FDS FD102CV-C-7-L User manual

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 1 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Installation and Operation Manual
FD102CV-C-7-L/R
10.2” LCD Monitor Left/Right Arm Mount

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 2 of 12
©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
Power and Ground Wiring......................................................................................................5
Power/Video...............................................................................................................................6
HDSDI Pinout ...........................................................................................................................7
Operation Instructions.............................................................................................................8
Button Control ...........................................................................................................................8
Technical Drawing....................................................................................................................9
Technical Support...................................................................................................................10
Instructions for Continued Airworthiness ........................................................................10
Warranty ...................................................................................................................................11
Log of Revisions......................................................................................................................12

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 3 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
General Information
The FD102CV-C-7-L/R is a special mission military monitor. It consists of two separate
parts, the LCD monitor and the articulating arm.
Built with retrofit aircraft integration in mind, this display can switch between two video
input sources using the buttons on the bezel. Additional functions are added using the 8
bezel keys. These functions are generated by the mission computer.
The arm has 2 pivot points which enable it to have a range of rotation up to 180° at each
pivot point. This monitor also tilt forward and AFT 20° in either direction and can rotate
45left and right.
The LCD features NVG technology which can be switched to Day or Night mode using
the rocker switch. The NVG LCD filters out infrared rays in the 1000nm range.
Front View
Additional Information
The FD102CV-C-7-L/R is made of all metal components. The milled aluminium arm
represents the evolution of several design enhancements for an optimum mounting
solution.

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 4 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Specifications
Display Type
10.2” TFT Color LCD
Display Color
262K color by 6 bi R.G.B Signal input
Screen Resolution
1024x600
Viewing Angle
140° Horizontal; 110° Vertical
Mount Dimensions (stowed)
11.10(W)x10.45(H)x2.95(D)
Mount Dimensions (deployed)
14.78”(W) x 10.45”(H) x 2.95”(D)
Display Dimensions
11.10”(W) x 6.75”(H)
Weight
4lbs. 5 oz.
Power
28V DC @ 1.0 Amp
Video Inputs Supported
2 - HDSDI
Video Types Supported
HDSDI
Screen Control
On Screen Display Menu
Mount Materials
Aluminum
DO-160 Testing
DO-160 Testing is completed on Parent
Products of a similar nature
Installation Instructions
All cabin entertainment equipment, such as the FD102CV-C-7-L/R, 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 monitor should it
become necessary.
Power
This is a 28VDC monitor that requires 1.0 Amps (28 Watts) of power.

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 5 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Power and Ground Wiring
This is a 28VDC monitor that requires 1 amp of power to operate. To operate properly this
monitor requires an input voltage of 18-29VDC.
The rated current of the equipment and associated voltage drop should be taken into
consideration when selecting 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 per 1000 feet, this equates to .81 Ohms for 50 feet. 1
Amp of current on .81 Ohms will drop .81 Volts.
Resistance of Wire Type M22759/16-**
(** = Gauge)
Gauge (AWG)
OHMS/1000’
24
26.20
22
16.20
20
9.88
16
4.81
12
2.02
10
1.26
8
.701
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.

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 6 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
J1 (Power/USB)
Connector P/N: M24308/2-287F
Contact, Socket P/N: M39029/57-354
J2 (HDSDI Input)
Pin
Number
Description
1
28VDC Power
2
28VDC Ground
3
N/C
4
N/C
5
N/C
6
N/C
7
N/C
8
N/C
9
N/C
10
N/C
11
N/C
12
N/C
13
N/C
14
N/C
15
N/C
16
N/C
17
N/C
18
N/C
19
N/C
20
N/C
21
N/C
22
USB Data + (Green)
23
USB Data –(White)
24
USB +5VDC (Red)
25
USB Ground (Black)
26
USB Shield

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 7 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
J3 (HDSDI Input)
Standard 75Ω BNC Receptacle (RG179 connector supplied)
Pin
Description
Center
Video Signal
Shell
Video Return

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 8 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Operation Instructions
The FD102CV-C-7-L/R is continuously on but can be de-energized by removing power
from the system. No pilot or aircrew action is necessary during flight or ground operation.
The operator will be able to change the video input from the FD102CV-C-7-L/R using the
rocker switch on the LCD monitor.
When applying 28VDC power, the display will turn on and look for a valid input on the
last known source. If video is not displayed when power is applied, then increase the
backlight brightness using the Right Arrow on the 5 button keyboard as the first step in
troubleshooting.
Button Controls
Located at the bottom of the FD102CV-C-7-L/R are five buttons.
Operations for both switches and buttons are as follows:
Day/NVG –Rocker switch turns night vision on and off
½ - Rocker switch allows user to switch from one HDSDI input connection to the other.
BUTTON
DESCRIPTION
M
Menu - Used to change the configuration of the picture
settings (Backlight, Brightness, Contrast, Saturation, Hue,
etc.)
Left Arrow –Adjusts Down
Right Arrow –Adjusts Up
Arrow Down –Scrolls Down
P
Power Button

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 9 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Technical Drawing

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 10 of 12
©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 [phone].
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-7-L/R is designed not to require regular general maintenance.

Document Number:
MAN –FD102CV-C-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 11 of 12
©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-7 (L/R)
Rev:
B
Revision Date:
05/05/2017
Page 12 of 12
©2017 FDS Avionics Corp.
All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Revisions Log
Rev
Date
Page
Description
A
02/21/2014
Initial Release
B
5/5/2017
All
New Format, New Company Name, new Warranty