FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering. Aircraft fairing (1) comprises elements for fastening (2) to outer surface of housing (3) and has a closed process opening (4). Fairing is equipped with two flaps (5, 6) conjugated with the fairing outer surface and with each other and detachable connections (7) fixed relative to the fairing. Flaps are hingedly (8) articulated with each other. Root flap (6) is hingedly (9) articulated with fairing in opening (4) bypass area.
EFFECT: invention is aimed at reducing the time for ground maintenance of devices placed under the fairing of an aircraft.
6 cl, 3 dwg
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