An aircraft subassembly comprises a fuselage structure, comprising a first side and a second side. The aircraft subassembly further comprises a main-landing-gear system, having a single pair of wheels. The main-landing-gear system additionally comprises a sponson, connected to and extending outward from the fuselage structure. The sponson comprises a central portion and a first main-landing-gear door that is moveable relative to the central portion between, inclusively, a closed position and an open position. The sponson further comprises a second main-landing-gear door that is moveable relative to the central portion between, inclusively, a closed position and an open position. The main-landing-gear system further comprises a first main-landing-gear assembly, connected to the first wheel and a second main-landing-gear assembly, connected to the second wheel.


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    Title :

    Aircraft subassembly, having main-landing-gear assembly and sponson, housing main-landing-gear assembly


    Contributors:

    Publication date :

    2021-10-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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