Youtor
Air France Flight 4590 Crash Footage
>> YOUR LINK HERE: ___ http://youtube.com/watch?v=8JhFhg9tmIA
Follow us on Instagram: https://www.instagram.com/aircrashdai... • Accident Description: https://www.instagram.com/p/CgbrC-zhv... • ๐๐ถ๐ฟ ๐๐ฟ๐ฎ๐ป๐ฐ๐ฒ ๐๐น๐ถ๐ด๐ต๐ ๐ฐ๐ฑ๐ต๐ฌ was an international charter flight from Paris to New York, operated by a Aérospatiale-BAC Concorde (Reg. F-BTSC) on ๐๐๐น๐ ๐ฎ๐ฑ, ๐ฎ๐ฌ๐ฌ๐ฌ. • At 14:42:17 the crew were cleared for takeoff. At 14:42:54.6, the co-pilot called 100 knots, then V1 nine seconds later. A few seconds after that, tyre no. 2 (right front) on the left main landing gear was destroyed after having run over a strip of metal lost by a Continental Airlines DC-10 (Reg. N13067) which departed Flight 055 to Newark 5 minutes before. The destruction of the tyre in all probability resulted in large pieces of rubber being thrown against the underside of the left wing and the rupture of a part of tank 5. A severe fire broke out under the left wing and around the same time engines 1 and 2 suffered a loss of thrust, severe for no. 2 and slight no. 1. • By 14:43:13, as the captain commenced the rotation, the controller informed the crew the presence of flames behind the plane. Nine seconds later the engine fire alarm sounded and the flight engineer announced shut down engine 2 then the captain called for the engine fire procedure. A few seconds later, the engine 2 fire handle was pulled and the fire alarm stopped. At 14:43:30, the captain called for landing gear retraction. Three seconds later, the GPWS alarm sounded several times. Then the no. 1 engine lost power as well. The plane entered a left turn until control was lost, crashing into hotel 'Hotellisimo' and bursting into flames. • ๐ฃ๐ฟ๐ผ๐ฏ๐ฎ๐ฏ๐น๐ฒ ๐๐ฎ๐๐๐ฒ๐: • The accident was due to the following causes: • • High-speed passage of a tyre over a part lost by an aircraft that had taken off five minutes earlier and the destruction of the tyre. • • The ripping out of a large piece of tank in a complex process of transmission of the energy produced by the impact of a piece of tyre at another point on the tank, this transmission associating deformation of the tank skin and the movement of the fuel, with perhaps the contributory effect of other more minor shocks and /or a hydrodynamic pressure surge. • • Ignition of the leaking fuel by an electric arc in the landing gear bay or through contact with the hot parts of the engine with forward propagation of the flame causing a very large fire under the aircraft's wing and severe loss of thrust on engine 2 then engine 1. • In addition, the impossibility of retracting the landing gear probably contributed to the retention and stabilisation of the flame throughout the flight.
#############################
