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Эксплуатация, продажа и аренда воздушных судов. Самолеты Ан-24, Ан-26, Ан-26Б-100. Приобретение и продажа запасных частей к самолетом Российского производства.
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Radar altimeter transceiver utilized in AA-300 Radio Altimeter System
Used to measure the altitude Above Ground Level (AGL)
Can be hard mounted toaircraft or mounted in shock isloated tray
Precision altitude output used to drive primary radio altitude display in up to five RA-315 or RA-335 indicator or EFIS displays
Auxiliary altitude putput is ARINC 552 signal used to drive rising runway bar in any Honeywell Altitude Director Indicator
In -9X1/-9X3/-9X4/-9X5 units, auxiliary output is limited to 0-500 foot range
In -9X2/-9X6/-9X7/-9X8 units, auxiliary output is full scale ARINC 552 (0-2500 feet)
Four trip point outputs available that provide a ground when system determines it is at or below the altitude associated with trip point
Pilot Activated Self Test (PAST) input available to verify system operation
Two separate inputs provided to inhibit self-test operation and may be used to prevent self-test when aircraft flight control system is engaged
Valid output signifies system status and separate logic output indicates when unit is tracking return signal
-91X,-92X, and -93X units have incorporated products improvements to improve ability to popeate in condition of excessive antenna leakage and interference signals
-93X units have improved HIRF immunity by way of added filtered connector to provide more RF filtering
