| 摘要 |
An engine cowl door assembly is provided for fuselage mounted turbine engines to minimize manufacturing costs and part counts. In one embodiment, the engine cowl door assembly includes at least one non-handed engine cowl door, a pylon apron coupled to the fuselage of an aircraft and providing an attachment point for a first portion of the engine cowl door and a fairing coupled to the turbine engine and providing a latching point for a second portion of the engine cowl door to the turbine engine. The pylon apron, positioned on an inboard side of the turbine engine, and the fairing, positioned on an outboard side of the turbine engine, are identically shaped to provide interchangeability of the engine cowl door from a turbine engine mounted on a first side of an aircraft fuselage to a turbine engine mounted on a opposed second side of an aircraft fuselage.
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