Overview

The Shadin Avionics F/ADC-2000 Fuel/Airdata Computer gives you access to more real-time flight information than ever before. Advanced technology has created an aircraft systems' link to your long range NAV with advanced capabilities at an affordable price. The highly-compatible Shadin Avionics F/ADC-2000 will interface with nearly every major GPS and Flight Management System, and automatically calculates real-time fuel, airdata, and navigation information which is displayed through your on-board NAV system, EFIS, and TAWS.

Automatic calculation without manual entry. The F/ADC-2000 unit links aircraft systems and your GPS receiver, automatically calculating fuel used, TAS, true air temperature, OAT, barometric pressure correction, density altitude and wind aloft without manual data entry. This information is totally dynamic in that it is based on real-time wind aloft and fuel flow.The F/ADC-2000 provides high resolution altitude management in ten-foot increments to 35,000 feet to drive the vertical NAV feature of new generation GPS receivers for approaches.In addition, F/ADC-2000 pressure altitude data is automatically used by most GPS manufacturers to substitute for the fourth satellite if it is not in range to compute three-dimensional postion. This provides 24-hour, 3D position accuracy with only three satellites, without manual entry of altitude.

Specifications

Input Data Range
Pitot	20 to 350 kts.
Static	-1000 to 55,000 ft.
OAT	-60°C to +60°C
Heading	0 - 360°
Fuel Flow	1 to 450 GPH Range Selected
K-Factor	500 to 130000 PPG Continuous
Output Data Range
PARAMETER	Accuracy	RANGE
IAS	Table 1	20 to 350 kts.
P.ALT	Table 2	–1000 to 50000 ft.
OAT	±1.5°C per TSO	–60°C to +60°C
TRUE HEADING	±2°	0 - 360 degrees
MAGNETIC HEADING	±1°	0 - 360 degrees
IVS	Table 3	± 10,000 ft./min.
TAS	Table 1	20 - 600 kts.
MACH	Table 4	.2 - .95
WIND SPEED	±5 kts.	5 - 360 kts.
WIND DIRECTION	±10°	0 - 360 degrees
FUEL FLOW	±2%	1 - 450 GPH