, LEFT STROBE POWER SUPPLY DISCONNECT
Connects to Ul001 left strobe light power supply located in left wing tip.
PL005
CONNECTOR, LEFT STROBE POWER SUPPLY DISCONNECT
Connects to UL003 left strobe light power supply located in left wing tip.
PL006
CONNECTOR
PL007
CONNECTOR
PL008
CONNECTOR, LEFT NAVIGATION LIGHT DISCONNECT
Connects to PL002 left wing disconnect located in left wing root.
PL010
CONNECTOR KIT
Left wing leading edge.
PL011
CONNECTOR KIT
Left wing leading edge.
PL020
CONNECTOR, LEFT COURTESY LIGHT DISCONNECT
Connects to J2 left courtesy light disconnect located in left wing tip.
PL021
CONNECTOR
PL301
CONNECTOR, FLUX TRANSMITTER
PL302
CONNECTOR KIT
PL900
PLUG, LEFT FUEL QUANITY SENSOR
PM300
CONNECTOR
PN006
CONNECTOR, EGT PROBE DISCONNECT
PN007
CONNECTOR, TIT PROBE
PN008
CONNECTOR, ALTERNATOR
PN009
CONNECTOR, FUEL FLOW DISCONNECT
PN011
CONNECTOR
PN012
CONNECTOR
PN013
CONNECTOR
PN014
CONNECTOR
PN015
CONNECTOR
PN016
CONNECTOR
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 20 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PN017
CONNECTOR
PN018
CONNECTOR
PN019
CONNECTOR
PN020
CONNECTOR
PN021
CONNECTOR
PN022
CONNECTOR
PN023
CONNECTOR
PN025
CONNECTOR
PN028
CONNECTOR
PR001
CONNECTOR, RIGHT WING DISCONNECT
Connects to UR002 right fuel transmitter located at the right wing disconnect in wing root.
PR002
CONNECTOR
PR003
CONNECTOR, RIGHT COURTESY LIGHT DISCONNECT
Connects to J1 right courtesy light disconnect located in right wing.
PR004
CONNECTOR, RIGHT STROBE POWER SUPPLY DISCONNECT
Connects to UR001 right strobe light power supply located in right wing tip.
PR004
CONNECTOR, RIGHT STROBE POWER SUPPLY DISCONNECT
Connects to UR003 right strobe light power supply located in right wing tip.
PR005
CONNECTOR, FLAP ACTUATOR ASSEMBLY
PR006
CONNECTOR
PR007
CONNECTOR, FLAP ACTUATOR ASSEMBLY
PR010
CONNECTOR, RIGHT NAVIGATION LIGHT DISCONNECT
PR011
CONNECTOR
PR020
CONNECTOR, RIGHT COURTESY LIGHT DISCONNECT
Connects to J2 right courtesy light disconnect located in right wing tip.
PR022
CONNECTOR, FLAP ACTUATOR
PR300
CONNECTOR, ROLL SERVO
Connects to UR300 roll servo actuator located in right wing.
PR301
CONNECTOR, ROLL SERVO ACTUATOR
Connects to UR300 roll servo actuator located in right wing.
PR302
CONNECTOR
PR900
PLUG, RIGHT FUEL QUANITY SENSOR
PR901
EVS-600 CAMERA
PS300
CONNECTOR, ROLL SERVO
Connects to JS300 roll servo actuator wing disconnect located in right wing near root.
PS301
HOUSING
PT001
CONNECTOR
PT005
CONTACT
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 21 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PT1003
CONNECTOR, COAX
PT1004
CONNECTOR, COAX
PT1005
CONNECTOR, COAX
PT1006
CONNECTOR, COAX
PT1007
CONNECTOR, COAX
PT1010
CONNECTOR
81318 & ON
08232 & ON
PT1011
CONNECTOR
PT1012
CONNECTOR
PT1013
CONNECTOR
PT1014
CONNECTOR
PT1015
CONNECTOR
PT1016
CONNECTOR
PT1017
CONNECTOR
PT1018
CONNECTOR
PT1019
CONNECTOR
PT1020
CONNECTOR
PT1021
CONNECTOR
PT1022
CONNECTOR
PT1023
CONNECTOR
PT1024
CONNECTOR, COAX
18281601 - 18281875
18208406 - 18208668
PT1025
CONNECTOR, COAX
18281601 - 18281875
18208406 - 18208668
PT1026
CONNECTOR, COAX
18281601 - 18281875
18208406 - 18208668
PT1027
CONNECTOR, COAX
18281601 - 18281875
18208406 - 18208668
PT1029
CONNECTOR, COAX
PT1030
CONNECTOR, COAX
PT1031
CONNECTOR, COAX
PT1045
CONNECTOR
PT1046
CONNECTOR
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 22 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PT1047
CONNECTOR
PT1048
CONNECTOR
PT1049
CONNECTOR
PT1050
CONNECTOR, COAX
PT1051
CONNECTOR
PT300
CONNECTOR, PITCH SERVO
Connects to UT300 pitch trim actuator located in tail.
PT301
CONNECTOR, PITCH TRIM ACTUATOR
Connects to UT301 pitch trim actuator located in tail.
PT302
CONNECTOR, KG102 DIGITAL GYRO
PT303
CONNECTOR
PT304
CONNECTOR
PT305
CONNECTOR
PT306
CONNECTOR
PT307
CONNECTOR, INTEGRATED AVIONIC 2
PT308
CONNECTOR
Integrated avionics #1
PT309
CONNECTOR
PT311
CONNECTOR
PT312
CONNECTOR
PT313
CONNECTOR
PT314
CONNECTOR
PT315
CONNECTOR
PT316
CONNECTOR
PT317
CONNECTOR
PT401
CONNECTOR, WX-500
PT402
CONNECTOR, WX-500
PT403
CONNECTOR, WX-500
PT502
CONNECTOR KIT, GSR 56
PT700
CONTACT
PT702
CONNECTOR
PT705
CONNECTOR
PT707
CONNECTOR
PT708
CONNECTOR
PT710
GTS 800, TRAFFIC ADVISORY SYSTEM
PT711
GTS 800, TRAFFIC ADVISORY SYSTEM
PT712
GTS 800, TRAFFIC ADVISORY SYSTEM
PT800
CONNECTOR
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 23 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
PT801
CONNECTOR, COAX
PT900
CONNECTOR
PT901
CONNECTOR
PT902
CONNECTOR
PT903
CONNECTOR
PT905
CONNECTOR
PV001
CONNECTOR, TAIL/STINGER DISCONNECT
Connects to FV001 vertical tail navigation light located in base of vertical tail.
PV003
CONNECTOR, VERTICAL TAIL DISCONNECT
PV004
CONNECTOR, BEACON LIGHT DISCONNECT
Connects to JV004 beacon light disconnect located in top of vertical tail.
PV005
CONNECTOR, VERTICAL TAIL DISCONNECT
Connects to JV005 vertical tail disconnect located in base of vertical tail.
PV1000
CONNECTOR, COMM 1 ANTENNA
PV1001
CONNECTOR, COMM 1 ANTENNA
PV1002
CONNECTOR, COMM 1 ANTENNA
PV1002
CONNECTOR
PV1003
CONNECTOR
PZ900
CONNECTOR, AVIONICS CIRCUIT BREAKER
Connects to HI106 circuit breaker behind instrument panel on left side.
PZ905
CONNECTOR KIT
PZ906
CONNECTOR
Q1
REGULATOR VOLTAGE, ADJUSTABLE
Pilot dome light.
Q2
REGULATOR VOLTAGE, ADJUSTABLE
Copilot dome light regulator.
QC001
REGULATOR VOLTAGE, ADJUSTABLE
Located behind overhead console in cabin.
QI001
REGULATOR VOLTAGE, ADJUSTABLE
Connects to PI029 glareshield light regulator disconnect located behind center instrument panel.
QI002
REGULATOR VOLTAGE, ADJUSTABLE
QZ001
REGULATOR, VOLTAGE
QZ002
REGULATOR, VOLTAGE
QZ003
REGULATOR, VOLTAGE
R1
POTENTIOMETER
R1
POTENTIOMETER
R1
RESISTOR
Left and right fuel quantity signal conditioner assembly.
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
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Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
81318 & ON
8232 & ON
R2
RESISTOR
Left and right fuel quantity signal conditioner assembly.
81318 & ON
8232 & ON
R3
RESISTOR
Left and right fuel quantity signal conditioner assembly.
81318 & ON
8232 & ON
RC001
POTENTIOMETER, DOME LIGHT
Located with pilot dome light regulator in overhead console.
RC002
RESISTOR
Located with pilot dome light potentiometer in overhead console.
RC003
RESISTOR
Located with pilot dome light potentiometer in overhead console.
RC004
POTENTIOMETER, PILOT FLOOD LIGHT
RC100
CONNECTOR
RF002
RESISTOR
RF003
RESISTOR
RF004
POTENTIOMETER, COPILOT FLOOD LIGHT
RI001
RESISTOR, GLARESHIELD/PEDESTAL LIGHTING
In dimming control module located behind center instrument panel.
RI002
RESISTOR, RADIO/INSTRUMENT LIGHTING
In dimming control module located behind center instrument panel.
RI003
RESISTOR
RI004
RESISTOR
In dimming control module located behind center instrument panel.
RI005
RESISTOR
In dimming control module located behind center instrument panel.
RI006
RESISTOR, AVIONICS DIMMING
Located behind left instrument panel.
RI007
RESISTOR, PEDESTAL DIMMING
Located behind left instrument panel.
RI008
RESISTOR, SWITCH/CIRCUIT BREAKER PANEL DIMMING
Located behind left instrument panel.
RI009
RESISTOR, STANDBY INDICATORS DIMMING
Located behind left instrument panel.
RI010
RESISTOR
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Retain printed data for historical reference only. For future maintenance, use only current data.
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Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
RI011
RESISTOR
Located behind left instrument panel.
RI012
RESISTOR
Located behind left instrument panel.
RN001
NIPPLE, LEFT MAGNETO
RN002
NIPPLE, RIGHT MAGNETO
RR001
RESISTOR, FLAP ACTUATOR ASSEMBLY
RR002
RESISTOR, FLAP ACTUATOR ASSEMBLY
RR900
RESISTOR
RZ001
RESISTOR, VARIBLE DIMMING
RZ001
RESISTOR, VARIBLE DIMMING
RZ002
RESISTOR, VARIBLE DIMMING
RZ002
RESISTOR, VARIBLE DIMMING
RZ003
RESISTOR, VARIBLE DIMMING
RZ003
RESISTOR, VARIBLE DIMMING
RZ005
RESISTOR, VARIBLE DIMMING
RZ006
RESISTOR, VARIBLE DIMMING
S1
SWITCH, CONTROL WHEEL MICROPHONE
S1
SWITCH, CONTROL WHEEL MICROPHONE
S2
SWITCH, AUTOPILOT DISC
S3
SWITCH, PITCH TRIM
S4
SWITCH, PITCH TRIM
SC001
SWITCH, COPILOT DOME LIGHT
Located in overhead console in cabin.
SC002
SWITCH, PILOT DOME LIGHT
Located in overhead console in cabin.
SC004
SWITCH, REAR DOME LIGHT
Located in overhead console in cabin.
SI001
SWITCH, AVIONICS MASTER
SI001
SWITCH, AVIONICS MASTER
SI002
SWITCH, IGNITION
SI003
SWITCH, ANNUNCIATOR TEST
SI004
SWITCH, ANNUNCIATOR TEST
SI005
SWITCH, ANNUNCIATOR TEST
SI006
SWITCH, ANNUNCIATOR TEST
SI007
SWITCH, FLAPS UP
SI008
TERMINAL, FLAPS DOWN, SWITCH
SI009
SWITCH, MASTER
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
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Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
SI010
SWITCH, AVIONICS MASTER
SI013
SWITCH
SI014
SWITCH, LANDING LIGHT
SI015
SWITCH, TAXI LIGHT SWITCH
SI016
SWITCH, NAVIGATION LIGHT SWITCH
SI017
SWITCH, STROBE LIGHT
SI018
SWITCH, FUEL PUMP
SI019
SWITCH, PITOT HEAT
SI020
SWITCH, PROP HEAT
SI021
SWITCH, STANDBY BATTERY
SI022
THERMOSTAT
SI023
SWITCH, CABIN POWER
SI034
SWITCH, LANDING RECOGNITION TAXI LIGHTS
SI036
SWITCH
SI037
SWITCH
SI300
SWITCH
SI302
INSTALL KIT
SI900
SWITCH, ELT INDICATOR
SI900
SWITCH, ELT INDICATOR
SL001
DETECTOR, STALL WARNING
SN001
SWITCH, OIL PRESSURE
SN011
SWITCH, VACUUM
SN012
SWITCH, VACUUM
SR001
TERMINAL, UP LIMIT SWITCH
SR002
SWITCH, DOWN LIMIT
TF001
PROBE, OUTSIDE AIR TEMPERATURE (OAT)
TF002
PROBE, OUTSIDE AIR TEMPERATURE (OAT)
TI001
THERMOCOUPLE
TL001
HEATER, PITOT
TL003
PROBE, OUTSIDE AIR TEMPERATURE
TN001
HEATER, PROPELLER
TN002
HEATER, PROPELLER
TN003
HEATER, PROPELLER
U100
COUPLER, ANTENNA
U1
SENSOR, CURRENT
U1
CONVERTER, POWER
U1
SENSOR, CURRENT
AIRCRAFT EFFECTIVITY WITHOUT NAV III OPTION IS 18281476 & ON, 1828337 & ON
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 27 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
UC001
BATTERY
UC001
BATTERY
UC001
TIMER/MONITOR, PROPELLER DEICE
UC003
TIMER
08001 & ON
UC007
BATTERY, STANDBY
UC1002
ANTENNA, COMM 2
UC1004
ANTENNA, GPS
UC1006
ANTENNA, TRANSPONDER
UC1007
ANTENNA, COMM
UC1008
ANTENNA, GPS
UC1010
ANTENNA, GPS 2
UC300
SPEAKER
UC500
SPEAKER
UC600
ANTENNA, KA-44B ADF
UC800
TRANSPONDER
UC901
FAN, AVIONICS COOLING
Forward of left instrument panel.
UF002
HORN ASSEMBLY, STALL WARNING
UF003
TRANSDUCER, VACUUM PRESSURE
UF005
FUEL PUMP
18281318 & ON 18208232 & ON
UF009
FUEL PUMP
J182T00001& ON
UF1001
ANTENNA, MARKER BEACON
UF1002
ANTENNA, COMM
UF1004
ANTENNA, STORMSCOPE
UF1010
ANTENNA, GPS 1
UI001
POWER SUPPLY, INVERTER
UI001
MODULE KIT, CONFIGURATION
UI005
ANNUNCIATOR PANEL
UI006
TRANSDUCER, OIL PRESSURE
UI007
ANNUNCIATOR PANEL
UI008
COMPUTER, ENGINE/AIRFRAME MONITOR
UI014
SWITCH PANEL, LED LIGHTED
UI015
SWITCH PANEL, LED LIGHTED
UI016
SWITCH PANEL, LED LIGHTED
UI017
SWITCH PANEL, LED LIGHTED
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 28 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
UI018
SWITCH PANEL, LED LIGHTED
UI021
CONSOLE COVER, LED PANEL
18282046 & ON
18208807 J182T00001 & ON & ON
UI026
RH SWITCH AND CIRCUIT BREAKER PANEL
UI300
COMPUTER, KC140 WING LEVELER
Located in audio panel in the center instrument panel.
UI302
GYRO, DIRECTIONAL
Located in left instrument panel.
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI303
COMPUTER, KC140 AUTOPILOT WITH ALTIMETER
Located behind center instrument panel.
80945 - 80967
8001 - 8001
UI303
COMPUTER, KC140 AUTOPILOT WITH ALTIMETER
Located behind center instrument panel.
80968 - 81144
8002 - 8160
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
81145 - 81232
8161 - 8206
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
81233 - 81289
8207 - 8224
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
81290 & ON
8225 & ON
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI303
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 29 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
UI304
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI304
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI304
COMPUTER, KC140 AUTOPILOT WITH ALTIMETER
Located behind center instrument panel.
80945 - 80967
8001 - 8001
UI304
COMPUTER, KC140 AUTOPILOT WITH ALTIMETER
Located behind center instrument panel.
80968 - 81144
8002 - 8160
UI304
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
81145 - 81232
8161 - 8206
UI304
COMPUTER, KC140 AUTOPILOT WITH ALTIMETER
Located behind center instrument panel.
81233 - 81289
8207 - 8224
UI304
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
81290 & ON
8225 & ON
UI304
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI304
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI304
COMPUTER, KC140 AUTOPILOT
Located behind center instrument panel.
UI304
AUTOPILOT COMPUTER
UI305
MODULE, CONFIGURATION
Located in center instrument panel on left side of KC140 flight computer.
UI307
INDICATOR, TURN COORDINATOR
Located in left instrument panel.
80001 - 81227
08001 - 08204
UI307
TURN COORDINATOR
81228 & ON
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 30 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
08205 & ON
UI308
INDICATOR, HORIZONTAL SITUATION
Located in center of left insturment panel.
UI309
INDICATOR, HORIZONTAL SITUATION
Located in center of left insturment panel.
UI310
SLAVE, NAV
UI311
SLAVE, NAV
UI312
DISPLAY, MULTIFUNCTION
UI313
COMPUTER, AIR DATA
UI317
DISPLAY, PRIMARY FLIGHT
UI406
DISPLAY, MULTIFUNCTION
UI500
AUDIO CONTROL
Located on center instrument panel.
UI501
RECEIVER, KX155 NAV/COMM
UI502
RECEIVER, KX155 NAV/COMM
UI503
RECEIVER, NAV/COMM
UI507
PANEL, KMA-26 AUDIO
Located on center instrument panel.
UI507
PANEL, KMA26 AUDIO
Located on center instrument panel.
UI507
PANEL, KMA-26 AUDIO
Located on center instrument panel.
UI508
PANEL, KMA-26 AUDIO
Located on center instrument panel.
UI508
PANEL, KMA26 AUDIO
Located on center instrument panel.
UI508
PANEL, KMA26 AUDIO
Located on center instrument panel.
UI510
NAV/COMM, KX-155A
UI511
RECEIVER, NAV/COM
UI512
NAV/COMM, KX-155A
UI516
AUDIO PANEL, KMA28
UI517
PANEL, AUDIO
UI518
RECEIVER, NAV/COMM
UI519
RECEIVER, NAV/COMM
UI531
PANEL, AUDIO
UI532
PANEL, AUDIO
UI600
NAV INDICATOR, KI-209
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 31 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
UI601
INDICATOR
UI602
RECEIVER, KR-87 ADF
UI603
ADF INDICATOR, KI-227
UI604
INDICATOR, NAVIGATION
Located on inboard edge of left instrument panel.
80631 & ON
8001 & ON
UI604
INDICATOR, NAVIGATION
Located on inboard edge of left instrument panel.
UI604
INDICATOR, NAVIGATION
Located on inboard edge of left instrument panel.
UI610
INDICATOR, GLIDESLOPE
UI700
RECEIVER, KLN-89 GPS
UI701
GPS RECEIVER, KLN-94
UI702
MODE SELECTOR, GPS
UI703
MODE SELECTOR, GPS
UI704
SWITCHING UNIT, NAVIGATION
UI705
SWITCHING UNIT, NAVIGATION
Located on upper left side of audio panel in center instrument panel.
UI800
TRANSPONDER
80945 - 81297
08001 - 08225
UI800
TRANSPONDER
UL001
POWER SUPPLY, LEFT STROBE
Located on left wing tip.
UL002
TRANSMITTER, LEFT FUEL QUANTITY
UL003
POWER SUPPLY, LEFT STROBE
Located on left wing tip.
UL004
SIGNAL CONDITIONER, FUEL QUANTITY
UL005
BALLAST KIT
Located on left outboard leading edge of left wing.
UL006
BALLAST KIT
Located on left outboard leading edge of left wing.
UL008
LED LIGHT, LEFT
UL301
TRANSMITTER, FLUX
UL302
MAGNETOMETER
UN003
PROBE, CYLINDER HEAD TEMPERATURE
UN004
SENSOR, OIL TEMPERATURE
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
Page 32 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
UN005
PROBE, EGT
80001 - 80474
UN005
PROBE, EGT
80475 - 80626
UN005
PROBE, EGT
80627 & ON
UN006
TRANSDUCER, PRESSURE
UN007
PUMP, FUEL
UN008
PROBE, TIT
80004 & ON
UN011
TRANSDUCER
UN014
PROBE, CYLINDER HEAD 1 EGT
UN015
PROBE, CYLINDER HEAD 2 EGT
UN016
PROBE, CYLINDER HEAD 3 EGT
UN017
PROBE, CYLINDER HEAD 4 EGT
UN018
PROBE, CYLINDER HEAD 5 EGT
UN019
PROBE, CYLINDER HEAD 6 EGT
UN020
PROBE, CYLINDER HEAD 1 CHT
UN021
PROBE, CYLINDER HEAD 2 CHT
UN022
PROBE, CYLINDER HEAD 3 CHT
UN023
PROBE, CYLINDER HEAD 4 CHT
UN024
PROBE, CYLINDER HEAD 5 CHT
UN025
PROBE, CYLINDER HEAD 6 CHT
UN026
PROBE, TIT
UN028
SENSOR, TACHOMETER
UN031
SENSOR, TACHOMETER
UR001
POWER SUPPLY, RIGHT STROBE
Located on right wing tip.
UR002
TRANSMITTER, RIGHT FUEL QUANTITY
UR003
POWER SUPPLY, RIGHT STROBE
Located on right wing tip.
UR004
SIGNAL CONDITIONER, FUEL QUANTITY
UR008
LED LIGHT, RIGHT
UR300
ACTUATOR, ROLL SERVO
Located on trailing edge of right wing.
UR301
ACTUATOR, ROLL SERVO
Located on trailing edge of right wing.
UR301
ACTUATOR, ROLL SERVO
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Page 33 of 34
Print Date: Mon Jul 02 05:08:47 CDT 2018
Model 182S/182T/T182T Wiring Diagram Manual (Rev 9)
-0 (Rev 9)
Located on trailing edge of right wing.
UR301
ACTUATOR, ROLL SERVO
UT300
PITCH, KC270C SERVO
Located in tailcone on right side at FS156.00
UT300
PITCH, KC270C SERVO
Located in tailcone on right side at FS156.00.
UT301
ACTUATOR, PITCH TRIM
Located in tailcone on left side.
UT301
ACTUATOR, PITCH TRIM
Located in tailcone on left side.
80004 - 80715
UT301
ACTUATOR, PITCH TRIM
Located in tailcone on left side.
UT301
ACTUATOR, PITCH TRIM
UT302
DIRECTIONAL GYRO
UT303
CONVERTER, NAV
UT304
INTEGRATED AVIONICS UNIT 1
UT307
INTEGRATED AVIONICS UNIT 2
UT314
AHRS
UT401
STORMSCOPE, WX-500
UT402
STORMSCOPE
UT403
STORMSCOPE, WX-500
UT800
TRANSPONDER, GTX33
UT900
BUZZER, SONALERT
UT901
FAN, AVINONICS COOLING
UV1001
ANTENNA, NAVIGATION
UV1003
ANTENNA, NAVIGATION
X1
TERMINAL BLOCK ASSEMBLY
X2
TERMINAL BLOCK ASSEMBLY
XN001
BRUSH BLOCK ASSEMBLY, PROPELLOR DEICE
Copyright © Textron Aviation Inc.
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