FDS FD215CV-C-5 Installation And Operation Manual

FDS FD215CV-C-5 Installation And Operation Manual

21.5” widescreen hd display

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Revision Date:
Rev:
Document Number:
01/10/2017
MAN – FD215CV-C-5
B
Page 1 of 25
Installation and Operation Manual
FD215CV-C-5
21.5" Widescreen HD Display
© 2017 FDS Avionics Corp.
TECHNICAL SUPPORT
All Rights Reserved.
470-239-7421 or FDSAvioncis.com

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Summary of Contents for FDS FD215CV-C-5

  • Page 1 Revision Date: Rev: Document Number: 01/10/2017 MAN – FD215CV-C-5 Page 1 of 25 Installation and Operation Manual FD215CV-C-5 21.5” Widescreen HD Display © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 2: Table Of Contents

    Operation Instructions ......................12 Button Control .........................13 Quad Screen or Full Screen ..................... 14-20 Technical Drawing........................21 Technical Support ........................22 Instructions for Continued Airworthiness ................22 Warranty ...........................23 Revisions Log ...........................24 © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 3: General Information

    01/10/2017 MAN – FD215CV-C-5 Page 3 of 25 General Information The FD215CV-C-5 is a special mission HD monitor which is designed to be mounted in a standard 19-inch rack. Front View Additional Information The FD215CV-C-5 utilizes a state of the art digital video decoding chipset for all video inputs.
  • Page 4: Specifications

    3A – 20µs Installation Instructions All cabin equipment, such as the FD215CV-C-5, should be installed on a non-essential bus and have a dedicated circuit breaker. The FD215CV-C-5 is designed to mount into a standard electronics rack using (4) 10-32 Machine screws.
  • Page 5: Wiring Suggestions

     Inverter cabling  Or any other potential noise source. We recommend coax cables be terminated using solder sleeve coaxial cable terminators such as Raychem Part Number CWT-4174-W122-5/9. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 6: Power And Ground Wiring

    Also, use short heavy gauge wire and a clean tight connection for ground. It is the installer's responsibility to understand the product's requirements to install the product in compliance with industry standards and safety. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
  • Page 7: Rear Panel Connectors And Configurations

    Scaler PCBs inside the monitor. Slave mode permits an external device to take control of the two internal subsystems . Set “Down” or “off” to put controller in Slave mode. Set the switch “up” ” to put controller in Master mode. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 8: Power/Video

    Power – D38999 connector (supplied) Connector P/N: D38999/26FB5SA or Equivalent Crimp Contacts P/N: M39029/56-351 or Equivalent Description Number 18-33 VDC Power 18-33 VDC Power 18-33 VDC Ground 18-33 VDC Ground © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 9 Revision Date: Rev: Document Number: 01/10/2017 MAN – FD215CV-C-5 Page 9 of 25 © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 10 Red Video Green Video Blue Video DDC Return (Optional) Red Return Green Return Blue Return Sync Ground DDC Data (Optional) Horizontal Sync Vertical Sync DDC Clock (Optional) © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 11: Pin Outs

    5 inches. This maximum length can be used if 100 Ohm low capacitance shielded twisted pair cable is used. Reduce length if the cable does not fully meet the USB specifications for best results. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
  • Page 12 DDC data TMDS data 1- TMDS data 1+ TMDS data 1 shield +5 V Ground Hot plug detect TMDS data 0- TMDS data 0+ TMDS data 0 shield © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 13: Operation Instructions

    The FD215CV-C-5 is continuously on but can be de-energized by removing power from the video system. No pilot or aircrew action is necessary during flight or ground operation. The operator will be able to change the video output from the FD215CV-C-5 using the video source select button on the display.
  • Page 14: Button Control

    Page 14 of 25 Button Controls Located on the front right of the FD215CV-C-5 are two sets of 4 buttons. These buttons are used to power up the unit and navigate through the different menus. The menu button is used as a toggle, push to view the menu screens, push again to exit.
  • Page 15: Quad Screen Or Full Screen

    This display has the capability to display a quad screen or full screen from any of the four HDSDI inputs. The image seen here is the bottom view of the FD215CV-C-5 Widescreen HD Monitor. Connecting the SDI input to the output of the attached quad box on the unit will enable the operator to view any image from any of the connected screens on board the aircraft.
  • Page 16 4) The video channel (DVI or VGA) associated with KVM channel 1 by the rear panel dip switch is stored in Volatile memory as the last requested computer source. 5) The Quad view of the four SDI inputs is stored in Volatile memory as the last requested video source. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
  • Page 17 Overall Button Operation: Video Select buttons accept Long press and Short press commands. Long Press (LP) button function: press and hold for > ¾ second. Activation is at time-out (release not required). © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
  • Page 18 Long Press (LP) of COMP moves that computer input to Main and turns PIP Off o Returning to PIP with COMP in the Main window, displays the last used video input in the PIP window © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
  • Page 19 With PIP On: Swaps sources between Main window and PIP window o With PIP Off: Swaps sources (computer or video) on the Main window © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
  • Page 20 Long Press (LP) moves that video source to the Main window and turns PIP Off o Returning to PIP with the selected video source (1, 2, 3, or 4) in the Main window, displays COMP in the PIP window © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved.
  • Page 21  Long Press moves QUAD video input to Main and turns PIP Off o Returning to PIP with QUAD in the Main window, displays COMP in the PIP window © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 22: Technical Drawing

    Revision Date: Rev: Document Number: 01/10/2017 MAN – FD215CV-C-5 Page 22 of 25 Technical Drawing © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...
  • Page 23: Technical Support

    01/10/2017 MAN – FD215CV-C-5 Page 23 of 25 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 24: Warranty

    Warranty Information All FDS Avionics Corp. (FDS) products are warranted to be free from material or manufacturing defects for a period of 24 months from the date of shipment for General Aviation customers or 12 months from the date of shipment for Government/Special Mission customers.
  • Page 25: Revisions Log

    Updates including pin out changes; additional instruction on KVM 06/10/2013 Switch functionality; user friendly explanation added for PIP/Quad Functions Company name change and formatting – No revision change 1/10/2017 necessary. © 2017 FDS Avionics Corp. TECHNICAL SUPPORT All Rights Reserved. 470-239-7421 or FDSAvioncis.com...

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