Specifications

PLEASE READ THE FOL -
LOWING IN STRUC TIONS
CARE FULLY!
TSO C126 PARA GRAPH D RE QUIRE -
MENTS:
“The con di tions and tests re quired
for TSO ap proval of this ar ti cle are
min i mum per for mance stan dards. It
is the re spon si bil ity of those de sir -
ing to in stall this ar ti cle on a spe -
cific type or class of air craft to
de ter mine that the air craft in stal la-
tion con di tions are within the TSO
stan dards. The ar ti cle may be in-
stalled only if fur ther eval u a tion b y
the ap pli cant doc u ments an ac cept
-
able in stal la tion and it is ap proved
by the ad min is tra tor.”
The ELT is de signed with the in staller
in mind. Ex tra ef fort has been made
to sim plify the in stal la tion pro cess.
Be cause of the crit i cal na ture of an
ELT, it is very im por tant that the in -
stal la tion be per formed ac cord ing to
the fol low ing in struc tions. In stal la tion
of the ELT is some what unique; it re-
quires ex pe ri ence in sheet metal work
and avi on ics. Only li censed tech ni -
cians should in stall the ELT.
Many prob lems as so ci ated with the
older ELTs were due to poor in stal la
-
tions. Many of those poor in stal la
-
tions oc curred at the fac tory o n
new air planes. There fore, du pli cat
-
ing a pre vi ous ELT in stal la tion with
the ARTEX ELT may not be ac cept
-
able.
In ad di tion to the pro ce dures out lined
herein, the in staller must ad here to
the guide lines es tab lished in
FAA-Advisory Cir cu lar 43.13-2A (Ac
-
cept able Methods, Tech niques a nd
Prac tices -Air craft Al ter ations). Spe
-
cifically, Chap ters 1 through 3, 11
and 13.
By sign ing ei ther the air craft log books
or the FAA Form 337, you are stat -
ing that the in stal la tion has been per
-
formed in ac cor dance with the cur rent
FARs and with the steps and pro ce -
dures out lined herein.
ARTEX AIRCRAFT SUPPLIES DOCUMENT #570-5000
06/30/99 PAGE 3-2
FIG URE 3-1 ELT AND RE MOTE SWITCH PANEL