Flash Technology VANGUARD FTS 370i-2, Справочное руководство

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FTS 370i-2 IR Revision A – 05/17/2019 iii
Front Matter
Abstract
This manual contains information and instructions for installing, operating and maintaining the
FTS 370i-2 IR LED Integrated Beacons.
Copyright
Copyright © 2019, Flash Technology
®
, Franklin, TN, 37067, U.S.A.
All rights reserved. Reproduction or use of any portion of this manual is prohibited without
express written permission from Flash Technology and/or its licenser.
Trademark Acknowledgements
Flash Technology
®
and Vanguard
®
are registered trademark names.
All trademarks and product names mentioned are properties of their respective companies and are
recognized and acknowledged as such by Flash Technology.
Applicable Specifications
The FTS 370i-2 IR beacon meets or exceeds requirements for an FAA Type L-864 beacon.
Additionally, the FTS 370i-2 IR beacon meets or exceeds requirements for an ICAO Annex 14,
Volume 1, 8
th
Edition Low Intensity Type B Obstacle Light.
Disclaimer
While every effort has been made to ensure that the information in this manual is complete,
accurate and up-to-date, Flash Technology assumes no liability for damages resulting from any
errors or omissions in this manual, or from the use of the information contained herein. Flash
Technology reserves the right to revise this manual without obligation to notify any person or
organization of the revision.
In no event will Flash Technology be liable for direct, indirect, special, incidental, or
consequential damages arising out of the use of or the inability to use this manual.
Warranty
Flash Technology warrants all components, under normal operating conditions, for 5 years.
Parts Replacement
The use of parts or components, in this equipment, not manufactured or supplied by Flash
Technology voids the warranty and invalidates the third party testing laboratory certification
which ensures compliance with FAA Advisory Circulars 150/5345-43J, 150/5345-53D, and
Engineering Brief No. 67D. The certification is valid as long as the system is maintained in
accordance with FAA guidelines (FR doc. 04-13718 filed 6-16-04).