9628201BS3

ADC 200 Digital Air Data Computer with Barometer Corrected Altitude

THE -1-B-S-3 INCORPORATES DC BARO-CORRECTION INPUT FROM A KEA-130A HONEYWELL ALTIMETER AND OUTPUTS BARO CORRECTED ALTITIUDE.UNIT WAS MFG FOR RAYTHEON BONANZA'S & BARONS.

Designed to interface with the latest GPS systems on the market, the ADC-200 delivers real-time fuel management information, winds aloft, and airdata information to instantly alert the pilot to changing flight conditions. The ADC-200 is remote-mounted, and requires no valuable panel space since all calculated functions are viewed directly on the GPS!

RS232/422 output fed to the GPS receiver automatically generates the following information to appear on the GPS fuel and wind pages:

• Individual engine fuel flow (GPS calculates fuel remaining/used, fuel to destination, left/right engine used)
• TAS, winds aloft, wind component
• Mach, Indicated Air Speed, Instantaneous Vertical Speed, True Air Temperature, Rate of Turn, Outside Air Temperature, Pressure Altitude, Density Altitude, Magnetic Heading.

Calculated pressure altitude fed from the ADC-200 to the GPS substitutes as 4th satellite navigation information, saving expense of wiring the existing encoder to the GPS.

For jet operators, pitot/static source error correction curves were added to ensure accurate pressure altitude and indicated airspeed readouts. A bootstrap HSI must be installed for heading information.

	Size:	6.3"L x 3.4"W x 3.5"H
	Weight:	20 oz.
	Operating Temperature:	-40°C to +70°C
	Operating Altitude:	Up to 55,000 feet
	Protection:	Not internally fused
	Power Supply:	28 VDC @ 1300 mA or 14 VDC @ 900 mA
	Categories:	F2BA(PKSMNO)XXXXXXBBBBAB
	Software:	DO-178A Level II
	Hardware:	DO-160B
	Input:	Pitot/Static Heading Synchro XYZ information from an HSI bootstrap, OAT from a Shadin Avionics OAT probe (supplied), Fuel Flow information (may require transducers), RS-232 / RS-422 from GPS
	Output:	RS-232 / 422 fed to the GPS receiver to display the following information: Individual engine fuel flow (GPS calculates fuel remaining/used, fuel to destination, left/right engine used, etc.), TAS, Winds Aloft, Wind Component, Mach, IAS, IVS, TAT, ROT, OAT, PA, DA, MH
	TSO Category:	C106, C44a
	Manufacturer's W arranty:	12 Months

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