FDS FD102CV-C-4 User manual

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 1 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Installation and Operation Manual
FD102CV-C-4
10.2” HD Touchscreen LCD

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 2 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Table of Contents
General Information .........................................................................................................3
Front View ..........................................................................................................................3
Additional Information....................................................................................................3
Specifications .....................................................................................................................4
Installation Instructions...................................................................................................4
Power ...................................................................................................................................4
Wiring Instructions ...........................................................................................................5
Power/Video .......................................................................................................................6
HDSDI Input to Display..................................................................................................6
Operation Instructions .....................................................................................................7
Button Control....................................................................................................................7
Technical Drawing ............................................................................................................8
Technical Support .............................................................................................................9
Instructions for Continued Airworthiness...................................................................9
Warranty............................................................................................................................10
Log of Revisions ..............................................................................................................11

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 3 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
General Information
The FD102CV-C-4 is a special mission high resolution 10.2” High-Definition
touchscreen LCD. The LCD features a sunlight readable display that provides the
ability to bring VGA video or any other HD-SDI or SDI video source regardless of light.
This product is designed to work with either the FDCONV-HDSDI-S VER SW or
FDCONV-HDSDI-D VER SW. The converter units enable the FD102CV-C-4 the ability
to select HDSDI, Composite or VGA using the right side rocker switch on the front top
of the unit. This LCD also features NVG technology which can be switched to Day or
Night mode using the rocker switch located on the left side of the front panel.
Front View
Additional Information
The manuals for the interface boxes listed above can be found on the FDS Avionics
Corp. website.
The LCD is protected with a .060” Lexan lens to prevent scratching of the LCD.

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 4 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Specifications
Display Type
10.2” Widescreen TFT Color LCD
Pixel Pitch
0.072 mm X 0.220 mm
Screen Resolution
1024x600
Supported Resolution
Up to 1600x1200
Brightness
300 cd/ m²
Contrast
500 : 1
Display Dimension
9.80”(W) x 6.32” (H) x 1.23” (D)
Weight
2 lbs. 7oz
Power
28VDC @ 0.5 Amp
Operating Temperature
-20°C/60°C
Storage Temperature
-30°C/70°C
Screen Control
Touchscreen - On Screen Display
Menu
Materials
Aluminum
Aspect Ratio
16:9
Installation Instructions
All cabin entertainment equipment, such as the FD102CV-C-4, 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 entertainment system
should it become necessary.
It is recommended that you leave approximately ¼ inch of space above and below the
display to have circulating air.
Power
This is a 28V DC monitor that requires .5 Amps of power to operate. The unit turns on
automatically upon power application.

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 5 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
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
Strobe wiring
DC motor supply cables
Inverter cabling
Or any other potential noise source.

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 6 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Power/Video
Pin out for High Density HD-15 Receptacle (supplied)
Connector P/N: M24308/2-286 or Equivalent
Crimp Contacts P/N: M39029/57-354 or Equivalent
*These signals control the FDCONV-HDSDI-S VER SW or FDCONV-
HDSDI-D VER SW. Refer to product manual for interface drawings.
HDSDI Input to Display
Standard 75Ω BNC Plug (RG179 connector supplied)
Pin
Description
Center
Signal
Shell
Shield
Pin
Number
Description
1
28VDC Power
2
28VDC Ground
3
N/C
4
*Source Select (Converted/Loop Out) CH1
5
*CH1 Source Select VGA
6
N/C
7
N/C
8
N/C
9
N/C
10
N/C
11
N/C
12
N/C
13
RS-232 GND
14
RS-2332 TxD
15
RS-232 RxD

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 7 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Operation Instructions
The FD102CV-C-4 is continuously on but can be de-energized by removing power from
the entertainment system.
Monitor Control Buttons
Button
Function
Description
DAY/NVG
Night Vision
Switch
User can toggle back and forth between Night Vision or
Daylight
M
Menu
Activates the OSD menu or goes to previous menu. This
button acts as a toggle switch. Press once to open menu
options, press again to close.
Left
Decreases the adjustment of the selected function.
Right
Increases the adjustment of the selected function.
S
Source
Scroll through video sources. In the menu selects between
options and menu pages.
P
Power
Turns unit on and off
VGA/COMP/
SDI
Rocker
Switch
This rocker switch allows the user to select their choice of
viewing pleasure toggle through VGA, COMP and SDI

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 8 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Technical Drawing

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 9 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
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
Phone: [phone]
Fax: [phone]
Email: [email protected]
For further product information, technical data and sample wiring diagrams, please click
on the Dealers section of our web site at www.FDSAvionics.com
Instructions for Continued Airworthiness
The FD102CV-C-4 is designed not to require regular general maintenance.

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 10 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Limited Warranty
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 [phone].
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.

Document Number:
MAN –FD102CV-C-4
Rev:
B
Revision Date:
04/27/2017
Page 11 of 11
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Revisions Log
Rev
Date
Page
Description
A
03/07/2014
ALL
Initial Release
B
4/27/2017
All
Company name change and formatting. No revision change
necessary.