| Specifications
- Media Interfaces: USB
- Optional 3.5-inch floppy disk (1.44MB)
- Aircraft Interfaces:
- 615-3 ARINC 429: 4 output, 8 input
- Ethernet: 2 channel, 10/100 Base Tx
- Discretes: 8 input, 8 output
- Upgradeable to ARINC 615A
- Internal Mass Storage: 256MB to 16 GB
- Display: 3.5 inch LCD
- Size: 5.75" W x 7.5" D x 4.5" H (146 x 203 x 114 mm)
- 5.75" W x 7.5" D x 3.75" H (146 x 190 x 95 mm)
- Weight: < 7 lbs / 3.2 kg
- Power Source: 115 VAC 400Hz or 28 VDC
- Environmental: DO-160E
Typical load configurations
Validation tests are systematically performed with each avionics system load configuration.
Typical load configurations include:
- Fight Management Systems (FMS)
- Integrated Display System (IDS)
- Aircraft Condition Monitoring System (ACMS)
- Advanced Cabin Entertainment and Service System (ACESS)
- Central Management System (CMS)
- Automatic Flight System (AFS)
- Centralized Fault Display System (CFDS)
- Aircraft System Controller (ASC)
- Flight Management Computer System (FMCS)
- Electronic Display System (EDS)
- Aircraft Data Acquisition System (ADAS)
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