Specifications

For in stal la tions us ing ELT/NAV In ter
-
face: Crimp a male ter mi nal pin (ARTEX
P/N 151-6627) to one end of each of the
wires which will run to the ELT/NAV In-
ter face unit (P/N 453-6500).
On the other end of each of the wires
which run to the ELT/NAV In ter face unit
sol der a con nec tor pin (ARTEX P/N
151-2100) as de scribed in the ELT/NAV
In ter face In stal la tion and Op er a tion Man ual
(570-4602).
NOTE: This ca ble may be con nected
now or af ter in stall ing ei ther the ELT or
the front panel switch as sem bly. All wir
-
ing must be in stalled in ac cor dance with
AC 43.13-1A.
3.6.2. Con necting the ELT
Re fer to Fig ures 3-9,3-10 and 3-11
Feed the crimp ter mi nated wires for the
12-pin con nec tor through the rect an gu lar
hole in the mount ing frame cap.
Fab ri cate a short jumper (about 1.5"
long) and in stall male ter mi nal pins on
each end. In stall the jumper be tween
pins 5 and 8 in the 12-pin re cep ta cle. In
-
stall the re main ing wires into the 12-pin
re cep ta cle as shown in Fig ures 3-10 and
3-11 Push the con nec tor into place in-
side the mount ing tray cap. The mount-
ing frame cap acts as a re tainer for the
con nec tor once the cap is in stalled on
the ELT.
Pin 1, as in scribed on the con nec tor,
must be in the lower left hand cor ner as
shown in Fig ures 3-10 and 3-11.
3.6.3. Wiring Switch As sem bly
9-pin Con nec tor
Be fore in sert ing the ca ble pins into the
9-pin con nec tor for the cock pit switch as
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ARTEX AIRCRAFT SUPPLIES DOCUMENT #570-5000
06/30/99 PAGE 3-15
2.25
2.25
1.125DIA
3.20
FIG URE 3-12 BUZZER BRACKET