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It features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear and a twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration. [1] The aircraft fuselage is made from bolted-together aluminum tubing. Its 22 ft (6.7 m) diameter rotor has two blades.
The aircraft has a 4130 steel tube frame fuselage and a wing constructed from aluminium tubing, all covered in doped fabric. The wings are equipped with slotted-style flaps and fold for transport or storage without a requirement to disconnect the flaps and ailerons. The landing gear is bungee suspended. The Sky Raider has a fully enclosed ...
Data from Purdy, Cliche & InterPlane General characteristics Crew: one Capacity: one passenger Length: 20 ft 0 in (6.10 m) Wingspan: 34 ft 5 in (10.49 m) Wing area: 163.6 sq ft (15.20 m 2) Empty weight: 490 lb (222 kg) Gross weight: 1,000 lb (454 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 twin cylinder two-stroke aircraft engine, 64 hp (48 kW) Performance Maximum ...
Pages in category "Single-engined jet aircraft" The following 200 pages are in this category, out of approximately 396 total. This list may not reflect recent changes .
A monoplane is a fixed-wing aircraft configuration with a single mainplane, in contrast to a biplane or other types of multiplanes, which have multiple planes. A monoplane has inherently the highest efficiency and lowest drag of any wing configuration and is the simplest to build. However, during the early years of flight, these advantages were ...
Single-engined jet aircraft (396 P) P. Single-engined twin-prop pusher aircraft (18 P) Single-engined pusher aircraft (1 C, 1,128 P) S. Single-engined helicopters (1 C)
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The new aircraft was the Martin 4-0-4. It had structural changes to the wings, pressurization and was lengthened slightly to take 40 passengers. Like the earlier 2-0-2, the 4-0-4 was a cantilever monoplane with a standard tail unit (cantilever tailplane and single vertical