FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering. Aircraft fairing (1) has closed opening (4) with end (5), root (6) and intermediate (7, 8) flaps fixed to fairing by detachable connections (9). Root (6) flap is hingedly (10) connected to fairing shell (1) in area of opening (11). Intermediate flaps (7, 8) are hingedly articulated to each other in pairs (12). One of the intermediate flaps, which is not in connection with two adjacent intermediate flaps, is hingedly connected (13) to end (5) flap, and other 8 is respectively connected (14) to root (6) flap.
EFFECT: invention is aimed at reducing the time for ground maintenance of devices placed under the fairing of an aircraft.
7 cl, 5 dwg
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