Abstract: An aircraft engine assembly including a mounting pylon including a rigid structure fitted with a central box, together with a forward extension and a rear extension each including an attached upper organ supported on an upper surface of the central box, and an attached lower organ supported on a lower surface of the front end. The forward and rear extensions support at least a part of the first fasteners interposed between the rigid structure and a turbine engine.
Type:
Application
Filed:
November 30, 2009
Publication date:
January 12, 2012
Applicant:
AIRBUS OPERATIONS (inc as a Societe per Act Simpl)