EVENTIDE AIRBORNE MULTIPURPOSE ELECTRONIC DISPLAY (EAMED)

Specifications

The technology in EAMED has already revolutionized general aviation instrumentation: thousands of ARGUS Moving Map Displays already installed and flying are working proof. EAMED puts all the data processing power and versatility of the ARGUS computer and display into an "EOM" format. Instead of the standard ARGUS Moving Map program, EAMED is supplied with a general purpose operating system that allows programmers to create custom software. EAMED includes all the other capabilities of ARGUS 5000 - RS232C and RS422 interfaces, slaved compass and ADF capabilities, large onboard memory, CPU, power supply, video board and an amazingly crisp, bright CRT display. Because EAMED's circuitry is identical to the fully-TSO'd Eventide ARGUS 5000, its hardware meets the reequirements of RTCA/DO-160B. EAMED is furnished with comprehensive documentation that explains its hardware and software, including detailed descriptions of the operating system function calls.

Powerful Yet Compact Digital Avionics Development Platform

Self-contained 16 bit avionics computer
Includes CPU board, power supply, video board and CRT
High memory capacity
Comprehensive set of input/output peripheral connections
Displays both test and graphics on a high-resolution sunlight-readable screen
Versatile, low-overhead operating system software
Clear, comprehensive documentation
Entire unit fits in a standard panel cutout
Hardware meets DO160B specs

Ideal For A Wide Range Of Avionics Applications, Including:

Ground-to-air data link terminal
On-board communications
Data acquisition
Reconfigurable indicators
Interactive situation displays
Plus many more

EAMED TECHNICAL SPECIFICATIONS
  • WEIGHT: 4.05 lbs (with mounting tray
  • SIZE: 3:ATI x 10.50 (including knob)
  • POWER INPUT: 11 to 33 VDC @ 15 Watts nominal

    DATA COMPATIBILITY:

    Data Input Port A: EIA Standard RS-232C/RS-422
    Data Input Port A: EIA Standard RS-232C
    Data Input/Output Port B: EIA Standard RS-232C

    SLAVED COMPASS SYSTEM COMPATIBILITY: ARINC 407 Synchro

    ADF INSTRUMENTATION CAPABILITY:
    ARINC 407 Synchro, AC or DC Sine/Cosine
    A/D conversion inputs can also be used to measure input voltages at high speed
    ENVIRONMENTAL CATEGORIES (RTCA/DO-160B, environmental conditions and test procedures for airborne equipment [fixed and rotary wing, non-pressurized]):
    Temperature: -20C to +55C - F1
    Altitude: to 55,000 feet
    Temperature variation: C
    Humidity: A
    Vibration/Shock: P,A,S
    Magnetic effect: Z
    Power Input: B
    Voltage spike: A
    Audio frequency conduction/susceptibility: A
    Radio frequency susceptibility: A
    Radio frequency energy emission: A
    *all specifications subject to change without notice

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