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  2. Airbus A330 MRTT - Wikipedia

    en.wikipedia.org/wiki/Airbus_A330_MRTT

    The A330 MRTT has a maximum fuel capacity of 111,000 kg (245,000 lb) without the use of additional fuel tanks, leaving space for 45,000 kg (99,000 lb) of additional cargo. The A330 MRTT's wing has common structure with the four-engine A340-200/-300 with reinforced mounting locations and provision for fuel piping for the A340's outboard engines.

  3. Lituanica - Wikipedia

    en.wikipedia.org/wiki/Lituanica

    New elongated wings were built, with two additional gasoline tanks installed in the fuselage, having 220 US gal (830 L) and 185 US gal (700 L) capacity, each equipped with emergency dump valves. Beneath the pilot's seat a 25 US gal (95 L) oil tank was outfitted with 12 cooling tubes. A longer horizontal stabilizer was built.

  4. Airbus A330 - Wikipedia

    en.wikipedia.org/wiki/Airbus_A330

    It was named A330-300HGW and had a takeoff weight of 240 tonnes (530,000 lb), 7 tonnes (15,000 lb) greater than the -300's weight at the time. The version would have a strengthened wing and additional fuel capacity from a 41,600-litre (11,000 US gal) centre section fuel tank.

  5. Caudron C.860 - Wikipedia

    en.wikipedia.org/wiki/Caudron_C.860

    Together with four smaller wing tanks, these gave a fuel capacity of 1,500 L (330 imp gal; 400 US gal). The pilot had an enclosed cockpit with his head raised only slightly above the fuselage under a shallow canopy with a horizontal strip of plexiglas for forwards and sideways vision, a solid top and an extended fairing aft. There were also ...

  6. Airbus A330neo - Wikipedia

    en.wikipedia.org/wiki/Airbus_A330neo

    The Airbus A330neo ("neo" for "New Engine Option") is a wide-body airliner developed by Airbus from the original Airbus A330 (now A330ceo – "Current Engine Option"). [4] A new version with modern engines comparable with those developed for the Boeing 787 was called for by operators of the A330ceo.

  7. Cessna 182 Skylane - Wikipedia

    en.wikipedia.org/wiki/Cessna_182_Skylane

    The 1978 model year introduced a new 28V electrical system, molded plastic control wheels, and an avionics master switch. 1979 saw the replacement of the fuel bladders with a 88 US gal (330 L) wet wing as well as the introduction of a redesigned brake master cylinder and an alternator control unit (ACU). 1980 introduced a redesigned audio panel ...

  8. Fuel bladder - Wikipedia

    en.wikipedia.org/wiki/Fuel_bladder

    Standard fuel bladder tanks sizes range from 100-US-gallon (380 L) to 200,000-US-gallon (760,000 L) capacities and larger. Custom fuel storage bladders and cells are available, although at sizes exceeding 50,000 US gallons (190,000 L) there is an increased spill risk.

  9. Architecture of the oil tanker - Wikipedia

    en.wikipedia.org/wiki/Architecture_of_the_oil_tanker

    An oil tanker's inert gas system is one of the most important parts of its design. [18] Fuel oil itself is very difficult to ignite, however its hydrocarbon vapors are explosive when mixed with air in certain concentrations. [19] The purpose of the system is to create an atmosphere inside tanks in which the hydrocarbon oil vapors cannot burn. [18]