Patent ID: 8899255

Claim:
A turbojet nacelle comprising: an air intake structure for channeling a stream of air towards a fan of the turbojet; a middle structure fastened to the air intake structure, the middle structure having an external housing with an internal casing serving to surround the fan of the turbojet; the air intake structure comprising an internal panel fastened to the internal casing of the middle structure and co-operating therewith to form a stationary structure, and an external panel incorporating an air intake lip at an end of the external panel remote from the middle structure, the external panel being movable in longitudinal translation relative to the internal panel; and further comprising at least one rod including a first end and a second end, the first end fastened on a flange of the air intake lip and the second end terminating in a loop; and an attachment member hinged about a pin secured to a hatch in the external housing of the middle structure, the attachment member engaging the loop of the second end for attaching and locking the external panel to the middle structure by exerting a traction force on the at least one rod, the attachment member actuated manually by a handle housed in the hatch.