Method and apparatus for covering an aircraft engine

Abstract

An apparatus, system and method for covering an aircraft engine. The apparatus comprises front and rear spaced apart plates with an edge engaging portion therebetween and a connector for securing the apparatus to a body to be applied to the aircraft engine shroud. The system comprises a front cover sized to surround a front portion of the aircraft engine, at least one apparatus for covering an aircraft engine at least one hook comprising the apparatus adapted to engage a trailing edge of the shroud of the aircraft engine and a strap operably connected to each at least one hook and extending to the front cover. The method comprises locating the front cover over the front portion of the engine, securing at least one hook to trailing edge of the engine shroud and tightening a strap operably connected to the at least one hook and the front cover.

Dependencies are inferred from the claim text.