Ultralight News says:
Sportlite 103 Ultralight | |
The Lite Sport Classic features standard three-axis control, side by side seating using a center-mounted stick and dual throttles and rudder pedals, with a steerable nosewheel.
The Lite Sport Ultra again features standard three-axis controls. It is available in a single place version, or a longer fuselage version two place.
As a single place powered by the Rotax 447UL (40hp) the Lite Sport Ultra is a Legal Part 103 ultralight aircraft.
The kit is available as a raw materials kit in which you do all the cutting, drilling and bending yourself, or as a quick build kit where you bolt the craft together and install your sail covering. | |
The factory reports that approximately 300 aircraft are currently flying.
Free Bird Innovations, Inc.
PO Box 904
1380 Legion Road
Detroit Lakes, MN 56502Phone: 1-800-850-3708 or 218-844-5914 | |
I don't see any other Spec's for the Part 103 version other than what's mentioned above.
For the Light Sport version they say these Spec's.
LiteSport Classic Specifications:
• Gross Weight:
900 lbs
• Empty Weight:
450 lbs
• Useful Load:
450 lbs
• Wingspan: 26 ft
• Wing Area: 121 sq ft
• Length: 17 ft
• Height: 6 ft 2\8 in
• Fuel Capacity: 10 gallons
• Build Time: 125 hours
Performance:
The Engine used for Tests: Rotax
582UL.
• Power:
65 hp
• Cruise: 80 mph
• Stall Speed: 32 mph
• VNE Speed: 110 mph
• Rate of Climb: 800 fpm
• Takeoff Distance: 125 ft
• Top Speed: 90 mph
I found these Spec's for the Part 103 version, but a little confusing, Why they don't just make separate Columns.
Sportlite 103 Specifications Performance | |
Empty Weight | 250 lbs |
Gross Weight: | 530 lbs (single seat) |
Gross Weight: | 900 lbs (two seat) |
Wingspan: | 26 ft 6 in |
Wing Area: | 127 sq ft |
Length: | 16 ft 7 in |
Height: | 6 ft 8 in |
Fuel Capacity: | 5 gallons |
Build Time (kit); | 125 hours |
Build Time (plans): | 250 hours |
Rotax 447: | 40 hp |
Cruise: | 55 mph |
Top Speed; | 62 mph |
Stall Speed: | 22 mph |
VNE Speed: | 75 mph |
Rate of Climb; | 850 fpm |
Takeoff Distance: | 75 ft |
When this plane came out in 2006, the 277UL (28hp) & 377UL (35hp) had already been Discontinued, and the 447UL (40hp) was Discontinued shortly after that. So was the 503UL (50hp).
So if it will make Part 103 Weight of 254 lbs with a Rotax 447UL, it will make Weight with a Rotax 377UL, & 277UL, a Kawasaki 340/440, a Hirth F23, F33, F36, the MZ34, and a Simonini Mini 3, and the Polini 250 DS. Avg Pilot Weight falls between 180-235 lbs.
If Plane is
250 lbs + 30 lbs (GAS) + 235 lb (Pilot) = 515 lbs.
515 lbs = 233.6001 kg / 10 kg = 23.36001 kw needed = 31.32629 hp needed.
Will it Fly at Full at that MTOW of 515 lbs on 26hp, 28hp, Yes! But Performance will suffer. Part 103 is not about Performance as much as about Flight Time with only 5 Gallons!
530 lbs = 240.404 kg / 10 kg = 24.0404 kw needed =
32.23871 hp needed.
900 lbs = 408.2331 kg / 10 kg = 40.82331 kw needed =
54.74496 hp needed!
A 377UL built to the 380HO Spec's can make
[email protected]! It Dynoed
[email protected] with an aftermarket Tuned Pipe! A 447UL is a 377UL 62mm Cylinder Big Bored to 67.5mm. You can actually go up to a 503UL 72mm Bore with a Custom made Sleeve.
With a Good Wide Band Tuned Pipe Designed for 6500rpm, Proper Carb and using 11.5cr:
Rotax:
277UL = 268.8cc/7cc=
[email protected]
377UL = 368.4cc/7cc=
[email protected]
447UL = 436.7cc/7cc=
[email protected]
503UL = 496.9cc/7cc=
[email protected]
Kawasaki:
292 = 292.5cc/7cc=
[email protected]
340 = 339.4cc/7cc=
[email protected]
440 = 435.9cc/7cc=
[email protected]