Collins Aerospace AHC-1000A - Code produit: 822-1871-201, État de l'unité: Nouveau

FEATURES

• Attitude Heading Reference Systems (AHRS)
• AHS-1000() System is designed for Non-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
• Designed for both new aircraft and as replacement installations
• Provides synchro and analog heading, attitude, rate and acceleration information
• Automated compass swing
• AHS-1000A replaces analog systems that use 6-wire flux detectors, such as the DGS-65
• AHS-1000S replaces iron gyros that use 5-wire synchro flux detector interfaces
• Operates in Basic Mode and requires No Air Data inputs
• Compact Design - Reduced weight, size & power requirements
• Mounts without a traditional mounting tray - choice of installing with or without provided mounting flanges
• Easier installation through new auto-leveling feature
• Configurable outputs for interface flexibility
• Typical AHC-1000A systems include:
  • AHC-1000A Attitude Heading Computer,
  • FDU-3000* Flux Detector Unit, and
  • ECU-3000 External Compensation Unit
• In AHC-1000A System - FDU-3000 is not required for aircraft that already have FDU-70() installed
• Typical AHC-1000S systems include:
  • AHC-1000S Attitude Heading Computer,
  • 323A-2G Flux Detector Unit (& ARINC standard 3 wire), and
  • ECU-3000 External Compensation Unit