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Fuel capacity: 2 x 212 L (56 US gal; 47 imp gal) outer wing tanks + 2x 312 L (82 US gal; 69 imp gal) tip-tanks + 1x 118 L (31 US gal; 26 imp gal) fuselage collector-tank Auxiliary fuel system: 1 x 236 L (62 US gal; 52 imp gal) optional fuselage tank, with provision for 2x 177 L (47 US gal; 39 imp gal) or 284 L (75 US gal; 62 imp gal) under-wing ...
In 2012, Air Combat Command requested the testing of a 600-US-gallon (2,300 L; 500 imp gal) external fuel tank which would extend the A-10's loitering time by 45–60 minutes; flight testing of such a tank had been conducted in 1997 but did not involve combat evaluation.
A 2,300-litre (600 US gal) Sargent Fletcher drop tank being moved across the flight deck of an aircraft carrier Bangladesh Air Force Chengdu F-7 carries a drop tank at under-fuselage hardpoint. In aviation, a drop tank (external tank, wing tank or belly tank) is used to describe auxiliary fuel tanks externally carried by aircraft. A drop tank ...
The Cessna A-37 Dragonfly, or Super Tweet, is a light attack aircraft designed and produced by the American aircraft manufacturer Cessna.. It was developed during the Vietnam War in response to military interest in new counter-insurgency (COIN) aircraft to replace aging types such as the Douglas A-1 Skyraider.
Aircraft fuel tanks are a major component of aircraft fuel systems. They can be classified into internal or external fuel tanks and can be further classified by method of construction or intended use. Safety aspects of aircraft fuel tanks were examined during the investigation of the 1996 TWA Flight 800 in-flight explosion accident.
In late 1948, Cessna began sales of the 170, with a metal fuselage and tail and fabric-covered constant-chord wings. These earliest 170s were four-seat versions of the popular 140 with a more powerful 145 hp (108 kW) Continental C145-2 and an extra interconnected fuel tank in one wing for a total of 36 gallons in three tanks. Like the 140, they ...
Cessna XL-19C Bird Dog. The U.S. Army was searching for an aircraft that could fly over enemy locations to collect information related to artillery fire target locations and distances, as well as perform liaison duties, and preferably be constructed of all metal, as the fabric-covered liaison aircraft used during World War II (primarily Stinson and Piper products) had short service lives.
The MD-83 features increased fuel capacity as standard (to 6,970 US gal (26,400 L)), which is carried in two 565 US gal (2,140 L) auxiliary tanks located fore and aft of the center section. The aircraft also has higher operating weights, with MTOW increased to 160,000 lb (73,000 kg) and MLW to 139,500 lb (63,300 kg).
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