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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    Titel :

    Stabilizer Sacrificial Surfaces


    Beteiligte:

    Erscheinungsdatum :

    30.10.2018


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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