Specifications; Installation Instructions - FDS FD141CV-C-6 Installation And Operation Manual

Specifications

Display Type
Display Color
Screen Resolution
Display Size
Weight
Power
Operating Temperature
Video Input (via TVS06RF-13-35P)
Video Type Supported
Screen Control
Materials
Certifications

Installation Instructions

All cabin equipment, such as the FD141CV-C-6, should be installed on a non-essential
bus and have a dedicated circuit breaker.
© 2017 FDS Avionics Corp.
All Rights Reserved.
Document Number:
MAN – FD141CV-C-6
14.1" TFT Color LCD
262K Colors
XGA 1024 x 768
14.7"(W) x 9.7"(H) x 1.7" (D)
6 lbs. 9 oz.
28V DC @ 2.0 Amps
0-50° C (32-122° F)
HDSDI, VGA, Composite Video
NTSC/PAL
On Screen Display Menu
Aluminum
Mil-STD 704 – Table IV for 28VDC
Altitude – MIL-STD-810F, Method 500.4, Procedure
II (Operation)
Low Temperature – MIL-STD-810F, Method 502.4,
Procedure II (Operation)
Humidity – MIL-STD-810F, Method 507.4, Procedure
II (Aggravated)
Vibration Performance – MIL-STD-810E, Method
514.4, Procedure I, Category 4
Shock – MIL-STD-810E, Method 516.4, Figure
516.4-4, Procedure I (Functional Shock)
Shock – MIL-STD-810E, Method 516.4, Figure
516.4-4, Procedure V (Crash Safety)
The
Explosive Atmosphere - RTCA-DO-160G, Sec 9.6.2
Cat E
Solar Radiation – MIL-STD-810F (N3) Method 505.4,
Procedure I, Cycle A1
High Temperature Operation – MIL-STD-810F (N3)
Method 501.4, Procedure II
Rapid Decompression – MIL-STD-810F (N3) Method
500.4, Procedure III,
Conducted Susceptibility MIL-STD-461F (N3)
Method 505.4, Procedure I, Cycle A1
Solar Radiation – MIL-STD-810F (N3) Method 505.4,
Procedure I, Cycle A1
Revision Date:
Rev:
04/27/2017
B
Page 4 of 34
TECHNICAL SUPPORT
470-239-7421 or FDSAvionics.com