103SOLO - Ultralight

103SOLO - Ultralight

103SOLO - Standard 

FAA Part 103 Vehicle

$7,500 to confirm your kit reservation

 

103SOLO Pricing:

 

Deposit = $7,500

 

- without engine / avionics / propeller = $15,500

- with engine / avionics / propeller = $22,000

- Option: Ballistic Chute = $3,000

 

Ultralight Model:

 

    Single Seat - standard stick and rudder controls
  • High Wing Designed for Back Country Flying and Weekend Adventure
  • Polini Thor 250 Engine, Basic Avionics, Prop, Fuselage, Wing, & Tail Parts. Main Wheels Set, Matco Hydraulic Disc Toe Brakes &  Tail Wheel
  • Ultralight – Meets FAA Part 103
    • No license required to fly
    • No registration required to fly
    • No medical required to fly

 

 

  • Performance Parameters / Limitations / V-speeds

                           

     Performance Parameters                            

    Configuration

    Single Place – Conventional Gear

    Empty Weight

    254 lb.

    Gross Weight

    550 lb.

    Length

    17.5 ft.

    Wing Span

    28.4 ft.

    Wing Area

    122 ft2

    Wing Load Limits @gross weight

    4.0

    Design Load Limits @gross Weight

    +4/-2

    Stall Speed

    24 mph

    Cruise Speed

    50 mph

    Aft Stability Limit

    25.3 in.

    Aft CG

    22.8 in.

    Roll Rate

    45-degree bank to 45-degree bank in 2.5 seconds

    Take off Distance

    350 ft.

    Landing Distance

    300 ft.

    Fuel Capacity

    5 gal.

    Endurance

    2 hrs.

    Fuel Consumption

    2 gallons/hour

    Range

    50-100 miles

     

    Limitations / V-speeds

    VNE

    100 mph

    VA 

    48 mph

    VY

    30 mph

    VX

    27 mph

    VS

    24.1 mph

    VSO

    22 mph

    V(Max)

    54 mph at 37 Hp

    Rate of Climb

    650 ft/min

    V (Min Sink)

    27.3mph

    Min Sink Rate

    580 ft/min

    VR

    28 mph

    Max Crosswind Component

    10 mph

    Max Wind Speed

    25 mph

    Max Bank Angle

    45 degrees

    Max Pitch Angle

    30 degrees

    L/D= @35 mph

    4.6

    Drag Polar = C(D)

    0.13+0.088*(C(L)^2)

     

    Permissible fuels: Refer to engine manual

    Maximum RPM: Refer to engine manual

$15,500.00Price