CN-4312 provides problem solving of navigation, planning, trajectory prediction, aircraft equipment control and air navigation process control using P RNAV requirements with RNP 0.3, RNP 1, RNP 5 accuracy.
Basic modes of navigation parameter determination: SNS, SNS SBAS, SNS GBAS, IS/ADS (Inertial System/ Air Data System), DME/DME, VOR/DME.
CN-4312 provides a joint operation with user and aeronavigation by data bases, automated control of interactive systems, performing of SID/STAR/ APPROACH procedures, categories 1, APV2, APV1 landing in differential mode.
CN-4312 equipment meets the requirements of the following documents:
КТ3401 (class A1, B1, С1), КТ178А, 9613 AN/937, JAA TGL-10.
| 24-channel receiver | GPS/GLONASS/SBAS data recovery 10 Hz |
|---|---|
| Display: - color LCD, display format | 78,7x53,6mm |
| User database: | 1000 WPT and 90 routes |
| Operating temperatures: - RICU (receiver indicator and control unit): - UPS (uninterruptible power supply) - A (antenna): - LNA-SSF (Low Noise Amplifier) | from – 20° C tо + 55° C from – 20° C tо + 55° C frоm 55° C tо + 85° C from 55° C tо + 55° C |
| Supply voltage: | + 27 V |
| Power consumption: | no more than 20 W |
| Dimensions: - RICU: - UPS: - A: - LNA-SSF: | 181х87х252 mm 160х173х52 mm 55x73,6x119,6 mm 140,5х70х19,5 mm |
| Weight: - RICU: - UPS: - A: - LNA-SSF: | no more than 2,5 kg no more than 1,1 kg no more than 0,2 kg no more than 0,24 kg |
| Digital interfaces: ARINC 429 8 inputs/4 utputs; 1PPS | 1 channel |
| Analog interfaces: - Output (±10 V) - current outputs (±150 mV) | 1 channel; 3 channels. |