KSG7200 Air Data Attitude Heading and Reference System
Additional features include:
- Honeywell designed and produced pressure and aviation-grade MEMS sensors for maximum accuracy and reliability – no global positioning system augmentation required
- Automated integrity monitor detects and eliminates incorrect attitude information, leading to improved safety and reduced pilot workload
- System can re-initialize in flight
- Reduced vertical separation minimum (RVSM)-compliant air data computer
- Remote-mounted for improved performance and ease of installation
- Automated aircraft alignment
- ARINC 429 digital output
- Airspeed gain scheduling of the flight control system
- Redundant sensor set for altimetry and airspeed
- Static source error correction (SSEC) for either altitude or airspeed
Specifications
Key Differentiators
Certifications
- TSO C3d, C4c, C6d, C106d
Features & Benefits
- ARINC 429 digital output
- Automated integrity monitor detects and eliminates incorrect attitude information, leading to improved safety and reduced pilot workload
- Honeywell-designed and -produced pressure and aviation-grade MEMS sensors for maximum accuracy and reliability – no GPS augmentation required
- Static Source Error Correction (SSEC) for either altitude or airspeed
- System can re-initialize in flight
Dimensions
Length
- 10.91 in.
- 27.71 cm
Width
- 14.71 cm
- 5.79 in
Weight
- 2.59 kg
- 5.70 lbs.
Dimensions
- 15.04 cm x 14.71 cm x 27.71 cm
- 5.92 in. x 5.79 in. x 10.91 in.
Performance Data
Power
- 15 to 34 VDC Watt
Temperature range
- -55°C to +70°C
Environment
- [A2F2]BBBSREWXXXXABA[BZ]ZKGMA3J33XXA
Mounting
- Remote rack
Altitude
- 55,000 ft. unpressurized foot
Cooling
- No external cooling required
Output
- ARINC 429 digital output