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Leupold and Stevens Mark 6 scope with variable magnification 3-18x44mm, mounted on a M24 SWS. IDF M24 SWS with Leupold Mark 6 3-18x44mm sniper scope. Leupold FX-II Ultralight scope on a Ruger 77/44. The company's riflescopes are used by organizations such as the United States Army, the Secret Service and the Navy SEALs. [13]
Data from Original aircraft operating manual General characteristics Crew: one Length: 5.1 m (16 ft 9 in) Wingspan: 9.2 m (30 ft 2 in) Height: 2.5 m (8 ft 2 in) Wing area: 13.34 m 2 (143.6 sq ft) Empty weight: 147 kg (324 lb) with Rotax 447 Gross weight: 250 kg (551 lb) Fuel capacity: 25L (50L fuel tank is usually used instead of the default one) Powerplant: 1 × Rotax 447 or 503 twin cylinder ...
Data from Bayerl General characteristics Crew: one Wingspan: 32 ft 10 in (10.0 m) Wing area: 160 sq ft (14.9 m 2) Empty weight: 205 lb (93 kg) Gross weight: 400 lb (181 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Kawasaki 340 two cylinder, air-cooled, two stroke snowmobile engine, 32 hp (24 kW) Propellers: 3-bladed composite Performance Maximum speed: 65 mph (105 km ...
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category and the US light-sport aircraft rules. [2] [3] It features a strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, retractable wheeled tricycle landing gear and dual floats and a single engine in pusher configuration.
Data from Cliche and the Virtual Ultralight Museum General characteristics Crew: one Capacity: one passenger Wingspan: 32 ft (9.8 m) Wing area: 160 sq ft (15 m 2) Empty weight: 253 lb (115 kg) Gross weight: 680 lb (308 kg) Fuel capacity: 4.5 U.S. gallons (17 L; 3.7 imp gal) Powerplant: 1 × Kawasaki 440 twin cylinder, two-stroke snowmobile engine, 40 hp (30 kW) Performance Maximum speed: 51 ...
The use of the 28 hp (21 kW) Rotax 277, or the similar weight and power Hirth F-33, allows the aircraft to fit into the US ultralight category if weight is carefully controlled during construction. However the H-3 is underpowered with this engine and most have been equipped with heavier engines of higher output, such as the 40 hp (30 kW) Rotax ...
Data from Cliche and the Virtual Ultralight Museum General characteristics Crew: one Length: 10 ft (3.0 m) Wingspan: 35 ft (11 m) Height: 11 ft (3.4 m) Wing area: 180 sq ft (17 m 2) Empty weight: 160 lb (73 kg) Gross weight: 380 lb (172 kg) Fuel capacity: 2.5 U.S. gallons (9.5 L; 2.1 imp gal) Powerplant: 1 × Zenoah G-25 single cylinder, two-stroke engine, 20 hp (15 kW) Propellers: 2-bladed ...
The Ultravia Pelican is the name given to two series of high-wing, single-engine, tractor configuration ultralight aircraft that were designed by Jean Rene Lepage and produced in kit form for amateur construction by Ultravia Aero International of Mascouche, Quebec and later Gatineau, Quebec. [1] [2] [3] [4]
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