FDS FD141CV-TS-HDSDI Installation And Operation Manual Download Page 8

 

Document Number: 

MAN 

– FD141CV-TS-HDSDI

 

Rev: 

Revision Date: 

01/12/2017 

Page 8 of 13 

 

 

©

 

2017 FDS Avionics Corp.  

All Rights Reserved. 

TECHNICAL SUPPORT 

470-239-7421 or FDSAvionics.com

 

 

Operation Instructions 

 

The FD141CV-TS-HDSDI is continuously on but can be de-energized by removing power 
from the entertainment system. No pilot or aircrew action is necessary during flight or 
ground operation. 

The passengers will be able to change the video output from the FD141CV-TS-HDSDI 
using the video source select button on the display. 

When applying 28V DC 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. 

Button Controls 

 

 

Located at the right of the FD141CV-TS-HDSDI are 8 buttons. Their functions are shown 
below as well as labelled on the left side of the monitor. 

 

 

BUTTON 

DESCRIPTION 

POWER  Toggles the power ON or OFF. Also, wakes the 

display up from SLEEP mode. 

MENU 

Opens the MENU. 

AUTO 

Auto-

adjusts the display’s size and position. 

DOWN 

Moves to the next selection in the menu. 

UP 

Moves to the previous selection in the menu. 

LEFT 

Decrease the selection’s value in the menu. 

RIGHT 

Increases the selection’s value in the menu. 

SOURCE  Switches between sources coming into the display*. 

*CMS will automatically control the monitor source 
switching when using the Cabin Control Modules. 

Summary of Contents for FD141CV-TS-HDSDI

Page 1: ...HDSDI Rev D Revision Date 01 12 2017 Page 1 of 13 2017 FDS Avionics Corp All Rights Reserved TECHNICAL SUPPORT 470 239 7421 or FDSAvionics com Installation and Operation Manual FD141CV TS HDSDI 14 1 H...

Page 2: ...com Table of Contents General Information 3 Front View 3 Rear View 3 Additional Information 4 Specifications 4 Installation Instructions 5 Power 5 Wiring Suggestions 5 Power Ground Wiring 6 Power Vide...

Page 3: ...en LCD The unit will allow installation in the smallest of mounting areas with the minimum of interface equipment This 14 display is intended to support applications where high brightness is a critica...

Page 4: ...has touchscreen capability using support programs with RS 232 The FD141CV TS HDSDI is made of all metal components Specifications Display Type WXGA LCD with LED Backlight Display Color 262 144 Colors...

Page 5: ...g locations are at the front corners of the unit Four 10 socket head screws not supplied are needed to secure the unit to the mounting surface It is strongly recommended that all four mounting locatio...

Page 6: ...lecting 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...

Page 7: ...cle Connector P N M24308 2 283 or Equivalent Crimp Contacts P N M39029 63 368 or Equivalent Pin Number Description 1 28VDC Power 2 28VDC Ground 3 Composite Video Signal 4 Composite Video Ground 5 N C...

Page 8: ...he last known source If no input is found the display will go to standby mode Pressing the Select button will select new video input Button Controls Located at the right of the FD141CV TS HDSDI are 8...

Page 9: ...Document Number MAN FD141CV TS HDSDI Rev D Revision Date 01 12 2017 Page 9 of 13 2017 FDS Avionics Corp All Rights Reserved TECHNICAL SUPPORT 470 239 7421 or FDSAvionics com Installation Drawing...

Page 10: ...Document Number MAN FD141CV TS HDSDI Rev D Revision Date 01 12 2017 Page 10 of 13 2017 FDS Avionics Corp All Rights Reserved TECHNICAL SUPPORT 470 239 7421 or FDSAvionics com Installation Drawing...

Page 11: ...s 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 co...

Page 12: ...dity 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...

Page 13: ...RT 470 239 7421 or FDSAvionics com Log of Revisions Rev Date Page Description A 06 18 10 Initial Release B 08 10 10 12 Updated Warranty info C 03 29 2011 4 5 Added a note to the General Information Up...

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