Textron Cessna 182S User Manual

CESSNA
AIRCRAFT COMPANY
MODEL 182/T182
WIRING DIAGRAM
MANUAL
INTRODUCTION
1. Coverage
A. The
Wiring Diagram Manual
is prepared in accordance
with Air Transport
Association Specification
100 for Manufacturer's
Technical
Data.
B. The information
in this publication
is based on data
available at the time
of publication and
is
updated, supplemented,
and automatically
amended
by all information
issued in Service
News
Letters, Service Bulletins,
Special Service
Projects, Supplier
Service Notices, Publication
Changes,
Revisions, Reissues
and Temporary Revisions.
All such
amendments become
part of and are
specifically
incorporated within
this publication.
Users are urged
to keep abreast of
the latest
amendments
to this publication
through information
available at Cessna
Authorized Service
Stations
or through the Cessna Product
Support subscription services. Cessna
Service Stations have
supplier
publications which
provide disassembly,
overhaul, and
parts breakdowns
for some of
the various
supplier equipment
items. Suppliers
publications are updated,
supplemented,
and
specifically amended
by supplier issued
revisions and service
information which may
be reissued by
Cessna,
thereby automatically
amending this publication
and are communicated
to the field
through
Cessna's Authorized
Service Stations and/or through
Cessna's subscription services.
WARNING:
ALL INSPECTION INTERVALS,
REPLACEMENT TIME
LIMITS,
OVERHAUL
TIME LIMITS,
THE METHOD
OF INSPECTION,
LIFE
LIMITS,
CYCLE
LIMITS, ETC.,
RECOMMENDED
BY CESSNA
ARE
SOLELY
BASED ON THE
USE OF
NEW, REMANUFACTURED,
OR OVERHAULED
CESSNA APPROVED
PARTS. IF PARTS
ARE
DESIGNED, MANUFACTURED,
REMANUFACTURED,
OVERHAULED, AND/OR
APPROVED BY ENTITIES
OTHER THAN
CESSNA,
THEN THE DATA IN CESSNA'S
MAINTENANCE/SERVICE
MANUALS AND
PARTS CATALOGS
ARE NO LONGER
APPLICABLE AND THE PURCHASER IS WARNED NOT TO RELY
ON SUCH DATA FOR
NON-CESSNA PARTS.
ALL INSPECTION
INTERVALS,
REPLACEMENT TIME
LIMITS, OVERHAUL TIME
LIMITS, THE METHOD
OF INSPECTION, LIFE LIMITS,
CYCLE
LIMITS,
ETC., FOR SUCH
NON-CESSNA PARTS MUST
BE
OBTAINED
FROM THE
MANUFACTURER
AND/OR
SELLER OF
SUCH
NON-CESSNA
PARTS.
C. Inspection,
maintenance
and parts requirements
for Supplemental
Type Certification
(STC)
installations
are not included in this manual. When
an STC installation is incorporated on
the
airplane, those portions of the
airplane affected by the installation must
be inspected in accordance
with the inspection program published
by the owner of the STC. Since STC
installations may change
systems interface,
operating characteristics
and component
loads or stresses
on adjacent structures.
Cessna provided inspection
criteria may not be valid for
airplanes with STC installations.
D. This manual
has been prepared
to assist personnel
in maintaining wiring
and electrical/electronic
components
in this airplane
and provides the necessary
information required
to troubleshoot,
remove
and replace components or repair systems.
E. Information
beyond the scope of
this manual may be
found in the Maintenance
Manual, Illustrated
Parts Catalog and Structural Repair
Manual. For technical assistance concerning
this manual, contact
Cessna
Aircraft Company, Propeller
Aircraft Product Support.
F. Technical Publications
available from
suppliers of various
components and systems,
which are not
covered in this manual, must be utilized
as required for maintenance of those
components.
© Cessna Aircraft Company
INTRODUCTION
Page 1
Mar
1/2004
I

Textron Cessna 182S Specifications

General

Brand	Textron
Model	Cessna 182S
Category	Tools
Language	English