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
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
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
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 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
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