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FD141CV-C-3

FDS FD141CV-C-3 Installation And Operation Manual

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Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Installation and Operation Manual
FD141CV-C-3
14” Widescreen HD Display
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 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 Suggestions ...............................................................................................................5
Power and Ground Wiring ...................................................................................................6
Power/Composite Pinout ......................................................................................................7
DVI Pinout ..............................................................................................................................8
VGA Pinout ............................................................................................................................9
HDSDI Inputs Pinout .........................................................................................................10
Rear View of Monitor with Connectors ..........................................................................10
Button Control ......................................................................................................................11
Technical Drawing......................................................................................................... 12-13
Technical Support ................................................................................................................14
Instructions for Continued Airworthiness .....................................................................14
Warranty ................................................................................................................................15
Revisions Log .......................................................................................................................16
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
General Information
The FD141CV-C-3 is a 14” High Definition LCD. This monitor includes four video source inputs: (1) HDSDI, (1) DVI Computer input, (1) VGA Computer Graphics input such as Moving Map CPU, and (1) Composite NTSC/PAL. In addition, there is (1) HDSDI Loop through Driver Output.
This monitor is designed to be mounted to a ruggedized articulating arm. The arm shown here can be used by both pilot and co-pilot by flipping over the base mount. These two units are sold separately.
Front View FD141CV-C-3
Additional Information
The LCD is protected with a .060” non-glare Lexan lens to prevent scratching of the LCD, and to meet stringent FAA abusive load criteria.
FDARM-ML-LG
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Specifications
Display Type
14.1” High Definition LCD
Display Color
6-bit, 262,144 Colors
Screen Resolution
1920 X 1080
Supported Resolution
1600 X 1200
Brightness
1000 cd/m2 (High Bright)
Dimensions
14.0”(W) x 9.05”(H) x 2.21”(D)
Weight
8 lbs. 4 oz.
Power
28V DC @ 1.5 Amps
Inrush Current
17A @ 2mS Peak In-Rush Current
1.4A @ 25mS Steady State Current
PC & Video Input
VGA, Composite, DVI, HDSDI & HDSDI Loop-through
Operating Temperatures
0-60°C (32-140°F)
Aspect Ratio
16:9
Materials
Aluminum
Installation Instructions
All cabin equipment, such as the FD141CV-C-3, should be installed on a non-essential bus and have a dedicated circuit breaker.
The FD141CV-C-3 is designed to mount onto a ruggedized articulating arm or into a standard electronics rack using (2) 10-32 Machine screws. See installation drawing on page 18 for measurement details.
When mounting onto the FDS Avionics Corp.’ FDARM-ML-LG, follow the installation instructions within that manual. The ruggedized industrial arm shown with this unit has the capability to configure viewing from either the pilot or the co-pilot. Instructions for making that quick adjustment are also found in the FDARM-ML-LG Manual.
Power
This is a 28VDC monitor that requires 1.5 Amps of power to operate. The unit turns on automatically upon power application. Wiring Suggestions
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 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 – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Power and Ground Wiring
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
This is a 28VDC monitor that requires 1.5 amps of power to operate. To operate properly this monitor requires an input voltage of 24-29VDC.
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.
1.5 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 to install the
product in compliance with industry standards and safety.
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Pin
Number
Description
1
15-28VDC Power
2
15-28VDC Ground
3
Composite Video Signal
4
Composite Video Return
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
N/C
23
N/C
24
N/C
25
N/C
Power/Composite
Standard Density DB-25 Receptacle – (supplied)
Connector P/N: M24308/2-283 or Equivalent
Crimp Contacts P/N: M39029/63-368 or Equivalent
Document Number:
MAN – FD141CV-C-3
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
DVI
Accepts a standard DVI-D (Single Link) male connector (not supplied)
Mating Face of Display Receptacle Shown
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
VGA
Pin
Number
Description
1
Red Video
2
Green Video
3
Blue Video
4
Ground
5
Ground (DDC Return)
6
Red Ground
7
Green Ground
8
Blue Ground
9
N/C
10
Sync Ground
11
Ground
12
DDC Data
13
Horizontal Sync
14
Vertical Sync
15
DDC Clock
High Density DB-15 Plug – (supplied)
Connector P/N: M24308/4-264 or Equivalent Crimp Contacts P/N: M39029/58-360 or Equivalent
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
HDSDI Inputs
Pin
Description
Center
Video Signal
Shell
Video Return
HDSDI Loop-through
Standard 75Ω BNC Plug (RG179 connectors supplied)
Rear View with Connectors
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Button Controls
BUTTON
DESCRIPTION
PWR
Turns ON/OFF the system.
MENU
Activates the OSD menu or goes to previous menu.
AUTO
Auto-adjustment in RGB.
Moves the highlight icon up to the function that user wants.
Moves the highlight icon down to the function that user wants.
Decreases the adjustment of the selected function.
Increases the adjustment of the selected function.
SCE*
Selects the Input Signal among VGA/DVI/Composite/SDI.
Located on the front-right side of the FD141CV-C-3 are 8 buttons. Their corresponding labels are located on the left side of the monitor. 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.
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Technical Drawing
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Technical Drawing
Document Number:
MAN – FD141CV-C-3
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 FD141CV-C-3 is designed not to require regular general maintenance.
Document Number:
MAN – FD141CV-C-3
Rev:
B
© 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 (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 – FD141CV-C-3
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Revisions Log
Rev
Date
Page
Description
A
02/14/2014
Initial Release
B
4/27/2017
All
Company name change, Warranty, and formatting.
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