Specifications; Installation Instructions; Power - FDS FD171CV VER TS Installation And Operation Manual

Specifications

Display Type
Display Color
Pixel Pitch
Screen Resolution
Brightness
Dimensions
Display Size
Weight

Power

PC & Video Input
Video Type Supported
Screen Control
Remote Control
Materials
DO-160E Testing

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.
© 2017 FDS Avionics Corp.
All Rights Reserved.
Document Number:
MAN – FD171CV VER TS
Rev:
A
17.1 TFT Color LCD
16.7 Million Colors
0.291 mm x 0.291 mm
1280 x 768
450 cd/m
2
16.25 (W) x 11.00" (H) x 1086" (D)
14.65"(W) x 8.81" (H)
7.6 lbs.
28 VDC @ 1.5 AMPS
One High Density DB-15 Connector
VGA
On Screen Display Menu, Touch Screen
IR
Aluminum
In Progress
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com
Revision Date:
01/12/2017
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