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  1. Hace 5 días · Two of these were found to be caused by structural failure resulting from metal fatigue in the airframe, a phenomenon not fully understood at the time; the other was due to overstressing of the airframe during flight through severe weather. The Comet was withdrawn from service and extensively tested.

  2. 2 de may. de 2024 · This was the first of two accidents caused by metal fatigue in the fuselage as a result of expansion and contraction during pressurization cycles. The DH.106 Comet I fleet was grounded and the aircraft were removed from service.

  3. 2 de may. de 2024 · This was the first of two accidents caused by metal fatigue in the fuselage as a result of expansion and contraction during pressurization cycles. The DH.106 Comet I fleet was grounded and the aircraft were removed from service. De Havilland Comet 1 G-AYLP (www.crash-aerien.news) © 2019, Bryan R. Swopes

  4. cienciatecnologiafoco.blogspot.com › 2024 › 05DE HAVILLAND DH.106 COMET IV

    Hace 6 días · O de Havilland DH.106 Comet foi uma antiga aeronave comercial quadrimotor de médio porte, com motorização turbojato, com capacidade para transportar entre 36 e 81 passageiros, dependendo da versão e da configuração de assentos adotada, em viagens internacionais e intercontinentais, projetada e desenvolvida durante a década de 1940 e fabricada em...

  5. 2 de may. de 2024 · Extensive testing by the Royal Aircraft Establishment determined that the Comet’s pressurized fuselage could be expected to fail from metal fatigue after 1,000 pressurization/depressurization cycles.

  6. Hace 4 días · Technical information that for any modern aircraft is relatively easy to find has been incredibly difficult to locate for the Comet. Very few aircraft were ever made and very few sets of manuals were printed.

  7. 26 de abr. de 2024 · The Comet faced significant technical hazards mostly due to design errors linked to metal fatigue and pressurization, resulting in severe structural failures. De Havilland had financial concerns because of the substantial expenses involved in research, development, and manufacture.