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  2. Fuselage - Wikipedia

    en.wikipedia.org/wiki/Fuselage

    The fuselage (/ ˈ f juː z əl ɑː ʒ /; from the French fuselé "spindle-shaped") is an aircraft's main body section. It holds crew , passengers, or cargo . In single-engine aircraft, it will usually contain an engine as well, although in some amphibious aircraft the single engine is mounted on a pylon attached to the fuselage, which in turn ...

  3. Aircraft fuel system - Wikipedia

    en.wikipedia.org/wiki/Aircraft_fuel_system

    Single-engine light aircraft fuel tanks are usually in the wings, but some aircraft have a small "header tank" between the normal fuel tank and the engine, to facilitate reliable fuel flow to the engine. On many small or very old single-engine header tanks (and even main tanks) are often mounted above and/or immediately behind the engine. A few ...

  4. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    Diagram of a typical gas turbine jet engine. Air is compressed by the compressor blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor blades. 1. Intake 2. Low pressure compression 3. High pressure compression ...

  5. Sikorsky S-61 - Wikipedia

    en.wikipedia.org/wiki/Sikorsky_S-61

    The fuselage is shortened by 50 in (1.3 m) to increase its single-engine performance and external payload. [7] The improved lift performance lent itself to utility operations, particularly in the construction market. [8] A unique version is the S-61 Shortsky, a conversion of S-61Ls and S-61Ns performed by Helipro International. [1]

  6. Cirrus VK-30 - Wikipedia

    en.wikipedia.org/wiki/Cirrus_VK-30

    The VK-30 was the predecessor of the Cirrus ST50, which had an almost-identical configuration to the VK-30, but included a larger ventral fin on the tail of the aircraft, a slightly larger fuselage, and was powered by a Pratt & Whitney Canada PT6-135 turboprop engine in place of the piston engine used in the VK-30.

  7. Taylorcraft B - Wikipedia

    en.wikipedia.org/wiki/Taylorcraft_B

    Data from Plane and Pilot General characteristics Crew: one Capacity: one passenger Empty weight: 860 lb (390 kg) Gross weight: 1,500 lb (680 kg) Fuel capacity: 18 U.S. gallons (68 L; 15 imp gal) Powerplant: 1 × Continental C-85 four-cylinder horizontally opposed aircraft engine, 85 hp (63 kW) Propellers: 2-bladed metal Performance Maximum speed: 120 mph (190 km/h, 100 kn) Cruise speed: 110 ...

  8. Narrow-body aircraft - Wikipedia

    en.wikipedia.org/wiki/Narrow-body_aircraft

    A narrow-body aircraft or single-aisle aircraft is an airliner arranged along a single aisle, permitting up to 6-abreast seating in a cabin less than 4 metres (13 ft) in width. In contrast, a wide-body aircraft is a larger airliner usually configured with multiple aisles and a fuselage diameter of more than 5 metres (16 ft), allowing at least ...

  9. Fixed-wing aircraft - Wikipedia

    en.wikipedia.org/wiki/Fixed-wing_aircraft

    The fuselage is typically long and thin, usually with tapered or rounded ends to make its shape aerodynamically smooth. Most fixed-wing aircraft have a single fuselage. Others may have multiple fuselages, or the fuselage may be fitted with booms on either side of the tail to allow the extreme rear of the fuselage to be utilized.