ACR&Artex C406-N - Manual (Page 91)

25-62-13
Page 91 of 109
MAR 1/13
ACR ELECTRONICS, INC / ARTEX PRODUCTS
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-N (453-5060), C406-N HM (453-5061)
APPENDIX C – REMOTE SWITCH CONTROL PANEL OPTION
TASK 25-62-13-870-801
1. Description and Operation
SUBTASK 25-62-13-870-001
A. Purpose
(1) The G737 control panel (453-0161) is an optional replacement for the standard 345-6196-04
cockpit remote switch.
(2) This panel is principally for use in Boeing aircraft, which are pre-wired for this type of ELT
control panel. However, this appendix does provide wiring instructions for aircraft that are not
provisioned for this type of panel.
(3) These instructions include installation of a buzzer modified for use with the Boeing
configuration. In addition, instructions and a wiring diagram are provided for installing the
standard buzzer with the remote switch control panel. The difference between the two buzzer
options is the means by which the buzzer is activated and controlled.
(a) The modified buzzer is activated by the “ELT ON” circuit and powered by the aircraft
battery.
(b) The standard buzzer is controlled and powered by the ELT.
SUBTASK 25-62-13-870-002
B. Control Panel Description
(1) The control panel is backlit panel comprised of an ELT status indicator light and a control
switch, which allows an operator to manually activate the ELT for testing and reset (i.e.,
deactivate) the ELT. See "Figure 31. Remote Switch Control Panel Assembly".
NOTE: The ELT CANNOT be disarmed or disabled from the cockpit. Cockpit operation is
limited to deactivating the ELT (i.e., reset) or manually activating the ELT.
Figure 31. Remote Switch Control Panel Assembly
ON
ELT
ELT
ARM