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:
-
- 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