
Century
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 121 kt / 140 mph / 225 kmh
VNE: 167 kt / 193 mph / 310 kmh
Empty Weight: 290 kg / 639 lbs
MTOW Weight: 600 kg / 1323 lbs
Climb Ratio: 1200 ft/min / 6 m/s

Century
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 121 kt / 140 mph / 225 kmh
VNE: 167 kt / 193 mph / 310 kmh
Empty Weight: 290 kg / 639 lbs
MTOW Weight: 600 kg / 1323 lbs
Climb Ratio: 1200 ft/min / 6 m/s

Rally
Stall: 35 kt / 40 mph / 65 kmh
Cruise: 107 kt / 123 mph / 198 kmh
VNE: 145 kt / 167 mph / 269 kmh
Empty Weight: 345 kg / 760 lbs
MTOW Weight: 599 kg / 1320 lbs
Climb Ratio: 1200 ft/min / 6,5 m/s
Storm Aircraft Rally LSA
New price: $107,900
Engine: Rotax 912 ULS, 100 hp
TBO: 1500 hr
Fuel: 100/mogas
Propeller: 70-inch, 3-blade FP
Landing gear type: Tri./Fixed
Max ramp weight:1320 lb
Gross weight: 1320 lb
Landing weight: 1320 lb
Empty weight, std: 760 lb
Useful load, std: 560 lb
Usable fuel, std: 21 USG
Payload, full std. fuel: 434 lb
Wingspan: 30 ft. 1 in
Height: 7 ft
Wing area: 125 sq. ft
Wing loading: 10.6 lbs./sq. ft
Power loading: 13.2 lbs./hp
Wheel size: 5.00 x 5 in
Seating capacity: 2
Cabin doors: 2
Cabin width: 43.7 in
Cabin height: 40 in
Cruise speed 75% power @ 24,000 ft.: 107 kt
Fuel consumption 75% power: 6 USgph
Vso: 35 kt
Best rate of climb (SL): 800 fpm
Service ceiling: 12,000 ft
Takeoff ground roll: 360 ft
Takeoff over 50-ft. obstacle: 600 ft
Landing ground roll: 450 ft
Landing over 50-ft. obstacle: 1000 ft

Rino Stoof of Cambridge, New Zealand, built his Stoof Joyrider in the late 1990s/early 2000s and got it to the stage of carrying out engine runs. Unfortunately it never made it into the air, but it was registered with CAA.
The tri-gear Stoof Joyrider was of all-wooden construction and had removeable wings and tailplane. It had a wingspan of around 10 metres and a length of around 6 metres. It was powered by a 2 litre EJ 20 Subaru engine with a Hintz gearbox and was fitted with a Ballistic Recovery Parachute.
ZK-RYD (c/n 05/01) was registered to Rino P P Stoof of Cambridge on 14 April 2005. It was withdrawn and cancelled from the register on 8 May 2013.
The 1931 Stone & Fry S-2 registered N10642 c/n 4 was a single place open cockpit monoplane, powered by a 120hp Anzani engine.
In 1931 Edward R Stone of Wichita KS., USA, built the B-2 type of aircraft. It is known that it was registered N568Y and powered by a Packard diesel engine.

The ‘Hybrid’ was completed by C.B. Stone in 1936. The fuselage is part of a Heath Parasol built about three years prior. The landing gear and centre section were designed by Stone, and the radiator was from one bank of a Hisso engine.
Top speed: 85 mph
Cruise: 70 mph
Landing speed: approx 40 mph

Franz Stolz built his design in 1909 in the German town Rastatt. Due to its form it was named the ‘Torpedo-Flugmaschine’ [Torpedo Flying machine]. To fund (further) construction the design of Stolz was exhibited against payment in the Carl Franz Halle, but this financial help was not enough. Stolz had to auction his machine in December 1909 and the machine never did fly.

Designed by Lou Stolp as a low-cost, low-horsepower, fun machine, it is inexpensive, easy to build, and very easy to fly. Basically a biplane version of the parasol-winged Starlet. First flown in 1981, the light wing loading insures a slow landing speed and short takeoff. Stability is excellent and ample control surfaces give rapid response to light control pressures.
The structure is stressed to withstand both plus and minus 9 G’s, and horsepower may vary from 60 to 125. With the 65 HP Continental, the rate of climb is about 600 fpm, cruise speed is 75 mph, stall speed is 35 mph. This aircraft also flies well with a Rotax, Subaru, Suzuki, or Lycoming engine.
The fuselage is constructed of welded steel tubing, and the wings have spruce spars and plywood ribs with 1/4″ cap strips. Raw material kits as well as kits with the tubing cut to length and scribed for fitting are available. Wing Kits may be bought with finished spars, spar plates, ribs cut out, and fittings cut to size.

Engine 100-hp Con¬tinental.
Gross Wt. 1000 lb
Empty Wt. 650 lb
Fuel capacity 20 USG
Wingspan 23’
Length 17’2”
Wing area: 141 sq.ft
Top speed 150 mph
Cruise 90 mph
Stall 35 mph
Climb rate 1800 fpm
Takeoff run (50’) 300 ft
Landing run (50’) 500 ft
Range 350 miles
Seats: 1
Engine: 65 hp
Speed max: 90 mph
Cruise: 75 mph
Range: 275 sm
Stall: 40 mph
ROC: 600 fpm
Take-off dist: 400 ft
Landing dist: 600 ft
HP range: 65-150
Fuel cap: 15 USG
Weight empty: 700 lbs
Gross: 1000 lbs
Height: 7.4 ft
Length: 17.1 ft
Wing span: 23 ft
Wing area: 141 sq.ft
Seats: 1
Landing gear: tail wheel

Designed by Jim Osborne & Morgan Schrack the Acroduster Too, originally called the Schrack-Stolp Super Star-duster Too, is a scaled-down 9/10 scale version of the Starduster Too and first flown in 1984. The Acroduster Too SA750 is a fully aerobatic, two-place machine stressed to plus & minus 9 G’s. It has modified symmetrical wings and is meant for minimum of 180 and up to 360 horsepower. It possible to remove the front windscreen, cover the front cockpit with a hatch cover, and add a sliding bubble canopy over the rear hole. The fuselage was also metalized back to the rear of the cockpit.
The optimum engine is the fuel-injected 200 HP Lycoming, with constant speed propeller. The prototype cruises about 160 mph, climbs 2300 fpm, and stalls at 55 mph. Although it has a comparatively sharp stall and sensitive control response, wings can be maintained in the level attitude with rudder alone or with aileron. This with stick full back by reducing power to idle and zero climb until stall is obtained.

Construction follows traditional biplane practices with steel tube structure and spruce wing spars. Ribs are plywood with cap strips.
All materials were available from Stolp Starduster Corporation, either in kit form or as raw materials.

Engine: 200 hp
HP range: 180-300
Height: 6.8 ft
Length: 18.5 ft
Wing span: 21.4 ft
Wing area: 130 sq.ft
Weight empty: 1050 lb
Gross: 1950 lb
Fuel cap: 35 USG
Speed max: 185 mph
Cruise: 155 mph
Stall: 55 mph
ROC: 2300 fpm
Landing dist: 1200 ft
Service ceiling: 16,000 ft
Seats: 2
Landing gear: tail wheel
Engine: 200 hp
HP range: 180-300
Height: 6.8 ft
Length: 18.5 ft
Wing span: 21.4 ft
Wing area: 130 sq.ft
Weight empty: 1050 lb
Gross: 1950 lb
Fuel cap: 35 USG
Speed max: 185 mph
Cruise: 155 mph
Stall: 55 mph
ROC: 2300 fpm
Landing dist: 1200 ft
Service ceiling: 16,000 ft
Seats: 2
Landing gear: tail wheel

First introduced in 1973, the SA-700 Acroduster is a single-seat, fully aerobatic biplane suitable for engines in the 125-200 hp range. Its fuselage is an all-metal structure constructed from light alloy, and its wings are conventional two-spar structures with spruce spars, plywood ribs and fabric covering. A unique feature of the Acroduster 1 is that when the stick is pulled back, all four ailerons are raised slightly to help maintain aileron control when the airplane is stalled in a normal attitude. The opposite happens when the stick is pushed forward to aid control when the airplane is in an inverted stall.

The Acroduster uses com¬pletely separate wing panels pinned in the center with a pivot type joint and tied to the fuselage with an open stance ca¬bane that has four mounting points on the wings.
They are always building from a kit because Osborne won’t sell a set of plans without the com¬plete materials kit to keep them compa¬ny. The kit is literally a complete, but disassembled, airplane that needs only the engine and propeller. Even the motor mount and gas tank are completely fin¬ished and ready to nail in place.
Engine: Lycoming, 200 hp
Height: 6.25 ft
Length: 15.75 ft
Wing span: 19 ft
Wing area: 105 sq.ft
Weight empty: 740 lb
Gross: 1190 lb
Aerobatic Weight 1050 lb
Fuel cap: 25 USG
Wing Loading 10 lb/sq ft
Power Loading 5.25 lb/hp
Speed max: 180 mph
Cruise: 165 mph
Stall: 70 mph
ROC: 3000 fpm
Service ceiling: 12,000 ft
Seats: 1
Landing gear: tail wheel
Aerovant Aircraft Corp Acroduster I
Engine: Lycoming, 200 hp
Height: 6.3 ft
Length: 15.8 ft
Wing span: 19 ft
Wing area: 105 sq.ft
Fuel capacity: 25 USG
Empty weight: 740 lb
Gross weight: 1190 lb
Top speed: 180 mph
Cruise: 165 mph
Rate of climb: 3000 fpm
Service ceiling: 12,000 ft
Seats: 1
Landing gear: tailwheel