Crew and passengers
Flight 781 was commanded by Captain Alan Gibson DFC, age 31, one of BOAC's youngest pilots. He had joined BOAC in 1946, after flying in theFlight and accident
Gerry Bull, a former BOAC engineer, said that when he performed a preflight inspection of the aircraft in Rome he looked for "incidental damage", and as he did not find any, he believed the Comet was fit for flight. Bull and the same team of engineers later examined South African Airways Flight 201 before its final flight."Comet Air Crash" ("Crash of the Comet"). '' Seconds From Disaster''. Flight 781 departed from Rome at 10:31Search and recovery
On 11 January 1954, ''Initial findings and reaction
To find more evidence concerning the cause of the crash, the bodies were brought to the coroner for post-mortem. During the examination, pathologist Antonio Fornari found broken and damaged limbs, which had apparently occurred ''after death''. He also discovered in most of the victims a distinct pattern of injuries, consisting of fractured skulls and ruptured and otherwise damaged lungs, which he identified as the actual ''cause of death''. Fornari was confused by the pattern of injuries because he could find no evidence of an explosion. The ruptured lungs were a sure indicator that the air cabin had depressurised, because the sudden decrease in pressure would have caused the lungs to expand until they ruptured. To support this theory, and also to confirm the cause of the skull fractures, the crash was simulated at the RAE in Farnborough by reproducing the conditions of the actual plane prior to the crash. To make this possible, a model fuselage was constructed that was similar to that of the Comet. Dummies were seated within the fuselage to replicate the possible movements of the passengers during the crash. In order to simulate the crash, the investigators deliberately ruptured the model fuselage by increasing the air pressure inside until it exploded. The movement of the dummies within the air cabin revealed the cause of the skull fractures: at the moment that the fuselage exploded, they were thrown out of their seats and slammed head-first into the ceiling. Upon examination of the aircraft wreckage by the RAE, it became evident that the aircraft had broken up in mid-air, and there was initially some speculation that the aircraft might have been brought down by a bomb. Suspicion then shifted to the possibility of an engineOriginal investigation
Initial examination and reconstruction of the wreckage of G-ALYP revealed several signs of inflight break-up: *Shreds of cabin carpet were found trapped in the remains of the Comet's tail section *The imprint of a coin was found on a fuselage panel from the rear of the aircraft *Smears and scoring on the rear fuselage were tested and found to be consistent to the paint applied to the passenger seats of the Comet With most of the wreckage recovered, investigators found that fractures started in the roof of the cabin, a window then smashed into the elevators, the rear fuselage then tore away, the outer wing structure fell, then the outer wing tips and finally the cockpit broke away and fuel from the wings set the debris on fire. To find out what caused the first failure, BOAC donated G-ALYU ("Yoke Uncle") for testing. The airframe was put in a large water tank, the tank was filled, and water was pumped into the plane to simulate flight conditions. The experiment was run 24 hours per day, 7 days per week. It could possibly have taken as long as five months. Official findings concerning BOAC Flight 781 and South African Airways Flight 201 were released jointly on 1 February 1955, in ''Civil Aircraft Accident: Report of the Court of Inquiry into the Accidents to Comet G-ALYP on 10 January 1954 and Comet G-ALYY on 8 April 1954''. After the equivalent of 3,000 flights simulated with G-ALYU, investigators at the RAE were able to conclude that the crash of G-ALYP had been due to failure of the pressure cabin at the forward ADF window in the roof. This window was one of two apertures for the aerials of an electronic navigation system in which opaqueEffects of the disaster and findings
The Comet's pressure cabin had been designed to a safety factor comfortably in excess of that required by British Civil Airworthiness Requirements (BCAR)—the requirement was 1.33 times ''P'' with an ultimate load of 2 times ''P'' (where ''P'' is the cabin's "Proof" pressure), but the safety factor used in the Comet was 2.5 times ''P''—hence the accident led to revised estimates for the safe loading strength requirements of airliner pressure cabins. In addition, it was discovered that the stresses around pressure cabin apertures were considerably higher than had been anticipated, particularly around sharp-cornered cut-outs, such asMemorial
There is a memorial in the cemetery ofIn popular culture
This accident was featured onSee also
*References
Publications
* Official Report (1955)Further reading
External links
* The official AI