ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
B406-4 (453-5004)
Page 50 of 70
25-62-03
TASK 25-62-03-450-803
4.
Remote Switch Panel
SUBTASK 25-62-03-450-001
A.
Location
NOTE:
In most cases, panel space and wiring have been pre-provisioned by the aircraft
manufacturer for the G737 control panel (remote switch panel assembly); however,
location and installation requirements are defined for installations in aircraft not
pre-provisioned for this remote switch panel.
1)
The Control Panel G737 (453-0161) must be mounted in the cockpit where the pilot can easily reach the
switch and see the status light.
2)
The panel assembly requires a space approximately 5.74 x 2.24 in. (146 x 57 mm) on the panel or
console surface, with a depth of 3.00 in. (77 mm), excluding room for the harness connection. See
Figure 18 Remote Switch Panel Assembly Outline and Dimensions.
Figure 18 Remote Switch Panel Assembly Outline and Dimensions
SUBTASK 25-62-03-450-002
B.
Installation
1)
Provide an opening in the instrument panel or other mounting location which meets the dimensional
requirements shown in Figure 18 Remote Switch Panel Assembly Outline and Dimensions.
2)
Mount Dzus rails on the sides of the opening, if necessary. See Figure 18 Remote Switch Panel Assembly
Outline and Dimensions for rail center line dimensions.
3)
Install the remote switch panel assembly.
NOTE:
Step (3) may be completed after wiring is completed on the ELT end and the harness plug
has been plugged into the panel assembly, in accordance with the requirements of
SUBTASK 25-62-03-450-008 on page 57. If such is the case, perform a fit check at this time.
4)
Apply a “For Aviation Emergency Use Only/Unauthorized Use Prohibited” placard as close to the switch
as practical, if required.
NOTE:
This placard is recommended for installations on aircraft that are not pre-placarded for
remote ELT control. If desired, the placard (591-0428) may be ordered from ACR
Electronics.
