FIELD: computer engineering, aviation. SUBSTANCE: device has unit 1 which gathers and inputs flight data, unit 2 which gathers information about fuel rest, board 3 which is used for input and check of internal data, power-independent memory unit 5. Said units are connected to unit 4 which calculates equivalent work load. In addition device has unit 6 which outputs information about calculation results. Results of calculation are displayed on information board of unit 6 which is located in convenient place. In addition results are stored as hard copy. EFFECT: automatic on-board calculation of equivalent workload of constructive members of airframe of airframe using flight data which are received from standard data-gathering unit. 1 dwg
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