FIELD: aviation.
SUBSTANCE: invention relates to an air intake of an aircraft engine. The air intake contains disassembly mechanism (100) having panel (100). Movable panel (100) is configured for attachment to a nacelle, using fasteners configured for being accommodated as a single whole in the nacelle. Disassembly method (100) has a cavity formed in a thickness of the air intake and closed with the movable panel in a flush closed position. Fasteners contain movable radial rods configured for connection to movable panel (110) and attachment to the air intake by means of a two-positioned cross-beam.
EFFECT: simplification of maintenance of a nacelle with preservation of an aerodynamic function.
13 cl, 18 dwg
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