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FD215CV-C-5

FDS FD215CV-C-5 Installation And Operation Manual

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Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Installation and Operation Manual
FD215CV-C-5
21.5” Widescreen HD Display
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.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
Rear Panel Connectors and Configurations..................................................................... 7-8
Power/Video ...............................................................................................................................8
Pin outs.................................................................................................................................. 9-12
Operation Instructions ...........................................................................................................12
Button Control .........................................................................................................................13
Quad Screen or Full Screen ............................................................................................. 14-20
Technical Drawing..................................................................................................................21
Technical Support ...................................................................................................................22
Instructions for Continued Airworthiness ........................................................................22
Warranty ...................................................................................................................................23
Revisions Log ...........................................................................................................................24
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
General Information
The FD215CV-C-5 is a special mission HD monitor which is designed to be mounted in a standard 19-inch rack.
Front View
Additional Information
The FD215CV-C-5 utilizes a state of the art digital video decoding chipset for all video inputs. Three video sources are activated: HD-SDI, DVI, and VGA (computer graphics i.e. moving maps).
The LCD is protected with a .060” non-glare Lexan lens to prevent scratching of the LCD, and to meet stringent FAA abrasive load criteria.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Specifications
Display Type
21.5” TFT Color LCD
Display Color
16.7 Million Colors
Screen Resolution
1920 X 1080
Screen Control
On Screen Display Menu
Brightness
300 cd/m2
Dimensions
20.0”(W) x 14.5”(H) x 2.78”(D)
Display Size
18.82”(W) x 10.61”(H)
Weight
10 lbs 13 oz
Power
28V DC @ 3 Amps
PC & Video Input
Analog RGB/VGA, HD-SDI, Digital (DVI-D)
Video Type Supported
NTSC/PAL
Viewing Angle
170° Horizontally 160° Vertically
Materials
Aluminum
Inrush Current
17A (max current) 3A – 20µs
Installation Instructions
All cabin equipment, such as the FD215CV-C-5, should be installed on a non-essential bus and have a dedicated circuit breaker.
The FD215CV-C-5 is designed to mount into a standard electronics rack using (4) 10-32 Machine screws. See installation drawing on page 23 for measurement details.
Power
This is a 28VDC monitor that requires 3.0 Amps of power to operate. The unit turns on automatically upon power application.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Wiring Suggestions
Shields used on wire bundles and power should be grounded to the connector at the source and left floating at the display. Shields for USB, SDI data, and video should be connected at both ends.
Avoid routing video wiring parallel to:
AC wiring Strobe wiring DC motor supply cables Inverter cabling Or any other potential noise source.
We recommend coax cables be terminated using solder sleeve coaxial cable terminators such as Raychem Part Number CWT-4174-W122-5/9.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.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
.70
Power and Ground Wiring
This is a 28VDC monitor that requires 3 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. 3 Amps of current on .81 Ohms will drop 2.43 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 – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Rear Panel Connectors and Configurations
A small cover plate can be removed on the rear panel to access an 8 position configuration switch. The switch is labeled 1 through 8. Switch 1 is toward the center of the monitor, Switch 8 is toward the outside edge of the monitor.
Switches 1 through 4 configure the monitor to support either VGA or DVI for each KVM video input. Switch number 1 corresponds to KVM switch input #1. Switch number 2 corresponds to KVM switch input #2. Switch number 3 corresponds to KVM switch input #3. Switch number 4 corresponds to KVM switch input #4. Set switch in “down” position for VGA input. Set switch in “up” position for DVI input.
Switch #5 configures the monitor to support either the Raritan Switchman KVM switch or the Adderview Pro KVM Switch. Set switch in “down” position for use with the Raritan Switchman KVM switch. Set switch in “up” position for use with the Adderview Pro KVM Switch.
Switches #6 and #7 set the mode for the USB Enumeration. #6 UP, #7 UP Keyboard Emulator. For use with KVM switch control. #6 UP, #7 Down Joystick/Game controller emulator #6 Down, #7 UP Virtual COM port (for configuration) #6 Down, #7 Down Not yet defined
Switch #8 is for RS-485 slave/master mode. In the Master mode the Monitor controller PCB assembly mounted internal to the monitor takes command of the Quad video processor and the Scaler PCBs inside the monitor. Slave mode permits an external device to take control of the two internal subsystems. Set “Down” or “off” to put controller in Slave mode. Set the switch “up” ” to put
controller in Master mode.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Pin
Number
Description
A
18-33 VDC Power
B
18-33 VDC Power
C
18-33 VDC Ground
D
18-33 VDC Ground
E
N/C
Power/Video
Power – D38999 connector (supplied)
Crimp Contacts P/N: M39029/56-351 or Equivalent
Connector P/N: D38999/26FB5SA or Equivalent
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Pin
Number
Description
1
Red Video
2
Green Video
3
Blue Video
4
GND
5
DDC Return (Optional)
6
Red Return
7
Green Return
8
Blue Return
9
NC
10
Sync Ground
11
GND
12
DDC Data (Optional)
13
Horizontal Sync
14
Vertical Sync
15
DDC Clock (Optional)
VGA Video (Accepts Industry Standard VGA connection HD15 plug, supplied)
Connector P/N: M24308/4-260 or Equivalent Crimp Contacts P/N: M39029/58-360 or Equivalent
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Pin
Number
Description
1
USB VBUS (Red)
2
USB D- (Green)
3
USB D+ (White)
4
USB Ground (Black)
5
Switch Input
6
RS-485A Quad
7
RS-485B Quad
8
RS-485A Scaler
9
RS-485B Scaler
DB9 Power/Control Connector:
Suggested source of supply for DB9 connectors, manufactured by Tyco/Amp: Connector P/N M24308/2-281 Crimp Contacts P/N M39029/63-368 Wire 20 gauge wire is recommended
DB9 Pinout & Female Mating Face Profile
Note. The USB interface board is set to USB1.0 mode in order to permit maximum flexibility in the choice of components used for the cable and connectors that are used between the monitor and the USB host or KVM switch. USB specifies maximum cable length for USB 1.0 and 2.1 devices as 16 feet, 5 inches. This maximum length can be used if 100 Ohm low capacitance shielded twisted pair cable is used. Reduce length if the cable does not fully meet the USB specifications for best results.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.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
HDSDI Inputs & Loop-Through Driver Output (Standard 75Ω BNC Plug, RG179 connector supplied)
DVI-D (Accepts a standard DVI-D (Single Link) male connector (supplied)
View into mounted receptacle
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
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
Operation Instructions
The FD215CV-C-5 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-5 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 Select button will select new video input.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
BUTTON
DESCRIPTION
BUTTON
DESCRIPTION
Moves the highlight icon up to the function that user wants.
MENU
Activates the OSD menu or goes to previous menu.
Decreases the adjustment of the selected function.
SCE
Selects the Input Signal among HD-SDI, DVI, and VGA.
Increases the adjustment of the selected function.
AUTO
Auto-adjustment in RGB.
Moves the highlight icon down to the function that user wants.
PWR
Turns ON/OFF the system.
MENU
SCE
AUTO
PWR
Button Controls
Located on the front right of the FD215CV-C-5 are two sets of 4 buttons. 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 – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
4 3 2 1
1 2 3 4
Q U A D
S W A P
C O M P
Quad Screen or Full Screen
This display has the capability to display a quad screen or full screen from any of the four HDSDI inputs. The image seen here is the bottom view of the FD215CV-C-5 Widescreen HD Monitor. Connecting the SDI input to the output of the attached quad box on the unit will enable the operator to view any image from any of the connected screens on board the aircraft. Simply connect the other units to the inputs labelled 1 through 4 on the quad box to initiate the connection.
The button display below is centrally located on the bottom of the bezel display of the unit. The number keys will allow you to look at that connection display or the user can use PIP (Picture in Picture) to set their own preference. The QUAD button will display all connected HDSDI inputs at once. The SWAP Button will enable the user to move around through the multiple HSDSI connections.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
User Interface and Front panel:
The 8 button group on the left side of the monitor control the KVM switch. The 7 button group in the center control the video selection. The 7 button group on the right side control the Scaler board On Screen Display menu.
The Monitor control system keeps up with the last KVM request to determine if the request for the “computer” channel will be VGA or DVI.
Operation of the KVM switch group:
There will be no nomenclature around the KVM buttons. Button operation from left to right will be to select KVM channels 1 through 4 respectively. Top row of buttons will control the KVM video section. The bottom row will control the KVM USB section.
Power up States:
Monitor will set internal and external subsystems upon initial application of power.
1) KVM video and USB will be set to channel 1.
2) The video channel (DVI or VGA) associated with KVM channel 1 by the rear panel dip switch will be displayed
in the Main screen area.
3) A Quad view of the four SDI inputs displayed in the PIP area.
4) The video channel (DVI or VGA) associated with KVM channel 1 by the rear panel dip switch is stored in
Volatile memory as the last requested computer source.
5) The Quad view of the four SDI inputs is stored in Volatile memory as the last requested video source.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Operation of the Video selection Switch group:
The slide-out monitor has two window fields: Main and Picture-in-Picture (PIP).
Power-on Default: Computer is displayed in the Main window and quad video is displayed in the PIP window (non-volatile memory).
Picture-in-Picture (PIP) default size and location = Medium and Top Right (Non-volatile memory) Opacity of the PIP image is set to 80%.
Mutually exclusive video modes:
With PIP active, the Main and PIP windows display opposing video (1, 2, 3, 4, or QUAD) and computer (COMP) inputs.
or
Cannot have the computer source displayed within both the Main and the PIP windows at same time. Cannot have a video source (1, 2, 3, 4 or QUAD) displayed within both the Main and the PIP windows at
same time.
Overall Button Operation:
Video Select buttons accept Long press and Short press commands. Long Press (LP) button function: press and hold for > ¾ second. Activation is at time-out (release not required).
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
COMP Button:
COMP (Computer): Short press – changes the Main display to the computer input; either the VGA or DVI input full screen. The VGA or DVI selection will be made by the last requested video channel on the KVM switch and the configuration from the rear panel DIP switch. . Only affects the Main display
PIP Off: displays computer in the Main
PIP On:
o If the computer input is in the Main window: no change. Video PIP remains. o If the computer input is in the PIP window: functions like a LP PIP, moving the computer display
to the Main window and the video display to the PIP window
Long Press (LP) of COMP moves that computer input to Main and turns PIP Off
o Returning to PIP with COMP in the Main window, displays the last used video input in the PIP
window
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
PIP Button:
Short press of PIP enables and disables the PIP display. If PIP is disabled, then a short press enables it. If it is enabled, then a short press disables it.
When enabling PIP, if the computer is displayed in the main screen area, then the PIP area contains the last requested Quad, 1, 2, 3, or 4 video source.
If any video source is displayed in the main screen area, then the PIP area contains the computer source.
Long press of PIP:
If PIP mode is enabled then a long press of the PIP button swaps the PIP and Main images. If PIP mode is not enabled, then a long press of the PIP button will swap the last requested computer source and the last requested video source. If computer is currently displayed, then a long press of the PIP button will put the last requested video channel (SDI 1, SDI2, SDI3, SDI4, or Quad view of all four SDI sources) into the full screen view on the monitor. If any of the video modes are currently displayed, then a long press of the PIP button will put the last requested computer channel into the full screen view on the monitor.
o With PIP On: Swaps sources between Main window and PIP window
o With PIP Off: Swaps sources (computer or video) on the Main window
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Buttons: 1, 2, 3, 4:
Short press - Changes the display to the selected Video source as follows:
o With PIP Off: switches the Main window to the selected video source (1, 2, 3, or 4)
o With PIP On and video in the Main window: switches the Main window to the selected video
source (1, 2, 3, or 4)
o With PIP On and video in the PIP window: switches the PIP window to the selected video source
(1, 2, 3, or 4)
Long Press (LP) moves that video source to the Main window and turns PIP Off
o Returning to PIP with the selected video source (1, 2, 3, or 4) in the Main window, displays
COMP in the PIP window
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Quad Button:
QUAD (Quad video): Displays all four video sources (1, 2, 3, & 4) in the affected window. Quad display only contains video inputs.
Short press – changes display to a QUAD video display
o With PIP Off: switches the Main window to QUAD video (1, 2, 3, & 4)
o With PIP On and video in the Main window: switches the Main window to QUAD video
o With PIP On and video in the PIP window: switches the PIP window to QUAD video
Long Press moves QUAD video input to Main and turns PIP Off
o Returning to PIP with QUAD in the Main window, displays COMP in the PIP window
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Technical Drawing
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.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-5 is designed not to require regular general maintenance.
Document Number:
MAN – FD215CV-C-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.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-5
Rev:
B
© 2017 FDS Avionics Corp. All Rights Reserved.
TECHNICAL SUPPORT
470-239-7421 or FDSAvioncis.com
Revisions Log
Rev
Date
Page
Description
A
05/10/2013
All
Initial Release
B
06/10/2013
All
Updates including pin out changes; additional instruction on KVM Switch functionality; user friendly explanation added for PIP/Quad Functions
B
1/10/2017
All
Company name change and formatting – No revision change necessary.
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