User Manual

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

ELT

ARM