FEATURES

    * Fuel/Airdata Computer
    * Interfaces with the latest GPS systems to deliver real-time fuel management information, winds aloft, & airdata information
    * Remote-mounted, all calculated functions are viewed directly on the GPS
    * Calculated pressure altitude fed from the ADC-200 to the GPS substitutes as 4th satellite navigation information
    * For jet operators, pitot/static source error correction curves were added. A bootstrap HSI must be installed for heading information.
    * RS232/422 output fed to the GPS receiver automatically generates the following information on the GPS fuel & wind pages:
         - Individual engine fuel flow
         - 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


SPECIFICATIONS
Weight:     20 oz.   
Size:     6.3"L x 3.4"W x 3.5"H
Temperature:     -40°C to +70°C   
Altitude:     Up to 55,000 feet
Protection:     Not internally fused     
Power Supply:     28VDC @ 1300mA or 14VDC @ 900mA
Categories:      F2BA(PKSMNO)XXXXXXBBBBAB     
Software:     DO-178A Level II
Hardware:     DO-160B     
Input:     Pitot/Static Heading Synchro XYZ info from an HSI bootstrap, OAT from a Shadin Avionics OAT probe, Fuel Flow info (may require transducers), RS-232/422 from GPS
Output:     RS-232/422 fed to the GPS receiver to display the following info: 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