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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 Lockheed Martin/Boeing F-22 Raptor is an American twin-engine, all-weather, supersonic stealth fighter aircraft.As a product of the United States Air Force's Advanced Tactical Fighter (ATF) program, the aircraft was designed as an air superiority fighter, but also incorporates ground attack, electronic warfare, and signals intelligence capabilities.
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.
A McDonnell Douglas F-15E Strike Eagle fitted with conformal fuel tanks under the wing roots Ground crew handling the CFT of an F-15E. Conformal fuel tanks (CFTs) are additional fuel tanks fitted closely to the profile of an aircraft that extend the endurance of the aircraft.
With the originally specified 82 lb (37 kg) Briggs & Stratton 401417, four-stroke, 656 cc, 16 hp (12 kW) lawn mower powerplant the aircraft has an empty weight of 230 lb (104 kg). The engine burns only 1 US gal (4 L) per hour giving an endurance of 5 hours on the specified 5 US gal (19 L) of fuel, hence the aircraft's name. [3]
Sargent Fletcher was founded as Fletcher Aviation in 1940 [2] and bought by Cobham in 1994.. According to a 1991 report the company submitted to regional air quality officials, the company's El Monte chrome-plating plant showed the highest cancer-risk level of any business in the San Gabriel Valley. [3]
Data from Sport Aviation General characteristics Capacity: 1 Wingspan: 25 ft 2 in (7.67 m) Empty weight: 254 lb (115 kg) Gross weight: 550 lb (249 kg) Fuel capacity: 5 US gallons (19 L; 4.2 imp gal) Ballistic parachute: Second Chantz system Powerplant: 1 × Compact Radial MZ-201 two stroke, 45 hp (34 kW) Propellers: 2-bladed Performance Cruise speed: 48 kn (55 mph, 89 km/h) Stall speed: 24 kn ...
The aircraft is built around a central bent aluminum keel tube that runs from the cockpit to the tail. Controls are standard three-axis type. Standard engines available are the 50 hp (37 kW) Rotax 503 and 64 hp (48 kW) Rotax 582 two-stroke powerplants. The fuel tank is of plastic construction, mounted under the pusher engine.
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