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  • Bell XV-15A

    1977










    Bell XV-15A

    The XV-15 was Bell's second successful experimental tiltrotor aircraft after the XV-3. Powered by two 1550 shps Textron Lycoming LTC1K-4K turboshaft / turboprop engines derivated of the T53-L-13B.

    See also Bell 301 XV-15




    Specifications


    Engine: 2 x Lycoming T53-L-13 1400 shp
    Capacity: 2 + 9
    Length: (m) 12.83
    Height: (m)
    Blades: 6
    Rotor diam.: (m) 7.62
    Disc area: (m2) 91.21
    Weight: (kgs) Empty: 4354     Max: 5897
    Speed: (km/h)     Max: 615
    Range: (km) 825
    Ceiling: (m)
    Rate/Climb: (m/min)
    blueprints


    List of Operators of Bell XV-15A


    From Organisation with model XV-15A
    1978
    usa NASA
        2 1978/03


    Construction Numbers on database of XV-15A or its versions

    2XV-15A




    Construction Numbers

    Help Us

    C/NBuilt asYearHistory
    0001 1977 US N702NA
    0002 US N703NA

    2 C/N.


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