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Related Manuals for FDS FD171CV VER TS
Summary of Contents for FDS FD171CV VER TS
- Page 1 Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 1 of 15 Installation and Operation Manual FD171CV VER TS 17.1” Widescreen Touchscreen LCD © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com...
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Page 2: Table Of Contents
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 2 of 15 Table of Contents General Information .........................3 Front View ..........................3 Additional Information ......................3 Specifications ..........................4 Installation Instructions ......................4 Power ............................4 Wiring Suggestions ........................5 S-Video/Composite and Audio Wiring ................5 VGA Wiring ..........................6... -
Page 3: General Information
Front View Additional Information The FD171CV VER TS utilizes a state of the art digital video decoding chipset for the analog VGA video input. The FD171CV VER TS can also be connected to existing video switchers and receive video inputs from a selector interface box. -
Page 4: Specifications
In Progress Installation Instructions All non-flight essential equipment, such as the FD171CV VER TS, 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 display should it become necessary. -
Page 5: Wiring Suggestions
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 5 of 15 Wiring Suggestions All shields should be grounded to the connector at the source, and floating at the display. Avoid routing video wiring parallel to: AC wiring ... -
Page 6: Vga Wiring
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 6 of 15 VGA Wiring Recommended cable for VGA purpose is ECS P/N 453005. This is a single shielded cable containing 5 separate coaxial cables, color-coded to match the functions of the wires. -
Page 7: Power And Ground Wiring
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 7 of 15 Power and Ground Wiring This is a 28VDC monitor that requires 1.5 amp of power to operate. To operate properly this monitor requires an input voltage of 18-29VDC. -
Page 8: Power/Video
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 8 of 15 Power/Video Pin out for P1 (High Density DB-15 Receptacle) Connector P/N: M24308/2-286 or Equivalent Crimp Contacts P/N: M39029/57-354 or Equivalent Description Number 28V DC Power... -
Page 9: Operations Instructions
Page 9 of 15 Operation Instructions The FD171CV VER TS is continuously on but can be de-energized by removing power from the unit at the circuit breaker panel or by cycling the power on/off bezel button on the top of the display. No pilot or aircrew action is necessary during flight or ground operation. -
Page 10: Remote Control
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 10 of 15 Remote Control © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com... -
Page 11: Technical Drawing #1
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 11 of 15 Technical Drawing © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com... -
Page 12: Technical Drawing #2
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 12 of 15 Technical Drawing © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvionics.com... -
Page 13: Technical Support
01/12/2017 MAN – FD171CV VER TS Page 13 of 15 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... -
Page 14: 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 15: Log Of Revisions
Revision Date: Rev: Document Number: 01/12/2017 MAN – FD171CV VER TS Page 15 of 15 Revisions Log Date Page Description 02/11/2013 Initial Release Company name change and formatting. No revision change 1/12/2017 necessary. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
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