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FD215CV-C-TS-1

FDS FD215CV-C-TS, FD215CV-C-TS-1 Installation And Operation Manual

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Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Installation and Operation Manual
FD215CV-C-TS FD215CV-C-TS-1
21.5” LCD Touchscreen Display
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Specifications
FD215CV-C-TS
FD215CV-C-TS-1
Display Panel Technology
21.5” TFT Color LCD
21.5” TFT Color LCD
Color
16.7 Million Colors
16.7 Million Colors
Native Resolution Refresh Rate
1920 x 1080
1920 x 1080
Touchscreen
Capacitive Touchscreen Glass
Capacitive Touchscreen Glass
Touchscreen Control
USB
RS-232
Brightness
300 cd/m²
300 cd/m²
Aspect Ratio
19:9
19:9
Viewing Angle
170º Horizontally 160º Vertically
170º Horizontally 160º Vertically
Power Power
28V DC @ 3 Amps
28V DC @ 2 Amps
Inrush Current
18.0 Amps @2.0 µS
4.0 Amps @ 2mS
2.0 Amp Steady State @ 3.5mS
18.0 Amps @2.0 µS
4.0 Amps @ 2mS
2.0 Amp Steady State @ 3.5mS
Environmental Conditions
Operating Temperatures
5º - 45º C
5º - 45º C
Dimensions
External
20.0”(W) x 13.25”(H) x 1.76” (D)
20.0”(W) x 13.25”(H) x 1.76” (D)
Active Display Area
18.64”(W) x 10.43” (H)
18.64”(W) x 10.43” (H)
Weight
10 lbs. 13 oz.
10 lbs. 13 oz.
Materials
Aluminum
Aluminum
Features
Menu Control
On Screen Display Menu
On Screen Display Menu
Qualified Testing
RTCA DO-160
160G Sec 21 Cat B – Emissions
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Connectivity
* NTSC or PAL
** Touchscreen Controller
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Table of Contents
General Information ...................................................................................................... 5
Front View ...................................................................................................................... 5
Additional Information .................................................................................................. 5
Installation Instructions ................................................................................................ 6
Power and Ground Wiring ............................................................................................ 6
VGA Wiring .................................................................................................................... 6
Pinouts ...................................................................................................................... 7-10
Operation Instructions ................................................................................................ 11
Button Control ............................................................................................................. 11
Touchscreen Driver .................................................................................................... 12
Technical Drawing ...................................................................................................... 13
Technical Support ....................................................................................................... 14
Instructions for Continued Airworthiness ................................................................ 14
Warranty ...................................................................................................................... 15
Log of Revisions ......................................................................................................... 16
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
General Information
The FD215CV-C-TS(-1) is a touchscreen enabled, special mission, high resolution, panel mounted 21.5” widescreen LCD.
Front View
Additional Information
The LCD features include:
Five video source inputs are available to include:
1. HD-SDI (for HD camera inputs)
2. DVI
3. VGA (for computer graphics, i.e.; moving maps)
4. S-Video (via BNC connectors for Y and C components)
5. Composite
Dual USB 2.0 powered ports are provided for connection to mission computers for
quick and easy access to files via thumb drive. Each port also supplies up to 500mA to power external devices.
Bezel buttons on front of display for operational convenience of OSD.
HD-SDI loop through for output to a HD-DVR or other displays.
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
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
Installation Instructions
Use (6) 8-32 Machine screws. See the technical drawing on page 13 for mounting locations and details.
All cabin equipment, such as the FD215CV-C-TS(-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 system should it become necessary.
Power and Ground Wiring
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, 1.5 amp equipment load 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. 1.5 Amp of current on .81 Ohms will drop 1.22 Volts.
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 in order to install the
product in compliance with industry standards and safety.
VGA Wiring
The FD215CV-C-TS(-1) uses standard VGA cables for input.
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Pin
Number
Description
A
28VDC Power
B
28VDC Power
C
28VDC Ground
D
28VDC Ground
E
N/C
Pinouts for FD215CV-C-TS (-1) Pinout for 28V PWR– D38999 connector (supplied)
Mating Connector P/N: D38999/26FB5SA or Equivalent
Crimp Contacts P/N: M39029/56-351 or Equivalent
MATING FACE
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Pin
Description
FD215CV-C-TS
FD215CV-C-TS-1
1
+5V POWER (FROM USB SOURCE)
N/C
2
DATA (DN) DIFFERENTIAL PAIR
RS-232 TX (Connect to Pin 2 on STD DB9
COM Port)
3
DATA (DP) DIFFERENTIAL PAIR
RS-232 RX (Connect to Pin 3 on STD DB9
COM Port)
4
POWER RETURN
N/C
5
CHASSIS GROUND
RS-232 GND (Connect to Pin 5 on STD DB9
COM Port)
6
N/C
N/C
7
N/C
N/C
8
N/C
N/C
9
N/C
N/C
Pinout for Touchscreen Control (DB-9F)
Connector P/N: M24308/2-281 or Equivalent
Crimp Contacts P/N: M39029/63-368 or Equivalent
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Pin
Description
Center
Video Signal
Shell
Video Return
Pin
Description
Center
Video Signal
Shell
Video Return
Pin
Description
Center
Y Signal
Shell
Y Return
Pin
Description
Center
C Signal
Shell
C Return
Pin
Description
Center
Video Signal
Shell
Video Return
Pin out for HD-SDI Input
(Standard BNC – 75 OHM) - Supplied
Pin out for HD-SDI Output
(Standard BNC – 75 OHM) - Supplied
Pin out for S-Video (Luminance - Y Component)
(Standard BNC – 75 OHM) - Supplied
Pin out for S-Video (Chrominance - C Component)
(Standard BNC – 75 OHM) - Supplied
Pin out for Composite Video
(Standard BNC – 75 OHM) - Supplied
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Pin
Number
Description
1
TMDS data 2-
2
TMDS data 2+
3
TMDS data 2 shield
4
N/C
5
N/C
6
DDC clock
7
DDC data
8
N/C
9
TMDS data 1-
10
TMDS data 1+
11
TMDS data 1 shield
12
N/C
13
N/C
14
+5 V
15
Ground
16
Hot plug detect
17
TMDS data 0-
18
TMDS data 0+
19
TMDS data 0 shield
20
N/C
21
N/C
22
TMDS clock shield
23
TMDS clock+
24
TMDS clock-
C1
N/C
C2
N/C
C3
N/C
C4
N/C
C5
N/C
Pin out for DVI-D
Accepts a standard DVI-D (Single Link) male connector (supplied)
View into mounted receptacle
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
BUTTON
DESCRIPTION
PWR
Turns ON/OFF the system.
MENU
Activates the OSD menu for the monitor settings or goes to previous menu.
AUTO
Auto-adjustment in RGB.
Moves the highlight icon down through menu options.
Moves the highlight icon up through menu options.
Decreases the adjustment of the selected function.
Increases the adjustment of the selected function.
SCE
Cycles through available input sources.
Operation Instructions
The FD215CV-C-TS(-1) 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 the video output from the FD215CV-C-TS(-1) using the video source select button on the display.
When applying 28VDC power, the display will turn on and look for a valid input on the last known source. If no input is found, the display will go to standby mode. Pressing the Source button will rotate through available video inputs.
Button Controls
Located on the front of the FD215CV-C-TS(-1) are 8 buttons:
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Touchscreen Driver
The FD215CV-C-TS and FD215CV-C-TS-1 utilize a touchscreen controller manufactured by 3M. The touchscreen driver is supplied by 3M and FDS Avionics Corp. recommends downloading the latest version of the driver during the installation of the FD215CV-C-TS/-1, at the following address:
http://solutions.3m.com/wps/portal/3M/en_US/Electronics_NA/Electronics/Tools_Suppo rt/Support/
Follow the web address above and select the operating system depending on the platform that will be connected to the FD215CV-C-TS (-1). Any of the MT7 drivers should work for either the FD215CV-C-TS or FD215CV-C-TS-1 as long as the correct operating system was selected.
Make sure to follow the installation instructions and plug in the touchscreen controller when asked by the installation software. The FD215CV-C-TS-1 driver installation may require a reboot of the system platform after installation for the RS-232 monitoring service to start.
The MT7 Software Users Guide can also be found at the same location as the driver download. This document has detailed instructions on how to use and setup the MT7 touch screen software. Topics include: Calibration, Linearization, Changing the Touch Down/Touch Up events, changing the audible beep and multi-display configuration.
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Technical Drawing
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 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: 470-239-7400 Fax: 470-239-7439 Email: sales@FDSAvionics.com
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 FD215CV-C-TS(1) is designed not to require regular general maintenance.
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 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 (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.
Document Number:
MAN – FD215CV-C-TS (-1)
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Rev
Date
Page
Description
A
12/06/2012
All
Initial Release
B
10/06/2015
All
Added provision for FD215CV-C-TS-1 RS232 Version. Updated Format, Warranty, Specifications
B
1/10/2017
All
Changed Company Name and Formatting – No Revision Change Necessary.
Log of Revisions
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