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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.
Ordnance crest "WHAT'S IN A NAME" - military education about SNL. This is a historic (index) list of United States Army weapons and materiel, by their Standard Nomenclature List (SNL) group and individual designations — an alpha-numeric nomenclature system used in the United States Army Ordnance Corps Supply Catalogues used from about 1930 to about 1958.
The Mite is constructed mainly of fabric-covered wood, with a single spruce and plywood "D" wing spar. The wing aft of the spar is fabric-covered. [2] The airfoil selected for the design was the NACA 64A215. [3] The M-18 represented the first time a NACA 6-series airfoil had been used on a civil aircraft after World War II. [1]
Data from Sport Aviation, Plane & Pilot and Purdy General characteristics Crew: one Capacity: one passenger in tandem seating Length: 22 ft 5 in (6.83 m) Wingspan: 35 ft 3 in (10.74 m) Height: 6 ft 8 in (2.03 m) Wing area: 178.5 sq ft (16.58 m 2) Airfoil: USA 35B Empty weight: 695 lb (315 kg) Gross weight: 1,400 lb (635 kg) Fuel capacity: 12 US Gallons, 45.42 litres Powerplant: 1 × Lycoming O ...
The wing main spar is a dismountable two-piece carbon fibre beam which joins under the front seat; an auxiliary spar carries the aileron and flap mountings. In plan, the leading edge is elliptical, and there is slight taper on the outer trailing edge where the ailerons are mounted. Single slotted, electrically-operated flaps occupy the rest of ...
The aircraft was a derivative of the 2-22, which in turn was based on the SGU 1-7 single place glider of 1937. The 2-33 retained the 2-22 and 1-7's metal wing, single spar and single strut arrangement. [1] [2] [5] The 2-33 was manufactured in three variants and remained in production for 14 years.
The F11 features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit that is 40 in (102 cm) wide, fixed conventional landing gear, or optionally tricycle landing gear, and a single engine in tractor configuration. [1] The aircraft is made from wood, with its flying surfaces covered in doped aircraft fabric.
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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