ATC / TCAS Rotary

Description

• Dual Mode-S configuration
• Transponder fail indicator (amber)
• Ident function
• Rotary knob entry for ATC code
• Altitude reporting OFF-ON
• Altitude source 1-2 selection
• Transponder 1-2 selection
• TCAS TA only, TA/RA
• System test function
• ABV/N/BLW function
• Altitude limit range: A = 2,700 ft, B = 7,000 ft
• Flight level function
• Built-in-test (BIT) capability
• Non-volatile storage of ATC code
• Modular design provides flexibility for custom layouts
• Modular construction contributes to economical maintenance