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Document Number: 

MAN 

– FD215CV-C-5

 

Rev: 

B

 

Revision Date: 

01/10/2017 

Page 14 of 25 

 

 

©

 

2017 FDS Avionics Corp.  

All Rights Reserved. 

TECHNICAL SUPPORT 

470-239-7421 or FDSAvioncis.com

 

 

 
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.  

 

 

 

 

BUTTON  DESCRIPTION 

BUTTON 

DESCRIPTION 

 

Moves the highlight icon up to 
the function that user wants. 

MENU 

Activates the OSD 
menu or goes to 
previous menu. 

 

Decreases the adjustment of 
the selected function. 

SCE 

Selects the Input 
Signal among HD-SDI, 
DVI, and VGA. 

 

Increases the adjustment of 
the selected function. 

AUTO 

Auto-adjustment in 
RGB. 

 

Moves the highlight icon 
down to the function that user 
wants. 

PWR 

Turns ON/OFF the 
system. 

 

 
 

MENU 

SCE 

AUTO 

PWR 

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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