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Model |
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Aircraft / Solid State |
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Ground
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Volts: |
18-55 |
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Current: |
25 Amps |
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GC-28B-25 INSTALLATION INFORMATION
| ( Requires Adobe Acrobat Reader ) Version 5.0 / PDF Format |
|---|
| Aircraft Instillation Schematic Page 1 File Size: 100K or Less |
FAA Approval: Use Form AC4313 Sub Section 1-B for installation of this unit.
Specifications for system operation <--- CLICK HERE to open / Close
GENERAL SYSTEM OPERATION
THE SYSTEM IS DESIGNED TO TURN ON AN AIRCRAFT COMMUNICATION
RADIO AND / OR AUDIO PANEL WITH A SINGLE PUSH BUTTON SWITCH. WHEN THE BATTERY
MASTER SWITCH IS TURNED ON THE GC-28B--25 IS DESIGNED TO DISENGAGE FROM THE BATTERY
AND CONNECT TO THE REGULAR AVIONICS POWER BUS.
GROUND CLEARANCE SWITCH
ALMOST ANY STANDARD PUSH BUTTON SWITCH WILL WORK. A SNAP ACTION SWITCH IS
RECOMMENDED WITH A LIGHT TO SHOW ACTIVATION OF THE GROUND CLEARANCE CIRCUIT FOR
THE PILOT. (REFER TO SCHEMATIC FOR CORRECT INSTALLATION).
THE GROUND CLEARANCE SWITCH SHOULD USE 22 GA WIRE
FROM THE SWITCH TO THE GC-28B-25 THE CONTINUOUS SWITCH CURRENT, IF
HELD DOWN, WILL BE APPROXIMATELY 15 mA.
1 Year Warranty
Meets All: FAA DO-160A Standard Specifications & Category Z
Homepage: Http://\www.Exec-Eng.com/