Aviat Solo

    A plans built aircraft

    specifications
     
    powerplant

    propeller
    length
    height
    wing span
    wing area
    seats
    empty weight
     useful load
    gross weight
    fuel capacity
    range    		 Rotax 503 with C Box optional. Czech Walter Mikron engines 111 Hirth 2702
    x
     18.5ft
    x
     29ft
    118sq. ft
    1
     540lb
    x
     x
     18gal
    450n.m

    performance

    takeoff distance, ground roll
    rate of climb
    max speed
    cruise speed
    landing distance, ground roll
     service ceiling    		 500ft
    800fpm
    105mph
     85mph
    300 ft
    x

    limiting and recommended speeds

    design manoeuvring speed (Va)
    never exceed speed (Vne)
    stall, power off (Vsl)
    landing approach speed     		x
    x
     35mph
    x

    All specifications are based on manufacturer's calculations