FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular, to the placed between the engine and the nacelle skins structures. Located between the aircraft engine and the nacelle skin structure comprises casing surrounding the engine and comprising plurality of sectors (12A, 12B), at least one radial bracket (14) providing connection to the nacelle; and plurality of fastening means for the said plurality of casing sectors attachment to each other or to the said at least one radial bracket. Plurality of fastening means comprises plurality of connecting plates (20). Each plate is made with two parallel rows of holes for reception of two corresponding rows of head bolts. First row passes through the corresponding plurality of holes of one casing sector, and the second row passes through the corresponding plurality of holes of the adjacent casing sector or adjacent radial bracket.
EFFECT: enabling easy access to the equipment components with minimizing the air flow interferences.
6 cl, 3 dwg
