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Wing ribs of a de Havilland DH.60 Moth. In an aircraft, ribs are forming elements of the airframe structure of a wing, especially in traditional construction.. By analogy with the anatomical definition of "rib", the ribs attach to the main spar, and by being repeated at frequent intervals, form a skeletal shape for the wing.
Aircraft utilizing three or more spars are considered multi-spar aircraft. Using multiple spars allows for an equivalent overall strength of wing, but with multiple, smaller, spars, which in turn allow for a thinner wing or tail structure (at a cost of increased complexity and difficulty of packaging additional equipment such as fuel tanks ...
The spars are made of spruce wood with plywood wooden wing ribs. The base engine is a Lycoming O-360 180 hp (134 kW) engine, but alternative examples have been built using the Lycoming IO-540 , Ranger, Ford V-8 and V-6, Continental, Jacobs, and even Pratt & Whitney R-985 engines.
The wing structure comprised steel spars with duralumin ribs and covering, and was braced using steel struts. The aircraft's tail assembly was also composed of duralumin. It was powered by three Bristol Jupiter radial engines, rated at 420 horsepower (310 kW) each, with one mounted in the nose and the other two on the leading edge of the wing ...
The Akro is a cantilever mid wing monoplane with a wooden, two spar mahogany skinned wing built in one piece, its forward spar passing unbroken through the fuselage and the rear spar in two parts. The plain, statically balanced ailerons have steel spars with spruce ribs and trailing edges ; they are fabric covered and carry ground adjustable ...
The aircraft is constructed with fabric covered 4130 steel tube structure and spruce wing spars. Ribs are plywood with cap strips. [1] ... Wing area: 140 sq ft (13 m 2)
Data from Jane's All the World's Aircraft 1948 General characteristics Crew: one, pilot Capacity: two passengers Length: 22 ft 10 in (6.96 m) Wingspan: 35 ft 5 + 1 ⁄ 2 in (10.81 m) Height: 6 ft 10 in (2.08 m) Wing area: 179.3 sq ft (16.66 m 2) Empty weight: 950 lb (431 kg) Gross weight: 1,750 lb (794 kg) Max takeoff weight: 1,753 lb (795 kg) Fuel capacity: 38 US gal (32 imp gal; 140 L ...
F-21 with 42 gal total fuel capacity and 1,750 TOGW. New wing spars and aluminium under-fuselage skinning. 15 built 1985-1990. A further development was the F-22: F-22A Tricycle gear F-22C STOL 180 Tricycle gear 180hp - 1 built
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