An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within the aft fuselage. A burst zone is defined about the turbine engine and a tail is disposed at least partially with the burst zone. The tail includes primary control surfaces and sacrificial control surfaces. The sacrificial control surfaces can break away in a defined manner to maintain integrity of the primary control surfaces outside of the burst zone.


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    Title :

    Stabilizer Sacrificial Surfaces


    Contributors:

    Publication date :

    2018-10-30


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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