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Main spar of a de Havilland DH.60 Moth. In a fixed-wing aircraft, the spar is often the main structural member of the wing, running spanwise at right angles (or thereabouts depending on wing sweep) to the fuselage. The spar carries flight loads and the weight of the wings while on the ground.
Data from Manufacturer's website & Kitplanes General characteristics Crew: one Length: 16 ft 6 in (5.03 m) Wingspan: 30 ft 6 in (9.30 m) Height: 5 ft 0 in (1.52 m) Wing area: 120 sq ft (11 m 2) Empty weight: 254 lb (115 kg) Gross weight: 535 lb (243 kg) Fuel capacity: 5 US Gallons (19 litres) Powerplant: 1 × Hummel Half VW 1037 cc four-stroke, two-cylinder horizontally opposed aircraft engine ...
A fixed-wing aircraft is a heavier-than-air aircraft, such as an airplane, which is capable of flight using aerodynamic lift. Fixed-wing aircraft are distinct from rotary-wing aircraft (in which a rotor mounted on a spinning shaft generates lift), and ornithopters (in which the wings oscillate to generate lift).
The city of Los Angeles briefly flew a fleet of Bell 407s in the late 1990s as a replacement for the AS-350B1s. However, in 2000 the LAPD started replacing the 407s with more powerful AS-350B2s. Two of the 407s were sold to the General Services Department, which uses the helicopters on flights for the Department of Water and Power. [citation ...
Data from Kitplanes, Murphy Aircraft and The Incomplete Guide to Airfoil Usage General characteristics Crew: one Capacity: one passenger Length: 18 ft 5 in (5.61 m) Upper wingspan: 21 ft 0 in (6.40 m) Lower wingspan: 19 ft 8 in (5.99 m) Height: 6 ft 5 in (1.96 m) Wing area: 153 sq ft (14.2 m 2) (168 sq ft with optional rounded wing tips) Airfoil: NACA 23012 Empty weight: 375 lb (170 kg) Gross ...
Structural metal fatigue was the problem in a major wing spar. Alloy 7075-T6 was used, which is susceptible to stress-corrosion cracking and low toughness. The airliner was grounded and modifications were made. The wing components were redesigned and the engines replaced. The changed type was designated the Martin 2-0-2A.
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The retirement life of the wing spar of a transport category aeroplane type-certificated to the safe-life principle is based on a safety factor applied to data obtained from flight tests and information about properties of the spar material. The life of 11,400 flights for the Viscount inner lower boom was based on safety factors of 3.5 for the ...
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