Avionics Computer

© 2002 Unicontrols, a.s.

AIRCRAFT BOARD COMPUTER FOR AE270 CZECH REPUBLIC

Ae270 is low wing, single-engine turboprop, utility transport aircraft under development in IBIS Aerospace Ltd., Joint Venture Company established by Aero Vodochody and Aerospace Industrial Development Corporation, R.O.C., Taiwan


Prepared modifications with pressurized, retractable landing gear or non-pressurized, fixed landing gear for 2 crew + 8 passengers

 General Information

Relative Standards RTCA/DO-160C
RTCA/DO-178B
Category (RTCA/DO-160C) A1WCAMXXXXXXABABAUAA2Z3XX
Hardware based on VME products 3U
Real Time Operating System VRTX

Total Number of Signals

DI 72
DO 24
AI 24
COM 4x RS232

Functions and Control Loops

  • Air-conditioning - pressurization 
  • Air-conditioning - temperature 
  • Electrical power - indication 
  • Wing flaps 
  • Fuel delivery
  • Fuel quantity indicator
  • Pneumatic deicing system
  • Cabin windshield deicing
  • Propeller deicing
  • WCS (Warning and Caution System)
  • Pilot-computer communication 
  • Landing gear extending and retracting
  • Temperature, speed. altitude
  • Return drain pump controlling
  • Fuel flow indicator
  • Engine monitoring
  • Auto-diagnostic 

MULTIFUNCTIONAL DISPLAY FOR AE270

General Information

Relative Standards RTCA/DO-160C
RTCA/DO-178B
Category (RTCA/DO-160C) A1WCAMXXXXXXABABAUAA2Z3XX
Type of Display LED / Character 16 x 5 rows
Number of Buttons> 5
Communication Channel 2 x RS232

Up