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Related Manuals for FDS FD151CV-C-HT
Summary of Contents for FDS FD151CV-C-HT
- Page 1 Revision Date: Rev: Document Number: 05/05/2017 MAN – FD151CV-C-HT Page 1 of 11 Installation and Operation Manual FD151CV-C-HT 15” Heated LCD Display on Military Arm © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com...
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Page 2: Table Of Contents
Power and Ground Wiring ......................5 Power/Video ..........................6 Operation Instructions ........................7 Button Control ..........................7 Technical Drawing........................8 Technical Support ........................9 Instructions for Continued Airworthiness ................9 Warranty ............................10 Log of Revisions .........................11 © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com... -
Page 3: General Information
MAN – FD151CV-C-HT Page 3 of 11 General Information The FD151CV-C-HT is a special mission monitor mounted on a ruggedized arm. The unit includes an internally mounted heater to ensure the LCD maintains an optimal operating temperature in the harshest environments. -
Page 4: Specifications
Section 7, Category B Installation Instructions All cabin equipment, such as the FD151CV-C-HT, should be installed on a non-essential bus and have a dedicated circuit breaker. It is a requirement that a switch be installed in the cockpit so that the pilot can de-energize the system should it become necessary. -
Page 5: Wiring Suggestions
(www.deerfieldlab.com, (650) 632-4090). In most cases this should be added to the video output of the source. Power and Ground Wiring 20 AWG wire is recommended for Power and Ground applications. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com... -
Page 6: Power/Video
Rev: Document Number: 05/05/2017 MAN – FD151CV-C-HT Page 6 of 11 Power/Video Aircraft side connector (provided by FDS Avionics Corp.): D38999/20WC98SN – wall mounted receptacle with sockets M85049/38S13W – Strain relief back shell Pin Letter Description 28 VDC (MONITOR) GROUND (MONITOR) -
Page 7: Operation Instructions
MAN – FD151CV-C-HT Page 7 of 11 Operation Instructions The FD151CV-C-HT is continuously on but may be de-energized by removing power from the display system. No pilot or aircrew action is necessary during flight or ground operation. When applying 28VDC power, the display will turn on and look for a valid input. If no input is found, the display will go to standby mode. -
Page 8: Technical Drawing
Revision Date: Rev: Document Number: 05/05/2017 MAN – FD151CV-C-HT Page 8 of 11 Technical Drawing © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com... -
Page 9: Technical Support
05/05/2017 MAN – FD151CV-C-HT Page 9 of 11 Technical Support Should you have any questions concerning this product or other FDS Avionics Corp. products, please contact our Product Support representatives at 470-239-7421. FDS Avionics Corp. 6435 Shiloh Road Alpharetta, GA 30005... -
Page 10: Warranty
This warranty is not transferable. Any implied warranties expire at the express limited warranty expiration date. FDS shall not be held liable for any indirect, special, punitive, incidental or consequential damages. Some states do not allow limitation on the length of an implied warranty. In such states, the exclusions or limitations of this limited warranty may not apply. -
Page 11: Log Of Revisions
Initial Release Updated DO-160 Testing, Added Operating Temperature, 10/24/2011 Updated Warranty Info, updated photo 06/29/2012 Format and Warranty Update 5/5/2017 New Format, New Company Name, new Warranty © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com...
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