A mounting apparatus for an aircraft engine that provides load path redundancy includes a forward mount that attaches the aircraft engine to a pylon at a forward position of the aircraft engine, an aft mount that attaches the aircraft engine to the pylon at an aft position of the aircraft engine and a thrust assembly connected to the forward mount, and the aft mount. The forward mount includes an aircraft engine attachment assembly and a fail-safe assembly. The aft mount includes an aircraft engine attachment assembly and a fail-safe assembly.
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