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CESSNA
SECTION 6
MODEL 182T NAV Ill
WEIGHT AhlD BALANCE/EQUIPMENT LlST
COMPREHENSIVE EQUIPMENT LlST
Figure 6-9 is a comprehensive list of all Cessna equipment which is available
for the Model 182T airplane equipped with Garmin GlOOO Integrated Cockpit
System. This comprehensive equipment list provides the following information in
column form:
In the ITEM NO column, each item is assigned a coded number. The first
two digits of the code represent the identification of the item within Air
Transport Association Specification 100 (1 1 for Paint and Placards; 24 for
Electrical Power; 77 for Engine Indicating, etc.).
These assignments also
correspond to the Maintenance Manual chapter for the airplane.
After the
first two digits, items receive a unique sequence number (01, 02, 03, etc.).
After the sequence number, a suffix letter is assigned to identify equipment
as a required item, a standard item or an optional item.
Suffix letters are as follows:
R= Required items or equipment for FAA certification (14 CFR Part 23
or Part 91).
S= Standard equipment items.
O= Optional equipment items replacing required or standard items.
A= Optional equipment items which are in addition to required or
standard items.
In the EQUIPMENT LlST DESCRIPTION column, each item is assigned a
descriptive name to help identify its function.
In the REF DRAWING column, a Cessna drawing number is provided which
corresponds to the item.
NOTE
I
If additional equipment is to be installed, it must be done in
accordance with the reference drawing, service bulletin or a
separate FAA approval.
In the WT LBS and ARM INS columns, information is provided on the weight
(in pounds) and arm (in inches) of the equipment item.
NOTE
Unless otherwise indicated, true values (not net change
values) for the weight and arm are shown.
Positive arms
are distances aft of the airplane datum; negative arms are
distances forward of the datum.
.Asterisks
(*)
in the weight and arm column indicate
complete assembly installations.
Some major components
of the assembly are listed on the
lines immediately
following.
The sum of these major components does not
necessarily equal the complete assembly installation.
U.S.
6-19
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