Airdriven AA-1 / AA-2 Airship

AA-1
Engine: Rotax 447, 42 hp
Total length: 33.8m
Maximum diameter: 12.6m
Envelope volume: 2600 cu.m
Maximum take-off weight: 650kg
Empty weight: 400kg
Payload: 250kg(2 seats)
Maximum level speed:
20km/h

AA-2
Engine: Rotax 582, 64hp
Total length: 33.8m
Maximum diameter: 13.2m
Envelope volume: 3000 cu.m
Maximum take-off weight: 800kg
Empty weight: 450kg
Payload: 350kg(4 seats)
Maximum level speed: 25km/h

Aircraft Rasukan UCL Maja

A 2004 ultralight, the UCL is a two place single-engine, high wing airplane of conventional configuration consisting of a composite fuselage and wood wings. It is equipped with a fixed tricycle landing gear. +4g/-2g

Stall: 35 kt / 40 mph / 65 kmh
Cruise: 65 kt / 75 mph / 120 kmh
VNE: 86 kt / 99 mph / 160 kmh
Empty Weight: 252 kg / 556 lbs
MTOW Weight: 475 kg / 1047 lbs
Climb Ratio: 800 ft/min / 4.0 m/s
Glide Ratio: 10:1
Take-off distance (50ft obstacle): 490 ft / 150 m
Landing distance (50ft obstacle): 590 ft / 180 m

Aircraft Manufacturing & Design Alarus CH2000

Designed by Chris Heintz and evolved from Zenair, the CH2000 is a two-place powered by a 115hp Lycoming O-235-N2C engine.

Priced at $84,900, ($99,000 IFR) sixty were built.

Alarus CH2000 N470AM

The FAA type certified (Utility/Normal and IFR TC TA5CH) Alarus is of all metal, semi-monocoque stressed skin construction with internal ribs, longerons, and bulkheads distribute the loads. It is simple, tough and easy to inspect and repair. The landing gear system containing a 65 lb piece of metal extending from one wheel to the other to absorb hard landings. New wheel axles are used, similar to other certified aircraft.

The nose gear system is a simple self-centering super tough bungee system and direct nose wheel steering is fitted. At the rear of the fuselage, an aluminum tailskid is attached. The tailskid is mounted on rubber dampeners.
Two different sizes of rudder are available for the 2000, the larger rudder, (used on the “spin certified option”) and a smaller standard sized rudder. Large and responsive flight surface controls make landings in cross winds of up to 25 knots possible.
The Lycoming 0235-N2C powerplant engine is standard including the Sensenich propeller, carburetor air intake filter, muffler system etc.
The cockpit area is manufactured out of Carbon Fiber with molded windshield and side windows. The butterfly (gull) doors open to a cabin of about 46 inches wide. The seats use NASA type Tetra foam, designed for 26g load absorption, and covered with micro porous grey leather-like fabric. The centre section of the seat belts are fastened to the main wing spar and the roll-over-protection tube between the seats. The AmSafe airbag seat belt system is standard equipment on the 2006 model.
For applications that does not require certification (military), the aircraft has been expanded to include a larger Lycoming engine up to 180-200 HP, and increased gross weight to 2,200 lbs. This aircraft is called the SAMA CH2000.

Alarus CH2000
Engine: Lycoming 0235-N2C, 116 hp
Propeller: Sensenich
Gross weight: 1,692 lb
Best climb speed: 63 kt
Rate of climb: 800+ fpm
Cruise: 95-100 kt
Approach speed: 60 kt

SAMA CH2000
Engine: Lycoming O-360, 180-hp
Propeller: fixed-pitch Sensenich 76-EM8-0-63 metal
Gross Weight: 2,200 lb
Empty weight: 1,200 lb
Max level speed: 157 mph / 251 km/h
Cruise speed (75% power @ 7,000 ft) : 150 mph / 240 km/h
Stall speed (flaps down): 47 mph / 76 km/h
Stall speed (flaps up): 58 mph / 93 km/h
Rate of climb: 950 fpm / 4.8 m/s
Service ceiling: 12,800 ft / 3,900 m
Endurance (standard): 3 hrs 45 min
Range (standard): 510 miles / 820 km
Take-off roll: 990 ft / 300 m
Landing roll: 1,150 ft / 350 m

Aircraft Manufacturing & Design Patriot 150

The Patriot 150 aircraft is only being supplied as a factory-built S-LSA aircraft, and is not available in kit form.

Engine: Continental O-200, 100 hp
Wing Span: 32 ft. 10 in / 10 m
Wing Chord: 48 inches / 1.23 m
Wing Area: 132 sq. ft / 12.25 m.sq
Length: 20 ft. 6 in / 6.3 m
Gross Weight: 1,310 lbs / 595 kg
Empty Weight: 785 lb / 356 kg
Useful Load: 525 lb / 240 kg
Fuel Capacity: 24 US Gallons (2 x 12) 90 litres
Load Limits: +6 G / -3 G
VNE (Never Exceed Speed): 143 mph / 230 km/h
Cruise Speed (75%): 124 mph / 200 km/h
Stall Speed: 41 mph / 66 km/h
Stall Speed, no flaps: 46 mph / 74 km/h
Rate of Climb: 1,100 fpm / 5.6 m/s
Range (no reserve): 500 sm / 800 km
Endurance: 5 hours 5 hours
Service Ceiling: 12,000+ ft / 3,660 m
Take-Off Roll: 400 ft / 122 m
Landing Roll: 500 ft / 150 m
Cabin Height: 45 inches / 1.13 m
Cabin Width: 46 inches / 1.16 m
Landing Gear: tricycle, steerable nosewheel
Landing Gear Width: 78 inches 2.0 m
Seats: 2 side by side

Air Command Elite Tandem

The Air Command Commander Elite is a two-seat kitbuilt autogyro. Construction of the tandem-seat F-30 began in late 1999 with the first flight was made on 1 March 2000, and a public debut at Sun ‘n’ Fun, April 2000. A side-by-side version of the F-30 has been introduced.
The Commander Elite features an open cockpit with a range of options and many subassemblies preconstructed by the factory. Quoted build time was 100 hours.
With pre-drilled and anodised 6061-T6 tubular airframe, with a 5 x 5cm tubing used for mast. With an optional glass fibre enclosure, the F-30 has aluminium rudder and composites horizontal stabiliser and tailfins. The optional enclosure givies 10-15 mph higher cruise speed.
The landing gear is of fixed tricycle type with glass fibre speed fairings, aluminium suspension system with Hager wheels and brakes on all wheels, the mainwheel with hydraulic brakes. The nose wheel is fully castoring with a leg of 4130 steel tube and 6.00×6 Azusa tyres: 7.6cm tailwheel.
The pilot and passenger sit in tandem on Elite F-30 and side by side on Elile F-30ES.
Basic engine instrumentation is provided with each kit, and options include hydraulic pre-rorator and clutch reduction drive on F-30; and pre-rotator, C Box upgrade and electric start on F-30ES. Optional is a New Horizons Components gyro recovery system rocket-powered ballistic parachute. Fuel capacity is 37.9 litres in two seat tanks; and an optional 68.1 litre seat tank.

Commander Elite Tandem

Versions were:
Elite F-30: Basic version, with Hirth F-30 engine.
Elite F-30ES: As F-30, but side-by-side seating.
Elite Mazda: As F-30, but with more powerful engine; withdrawn 2002.
Over 200 kits had been sold by the end of 2002.
The kit pricee in 2001 were:
Tandem light weight without engine: $12,570
Tandem heavy weight without engine: $14,235
F-30 Tandem, basic kit: $19,975
F-30 Tandem, all options: $24,975
Mazda Tandem, basic kit: $22,975
Mazda Tandem, all options: $28,450
The 2003 kit prices were: F-30 US$22,475; F-30ES USS21,792, both including engine.
Engine options include the 67 hp Rotax 582, 100-120 hp Arrow or the original 82.0kW Hirth F-30 driving a 68”four-blade Warp Drive propeller and 27’ x 8” Sky Wheels composite rotor blades. Tandems reach speeds up to 120 mph with a 160-hp engine or 110 mph with a 110-hp Hirth F-30, while the side-by-side can get up to only 85 mph with the F-30. A Patrol version came fully equipped with options.

Tandem
Engine: Rotax 582
Width: 5’7”
Height: 8’10”
Length: 13’5”
Empty wt: 450 lb
Useful load: 685 lb
Gross wt: 1135 lb
Min speed: 20 mph
Cruise: 75 mph
Top speed: 105 mph

Tandem 1000
Engine: Arrow 1000, 100 hp
Speed max: 105 mph
Cruise: 75 mph
ROC: 1000 fpm
Take-off dist: 300 ft
Landing dist: 0-5 ft
Service ceiling: 10,000 ft
Fuel cap: 12 USG
Weight empty: 380 lb
Gross: 1000 lb
Height: 8.9 ft
Length: 13.4 ft
Disk span: 27 ft
Seats: 2
Landing gear: nose or tail wheel

Tandem Subaru
Engine: Subaru EJ22, 135 hp
Propellor: 3 blade 68″
Rotorblades: 28-29′ Dragon Wings, Sky Wheels
Take off roll: 350′-750′
Cruise: 65-95 mph
Fuel Consumption: 3-5 gph

Tandem Mazda
Engine: Mazda 13B Rotary, 170 hp
Height: 8.9 ft
Length: 14 ft
Disk span: 29 ft
Empty weight: 700 lb
Gross weight: 1500 lb
Fuel capacity: 14 USG
Max speed: 120 mph
Cruise: 75 mph
Rate of climb: 1000 fpm
Takeoff dist: 350-700 ft
Landing dist: 0-20 ft
Service ceiling: 10,000 ft
Seats: 2

Tandem Hirth F-30
Engines: Hirth F-30, 110 hp
Propeller: Warp Drive 68″
Rotor Blades: 28-29′ / 8.53m Dragon Wings, Sky Wheels
Width: 6’2″ / 1.88m
Height: 9′ / 2.74m
Length: 13’5″ / 4.09m
Empty Weight: 490 lbs / 222kg
Useful Load: 420 lbs
Gross Weight: 910 lbs / 578kg
Max. operating speed: 177km/h
Min Speed: 20 mph / 33km/h
Cruising speed: 121-129km/h
Top Speed: 75-80 mph
Max rate of climb at sea level: 366m/min
Service ceiling: 3050m
Take-off run: 31-76m
Landing run: 0-6m

Tandem Hirth F-30ES
Rotor diameter: 8.84m
Fuselage length: 3.25m
Height to top of rotor head: 2.13m
Width: 1.70m
Max. take-off weight: 412kg
Empty weight: 141kg
Max. operating speed: 135km/h
Cruising speed: 105km/h
Min flying speed: 36km/h
Service ceiling: 3050m
take-off run: 31-76m
Landing run: 0-6m

Air Command Commander Elite Single

Commander Elite Single Place

The single-person Commander has center-line thrust to increases pitch stability and decrease drag. It takes up to a 67-hp Rotax 582 engine, but passes as an ultralight when equipped with a 40-hp Rotax 447. Cruising speeds range from 50 to 65 mph, depending on engine choice. All models can be upgraded to larger engines. Engines options include: 40 hp Rotax 447,52 hp Rotax 503,67 hp Rotax 582, and Hirth 3202 and 3203.
The Air Command Sports Elite is a kit-built gyroplane built in the USA since the early 1990s. Powered by a Rotax 532 engine, the aircraft can take off within 600 feet in still air and can land within 10 feet. The cruising speed is 60 – 80 mph.
Around 65 of the kits were imported into Britain but, after a number of fatal accidents, the aircraft type was grounded by the CAA. After several modifications type regained a flying permit and flew successfully for several years until the CAA again grounded the type.
In 2001 the kit prices were:
without engine: $7935
447 (40 hp) legal ultralight: $9875
503 (52 hp): $11,255
582 (67 hp): $12,675
2704: $12,996
2706: $14,995

Engine: Rotax 582
Rotor Blades: 25ft Dragon Wings, Sky Wheels

Engine: Rotax 447
Propeller: Warp drive 60″ or 68″
Rotor Blades: 23 ft Dragon Wings, Sky Wheels
Min Speed: 8 mph
Cruise: 50 mph
Top Speed: 63 mph
Empty Weight: 252 lbs
Useful Load: 300 lbs
Gross Weight: 552 lbs
Width: 5’7″
Height: 7′ or 7’10”
Length: 10’8″

Engine: Hirth 3202
Propeller: Warp drive 60″ or 68″
Rotor Blades: 25′ Dragon Wings, Sky Wheels
Min Speed: 8 mph
Cruise: 55 mph
Top Speed: 75 mph
Empty Weight: 275 lbs
Useful Load: 320 lbs
Gross Weight: 590 lbs
Width: 5’7″
Height: 7′ or 7’10”
Length: 10’8″

Engine: Hirth 3203
Propeller: Warp drive 60″ or 68″
Rotor Blades: 25 ft Dragon Wings, Sky Wheels
Min Speed: 8 mph
Cruise: 65 mph
Top Speed: 95 mph
Empty Weight: 275 lbs
Useful Load: 475 lbs
Gross Weight: 750 lbs
Width: 5’7″
Height: 7′ or 7’10”
Length: 10’8″