FDS FD171CV VER HDSDI User manual

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 1 of 15

TECHNICAL SUPPORT

470-239-7421 or FDSAvionics.com

Installation and Operation Manual

FD171CV VER TS

17.1” Widescreen Touchscreen LCD

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 2 of 15

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

S-Video/Composite and Audio Wiring ................................................................................5

VGA Wiring ...............................................................................................................................6

Power and Ground Wiring......................................................................................................7

Power/Video...............................................................................................................................8

Operations Instructions ...........................................................................................................9

Button Controls .........................................................................................................................9

Remote Control........................................................................................................................10

Technical Drawing #1 ............................................................................................................11

Technical Drawing #2 ............................................................................................................12

Technical Support...................................................................................................................13

Instructions for Continued Airworthiness ........................................................................13

Warranty ...................................................................................................................................14

Log of Revisions......................................................................................................................15

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 3 of 15

TECHNICAL SUPPORT

470-239-7421 or FDSAvionics.com

General Information

The FD171CV VER TS is a 17.1” Widescreen Touchscreen LCD which has features that

allow installation in the smallest of mounting areas with the minimum of interface

equipment. The FD171 VER TS has a capacitive touchscreen that uses RS-232 to

interface with the equipment it controls.

Front View

Additional Information

The FD171CV VER TS utilizes a state of the art digital video decoding chipset for the

analog VGA video input.

The FD171CV VER TS can also be connected to existing video switchers and receive

video inputs from a selector interface box.

The FD171CV VER TS is made of all metal components.

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 4 of 15

TECHNICAL SUPPORT

470-239-7421 or FDSAvionics.com

Specifications

Display Type

17.1 TFT Color LCD

Display Color

16.7 Million Colors

Pixel Pitch

0.291 mm x 0.291 mm

Screen Resolution

1280 x 768

Brightness

450 cd/m2

Dimensions

16.25 (W) x 11.00” (H) x 1086” (D)

Display Size

14.65”(W) x 8.81” (H)

Weight

7.6 lbs.

Power

28 VDC @ 1.5 AMPS

PC & Video Input

One High Density DB-15 Connector

Video Type Supported

VGA

Screen Control

On Screen Display Menu, Touch Screen

Remote Control

Materials

Aluminum

DO-160E Testing

In Progress

Installation Instructions

All non-flight essential equipment, such as the FD171CV VER TS, 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 display should it become

necessary.

There are eight 8-32 UNC mounting holes located on the sides and back of the display.

Four holes are located at the four corners of the back and four holes are located two on

each side of the bezel. It is sufficient to mount the display by four attach points.

Mounting against the bulkhead or on a bracket: The unit can be mounted internal,

external, or partially internal to the bulkhead. It is recommended that at least a ¼ inch of

space around the rear, top and bottom of the display for the internal exhaust fan to be

able to circulate air through the unit. When mounting from inside the bulkhead it is

possible to have only the LCD visible to the cabin. The unit will come on automatically

upon power application.

Power

This is a 28VDC monitor that requires 1.5 AMPS of power to operate.

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 5 of 15

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.

S-Video/Composite and Audio Wiring

Recommended cable for s-video/composite and audio purposes is PIC 75 Ohm Coax,

P/N V76261. This is a lightweight, flexible, and low signal loss cable which meets FAA

flammability requirements of FAR 23.1359(d), FAR 25.853(a) and FAR 25.869(a)(4).

Similar aviation coaxial cable can be used from other vendors, as well. Some aircraft are

prone to AC noise - we recommend adding to the composite source a 75Ohm video

isolation transformer such as Deerfield Laboratory, Inc. Part No. 162-1

(www.deerfieldlab.com, (650) 632-4090). In most cases this should be added to the video

output of the source.

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 6 of 15

TECHNICAL SUPPORT

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VGA Wiring

Recommended cable for VGA purpose is ECS P/N 453005. This is a single shielded

cable containing 5 separate coaxial cables, color-coded to match the functions of the

wires.

Coax cables should be terminated using solder sleeve coaxial cable terminators,

Raychem P/N: CWT-4174-W122-5/9

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 7 of 15

TECHNICAL SUPPORT

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Power and Ground Wiring

This is a 28VDC monitor that requires 1.5 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. 1.5 Amps of current on .81 Ohms will drop 1.22 Volts.

Resistance of Wire Type M22759/16-**

(** = Gauge)

Gauge (AWG)

OHMS/1000’

26.20

16.20

9.88

4.81

2.02

1.26

.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 –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 8 of 15

TECHNICAL SUPPORT

470-239-7421 or FDSAvionics.com

Power/Video

Pin out for P1 (High Density DB-15 Receptacle)

Connector P/N: M24308/2-286 or Equivalent

Crimp Contacts P/N: M39029/57-354 or Equivalent

Number

Description

28V DC Power

28V DC Ground

5V DC Power (Touch Screen)

5V DC Ground (Touch Screen)

GND

Blue Ground (Pin 8 on Standard VGA)

Red Video (Pin 1 on Standard VGA)

Green Video (Pin 2 on Standard VGA)

Blue Video (Pin 3 on Standard VGA)

Red Ground (Pin 6 on Standard VGA)

Green Ground (Pin 7 on Standard VGA)

Horizontal Sync (Pin 13 on Standard

VGA)

Vertical Sync (Pin 14 on Standard VGA)

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 9 of 15

TECHNICAL SUPPORT

470-239-7421 or FDSAvionics.com

Operation Instructions

The FD171CV VER TS is continuously on but can be de-energized by removing power

from the unit at the circuit breaker panel or by cycling the power on/off bezel button on

the top of the display. No pilot or aircrew action is necessary during flight or ground

operation.

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.

Button Controls

There are 5 buttons located on the top center. Their functions are shown below:

BUTTON

DESCRIPTION

POWER

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

up from SLEEP mode.

Opens the MENU.

DOWN

Moves to the next selection in the menu.

Moves to the previous selection in the menu.

SOURCE

Switches between sources coming into the display.

Document Number:

MAN –FD171CV VER TS

Rev:

Revision Date:

01/12/2017

Page 10 of 15

TECHNICAL SUPPORT

470-239-7421 or FDSAvionics.com

Remote Control

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