FIELD: aviation. SUBSTANCE: deviations of edges of doors are determined with the aid of oscillation amplitude and frequency sensors which are positioned in way of flight on front wall of each compartment of fuselage for fine adjustment of sensor position relative to mating surface of bearing member of door at angle of 90 deg relative to it; mating surface of door is located on joint of transverse and longitudinal edges for performing adjustment by means of shims. EFFECT: enhanced accuracy of determination of degree of drawing off the compartment doors under varying flying conditions. 2 cl, 5 dwg
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Authors
Dates
1995-08-20—Published
1990-02-02—Filed