AFC001AC
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Automatic Flight Controller The Archangel Systems Automatic Flight Controller Alternating Current (AFC001AC) is opening the path for legacy aircraft with Interfaces seamlessly with ARINC 429 ADAHRS. analog instruments and Flight Guidance systems to update to modern digital avionics. The AFC001AC receives data over a Hi-Speed ARINC 429 Buss and converts Roll, Pitch and Heading to standard ARINC 407 signals to drive a variety of autopilots, analog indicators and all the functional avionics that require Attitude and Heading ARINC 407 data. Certified for Part 23, 25, 27, and 29 aircraft Accurate Synchro signals for A/P use. Mil Spec 38999 filtered connectors AFC001AC supports Legacy 407 indicator using synchro DG/VGs. This eliminates costly DG/VG repairs and downtime while providing increased performance at a cost-competitive price. Combining the AFC001AC with the Archangel flagship ADAHRS AHR150A will create a seamless and low-cost Air Data and Attitude solution at low-size, weight, and power. CERTIFICATIONS FAA TSO C9c DO-160E Environmental certifications including EMI, EMC, and HIRF EXPORTING Exportable worldwide No end-user statement required www.archangel.com lets.talk@archangel.com 334.826.8008 x22 Dan Reida – Director of Sales 417.896.4407

Automatic Flight Controller Environment/Power Temperature Altitude Power -40°C to +70°C operating -55°C to +125°C non-operating -1,000 to 52,000 ft pressure altitude 16–36 VDC, 0.6 A @ 28 V nominal AFC001AC Dimensions/Weight Size Weight Orbit Flight Data Test ARINC 429 High-speed receive port from input ADAHRS/AHRU Discrete Input Altitude Hold Three discrete fault outputs lines with Discrete two different configurations for the Active Outputs Valid flags (Active High and Low). ARINC 407 Pitch 3 Wire Synchro 200mv / Deg Outputs Roll 3 Wire Synchro 200mv / Deg Heading 3 Wire Synchro 200mv /...