SUBJECT
REF. MDL.
REPORT NO.
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
GA182
ICA182-2
Rev. A
10/15/12
SEE NON-DISCLOSURE NOTICE ON THE COVER PAGE
32 of 101
Copyright 2012
Eagle Copters
All Rights Reserved
Section 6.0 Cable Maintenance
6.1
General Notes
a.
The installation of the
Eagle Audio
GA182 Audio System requires
the
application of accepted aircraft equipment practices, according to
FAA
publication, AC43.13-1B,
ACCEPTABLE METHODS,
TECHNIQUES
AND PRACTICES, AIRCRAFT INSPECTION AND
REPAIR
,
and the
installer shall strictly comply with paragraph 428.a of
that Advisory
Circular.
b.
The requirement regarding the securing of wire bundles using
nonmetallic clamps is addressed by the use of nylon cable ties. The
part numbers and description of these ties is as follows:
Cable Tie Selection Chart
Thomas & Betts Brand
Cat.
No.
UPC
Bod Width
in.
Length
in.
Max. Wire
Bundle Dia. in.
Military Standard
Part No.
Tensile
Strength lbs.
TY23M 82436
.091
3.62
.625
MS3367-4
18
TY24M 82447
.140
5.50
1.125
MS3367-5
40
TY25M 82457
.184
7.31
1.750
MS3367-1
50
c.
Following
the guidelines in AC43.13-1B, cable ties are attached at a
maximum of 4” spacing and ties are attached to nylon cable tie
anchors, as necessary.
d.
The configuration of the wiring and cabling will vary from aircraft to
aircraft. The installation of the
Eagle
Audio System will not
change the
existing wiring or cabling, but rather will utilize existing wire
and cable
runs and will not interfere with the existing aircraft equipment
installations.
