Fuel mass measurement in each tank and airplane total fuel mass calculation
Calculation of total fuel mass and fuel mass on airplane sides under fuel flow data for each engine
Formation of signal in regards to excess permissible difference between values of total fuel mass, measured by fuel flow meter computed by fuel flow data by each airborne engine
Tanks fuel temperature calculation and temperature near fuel crystallization signal formation
Reserve remaining fuel on each airplane side and fuel consumed reservoirs signals formation
Formation of signal on free water existence in fuel tanks
Automatic and manual fueling control signals formation
Automatic monitoring of sensors serviceability, communication links, measuring-processing block and monitoring results preservation in non-volatile memory for post-flight analysis of system operation
Airplane fuel quantity data formation and output to airborne systems according to standards ARINC-429 and MIL-STD-1553
