Options

• Vibrating cylinder pressure sensors
• RVSM compliant
• RTCA/DO-178 B Level A Software
• RTCA/DO-160 D Env. CAT YY tested
• Static Source Error Correction, 2 x 16 curves
• Continuous Built-In-Test
• BIT Failure memory
• RS232 Maintenance Interface

Approved with TAWS-Systems from Honeywell, Sandel, Universal Avionics
and L3.
Approved with EFIS-Displays from Rockwell Collins, Universal Avionics and
Chelton Flight Systems.
Approved with digital Flight Recorder MADRAS from L3