FDS FD102CV-C-1 User manual

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 1 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Installation and Operation Manual
FD102CV-C-1
10.2” Widescreen LCD

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 2 of 13
©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...........................................................................................................................................5
Wiring Suggestions ..................................................................................................................5
S-Video/Composite...................................................................................................................5
VGA Wiring ...............................................................................................................................6
Power/Video...............................................................................................................................7
Operation Instructions.............................................................................................................8
Monitor Control Buttons .........................................................................................................8
Remote Control Buttons ..........................................................................................................9
Technical Drawing..................................................................................................................10
Technical Support...................................................................................................................11
Instructions for Continued Airworthiness ........................................................................11
Warranty ...................................................................................................................................12
Log of Revisions......................................................................................................................13

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 3 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
General Information
The FD102CV-C-1 is a special mission high resolution 10.2” widescreen LCD. The LCD
features NVG technology which can be switched to Day or Night mode using the rocker
switch. The FD102CV-C-1 will support composite video, s-video, VGA and DVI-D single
link.
Front View
Additional Information
The FD102CV-C-1 can be connected to existing video switchers and can take a
composite video input from a selector interface box. Multiple input sources can be
selected and displayed on the monitor.
The FD102CV-C-1 is made of all metal components. DO-160 testing has been
completed and is available upon request.
The LCD is protected with a .060” Lexan lens to prevent scratching of the LCD.

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 4 of 13
©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
9.8”(W) x 6.32” (H) x 1.23” (D)
Display Size
8.70”(W) x 5.215” (H)
Weight
2 lbs. 7oz
Power
28VDC @ 0.5 Amp
Operating Temperature
-20°C/60°C
Storage Temperature
-30°C/70°C
PC & Video Input
VGA (Analog RGB 15 pin D-sub)
Composite Video, S-Video, DVI-D
Single Link
Video Type Supported
NTSC/PAL
Screen Control
On Screen Display Menu
Remote Control
IR, included
Materials
Aluminum
Aspect Ratio
16:9
Installation Instructions
All cabin entertainment equipment, such as the FD102CV-C-1, 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.

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 5 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Power
This is a 28V DC monitor that requires .5 Amps of power to operate. The unit turns on
automatically upon power application.
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.
S-Video/Composite and Audio Wiring
Recommended cable for s-video/composite and audio purposes is PIC 75 Ohm Coax,
P/N V76261. This is a lightweight, flexible, and low signal loss cable which meets FAA
flammability requirements of FAR 23.1359(d), FAR 25.853(a) and FAR 25.869(a)(4).
Similar aviation coaxial cable can be used from other vendors, as well.
Some aircraft are prone to AC noise –we recommend adding to the composite source a
75Ohm video isolation transformer such as Deerfield Laboratory, Inc. Part No. 162-1
(www.deerfieldlab.com, [phone]). In most cases this should be added to the video
output of the source.

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 6 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
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.
Coax cables should be terminated using solder sleeve coaxial cable terminators,
Raychem P/N: CWT-4174-W122-5/9

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 7 of 13
©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
Pin
Number
Description
1
28VDC Power
2
28VDC Ground
3
Composite Video 1 –Signal
4
Composite Video 1 –Shield
5
S-Video Y - Signal
6
S-Video Y - Shield
7
S-Video C - Signal
8
S-Video C - Shield
9
Red Video (Pin 1 on Standard VGA)
10
Green Video (Pin 2 on Standard VGA)
11
Blue Video (Pin 3 on Standard VGA)
12
Red Ground (Pin 6 on Standard VGA)
13
Green Ground (Pin 7 on Standard VGA)
14
Horizontal Sync (Pin 13 on Standard VGA)
15
Vertical Sync (Pin 14 on Standard VGA)

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 8 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Operation Instructions
The FD102CV-C-1 is continuously on but can be de-energized by removing power from
the entertainment system.
Monitor Control Buttons
Button
Function
Description

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 9 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Remote Control Buttons
The remote control included with the FD102CV-C-1 contains the same functionality
available on the display buttons, to include power, source, menu, and directional arrows.

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 10 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Technical Drawing

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 11 of 13
©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-1 is designed not to require regular general maintenance.

Document Number:
MAN –FD102CV-C-1
Rev:
B
Revision Date:
04/27/2017
Page 12 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.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 [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-1
Rev:
B
Revision Date:
04/27/2017
Page 13 of 13
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Log of Revisions
Rev
Date
Page
Description
A
06/29/2012
---
Initial Release
B
4/27/2017
All
Company name change, Warranty, and format.