FEATURES

• Attitude Heading Reference Systems (AHRS)
• AHS-3000() System is designed for ARINC 429 equipped aircraft
• Featuring digital quartz microelectromechanical systems (MEMS) sensors that provide heading and attitude information to the flight deck and other on board systems
• Solid-state sensor technology for high reliability
• Up to 10,000-hour mean time between failures rating
• Designed for both new aircraft and as replacement installations
• Analog and synchro interface for retrofit applications
• Primary function is to provide measurements of the aircraft pitch, roll and heading Euler angles for use by the flight deck displays, flight control systems and other avionics equipment
• High-quality body rate, Euler rate and linear acceleration outputs are provided for enhanced flight control system performance
• Advanced EMI/HIRF/Lightning isolation
• Built to withstand extreme environments involving high roll rates & vibration, designed for use in a variety of aircraft types
• Automated compass swing
• Uses existing five or six wire flux detector interfaces
• Compact Design – Reduced weight, size & power requirements
• Easier installation through new auto-leveling feature
• Configurable outputs for interface flexibility
• Typical AHC-3000A systems include:
  • AHC-3000A Attitude Heading Computer,
  • FDU-3000* Flux Detector Unit,
  • MMT-3010 Multi Modular Mount, and
  • ECU-3000 External Compensation Unit
  • *In AHC-3000A System – FDU-3000 is not required for aircraft that already have FDU-70() installed
• Typical AHC-3000S systems include:
  • AHC-3000S Attitude Heading Computer,
  • 323A-2G Flux Detector Unit (& ARINC standard 3 wire),
  • MMT-3010 Multi Modular Mount, and
  • ECU-3000 External Compensation Unit