Avio NG Components »
Avio NG Primary Function Display
Avio NG Multi Function Display
The standard multiple, redundant computers, sensors and displays which power Avio NG include:
- Dual aircraft computer systems (ACS)
- Dual full authority digital engine controls (FADEC) per engine
- 3-axis autopilot
- Autopilot control panel (ACP)
- Dual integrated sensor suites (ISS)
- Attitude heading reference system (AHRS)
- Magnetic azimuth detector (MAD)
- Dual global positioning systems (GPS) with Wide Area Augmentation System (WAAS) enabled
- Air data system
- Dual air data computers (ACD)
- Dual static port systems
- Dual combination pitot/angle-of-attack probes
- Secondary pitot probe
- Dual outside air temperature (OAT) sensor probes
- Dual 10.4 inch active matrix liquid crystal flight displays (PFD)
- Single 15 inch active matrix liquid crystal multi function display (MFD)
- Electrical power distribution system (EPDS)
- Dual 200 amp starter generators
- Dual 24 Vdc, 22 amp-hr lead acid batteries
- 127 electronic circuit breaker (ECB)
- Six electronic contactors for fault isolation of the power distribution buses
- Sic main power distribution buses (for equipment buses and two battery buses)
- Smart actuators for landing gear, flaps and autopilot