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Document Number: 

MAN 

– FD215CV-C-5

 

Rev: 

B

 

Revision Date: 

01/10/2017 

Page 24 of 25 

 

 

©

 

2017 FDS Avionics Corp.  

All Rights Reserved. 

TECHNICAL SUPPORT 

470-239-7421 or FDSAvioncis.com

 

 

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.   Any material  or  repair  workmanship  for  in  warranty  repair  service  will  be 
specifically warranted for 90 days or the remainder of the original warranty period, whichever is longer.  If the original 
warranty  period has expired,  the  90  day  repair  warranty  is  limited  to  the material  and  workmanship specific  to  the 
repair activity completed. 

The following conditions are exclusions to warranty coverage: 

1.  Labor costs associated with installation, removal or reinstallation of any product. 
2.  Damage to or malfunction caused by any unauthorized alteration made to the product. 
3.  Resolving  signal  quality  issues  caused  by  externally  generated  noise  introduced  by  aircraft  electrical 

systems or other components connected to any FDS product. 

4.  Any  malfunction  caused  by  improper  installation  or  connection  to  aircraft  wiring,  industry  standard  cabin 

management/ inflight entertainment systems, or third party commercial equipment not specifically identified 
as compatible with FDS products. 

5.  Any  malfunction  caused  by  installation  that  does  not  conform  to  precautions  associated  with  operating 

environments  listed  in  the  operating  manual  or  consistent  with  industry  best  practices  such  as;  high 
temperature, adequate ventilation, high humidity, high dust, or power surges. 

6.  Cosmetic  damage  or  damage  to  internal  components  caused  by  installation  or  removal,  failure  to  follow 

installation or operating instructions, or any neglect or misuse of the product. 

7.  Any product that is returned for service with a broken tamper evident seal, indicating tampering or improper 

handling of the product by an unauthorized person. Violation of product tamper evident seals or modification 
of factory installed serial and PMA labels voids any warranty, either expressed or implied. 

The  FDS  technical  support  team  is  available  to  provide  distance  troubleshooting  support  during  business  hours 
(8:00am to 5:00pm EST) Monday through Friday at (470) 239-7421. 
 
Many  repair  requests  can  be  resolved  through  distance  support and may  not  require  return  of merchandise  to  the 
factory.    If  a  product  must  be  returned  to  the  factory  for  repair,  an  RMA  number  will  be  issued  as  directed  by  the 
technical support team and communicated by the repair coordinator.   
 
Upon  request  by  the  customer,  FDS  may  send  a  service  technician  onsite  to  repair  any  non-PMA  products.    The 
travel expenses incurred to include transportation, lodging and meals along with the technician’s hourly rate shall be 
payable by the customer in accordance with FDS’ applicable rates and procedures. 
 
FDS Avionics Corp. will, upon receipt of returned merchandise, remanufacture or replace the unit at our discretion 
and return the product by Ground Return Shipping.  Express return shipment will be the responsibility of the sender. 
 
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. 

Содержание FD215CV-C-5

Страница 1: ...D215CV C 5 Rev B Revision Date 01 10 2017 Page 1 of 25 2017 FDS Avionics Corp All Rights Reserved TECHNICAL SUPPORT 470 239 7421 or FDSAvioncis com Installation and Operation Manual FD215CV C 5 21 5 W...

Страница 2: ...3 Front View 3 Additional Information 3 Specifications 4 Installation Instructions 4 Power 4 Wiring Suggestions 5 Power and Ground Wiring 6 Rear Panel Connectors and Configurations 7 8 Power Video 8...

Страница 3: ...n 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 input...

Страница 4: ...V DC 3 Amps PC Video Input Analog RGB VGA HD SDI Digital DVI D Video Type Supported NTSC PAL Viewing Angle 170 Horizontally 160 Vertically Materials Aluminum Inrush Current 17A max current 3A 20 s Ins...

Страница 5: ...er should be grounded to the connector at the source and left floating at the display Shields for USB SDI data and video should be connected at both ends Avoid routing video wiring parallel to AC wiri...

Страница 6: ...cting wire gauge The following example is based on an install with a 28VDC power system and a total of 50 feet of wire between the circuit breaker monitor and ground Example 22awg wire has 16 2 Ohms p...

Страница 7: ...n position for VGA input Set switch in up position for DVI input Switch 5 configures the monitor to support either the Raritan Switchman KVM switch or the Adderview Pro KVM Switch Set switch in down p...

Страница 8: ...Rights Reserved TECHNICAL SUPPORT 470 239 7421 or FDSAvioncis com Power Video Power D38999 connector supplied Connector P N D38999 26FB5SA or Equivalent Crimp Contacts P N M39029 56 351 or Equivalent...

Страница 9: ...Document Number MAN FD215CV C 5 Rev B Revision Date 01 10 2017 Page 9 of 25 2017 FDS Avionics Corp All Rights Reserved TECHNICAL SUPPORT 470 239 7421 or FDSAvioncis com...

Страница 10: ...epts Industry Standard VGA connection HD15 plug supplied Connector P N M24308 4 260 or Equivalent Crimp Contacts P N M39029 58 360 or Equivalent Pin Number Description 1 Red Video 2 Green Video 3 Blue...

Страница 11: ...board is set to USB1 0 mode in order to permit maximum flexibility in the choice of components used for the cable and connectors that are used between the monitor and the USB host or KVM switch USB s...

Страница 12: ...Standard 75 BNC Plug RG179 connector supplied DVI D Accepts a standard DVI D Single Link male connector supplied View into mounted receptacle Pin Number Description 1 TMDS data 2 2 TMDS data 2 3 TMDS...

Страница 13: ...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 th...

Страница 14: ...nt menus The menu button is used as a toggle push to view the menu screens push again to exit BUTTON DESCRIPTION BUTTON DESCRIPTION Moves the highlight icon up to the function that user wants MENU Act...

Страница 15: ...n the unit will enable the operator to view any image from any of the connected screens on board the aircraft Simply connect the other units to the inputs labelled 1 through 4 on the quad box to initi...

Страница 16: ...around the KVM buttons Button operation from left to right will be to select KVM channels 1 through 4 respectively Top row of buttons will control the KVM video section The bottom row will control th...

Страница 17: ...default size and location Medium and Top Right Non volatile memory Opacity of the PIP image is set to 80 Mutually exclusive video modes With PIP active the Main and PIP windows display opposing video...

Страница 18: ...channel on the KVM switch and the configuration from the rear panel DIP switch Only affects the Main display PIP Off displays computer in the Main PIP On o If the computer input is in the Main window...

Страница 19: ...er source Long press of PIP If PIP mode is enabled then a long press of the PIP button swaps the PIP and Main images If PIP mode is not enabled then a long press of the PIP button will swap the last r...

Страница 20: ...Off switches the Main window to the selected video source 1 2 3 or 4 o With PIP On and video in the Main window switches the Main window to the selected video source 1 2 3 or 4 o With PIP On and video...

Страница 21: ...ow Quad display only contains video inputs Short press changes display to a QUAD video display o With PIP Off switches the Main window to QUAD video 1 2 3 4 o With PIP On and video in the Main window...

Страница 22: ...Document Number MAN FD215CV C 5 Rev B Revision Date 01 10 2017 Page 22 of 25 2017 FDS Avionics Corp All Rights Reserved TECHNICAL SUPPORT 470 239 7421 or FDSAvioncis com Technical Drawing...

Страница 23: ...s Corp products please contact our Product Support representatives at 470 239 7421 FDS Avionics Corp 6435 Shiloh Road Alpharetta GA 30005 Phone 470 239 7400 Fax 470 239 7439 Email sales FDSAvionics co...

Страница 24: ...ty high dust or power surges 6 Cosmetic damage or damage to internal components caused by installation or removal failure to follow installation or operating instructions or any neglect or misuse of t...

Страница 25: ...0 239 7421 or FDSAvioncis com Revisions Log Rev Date Page Description A 05 10 2013 All Initial Release B 06 10 2013 All Updates including pin out changes additional instruction on KVM Switch functiona...

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