BOAC Flight 781

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BOAC Flight 781
Summary
Date  10 January 1954
Type  In-flight metal fatigue failure
Site  Mediterranean off Elba
Fatalities  35
Injuries  0
Aircraft
 Aircraft type  de Havilland DH-106 Comet 1
Operator  British Overseas Airways Corporation
Tail number  G-ALYP
Passengers  29
Crew  6
Survivors  0

On 10 January 1954, BOAC Flight 781 a de Havilland Comet 1 (type DH-106), took off from Ciampino Airport in Rome, Italy en route to Heathrow Airport in London, England on the final leg of its flight from Singapore. At about 10:00 GMT, the aircraft suffered an explosive decompression at altitude and crashed into the Mediterranean Sea, killing everyone on board.

The flight was operated by British Overseas Airways Corporation (BOAC) using the aircraft G-ALYP ("Yoke Peter").

Contents

[edit] Flight and disaster

On 10 January 1954, the flight took off at 09:34 GMT for the final stage flight to London.

At about 09:50 GMT a passing BOAC Argonaut G-ALHJ was in contact with Yoke Peter's Captain, Alan Gibson. During a radio communication about weather conditions,the conversation was abruptly cut-off. The last words heard from Captain Gibson were "George How Jig, did you get my..". At about this time wreckage was seen falling into the sea by a fisherman.

[edit] Search, recovery and investigation

The de Havilland DH-106 Comet 1 G-ALYP ("Yoke-Peter").
The de Havilland DH-106 Comet 1 G-ALYP ("Yoke-Peter").

An extensive search for the aircraft was organised including the Royal Navy ship HMS Barhill and the civilian salvage vessel Sea Salvor from Malta.

Wreckage of the aircraft was eventually found on the sea floor and subsequently raised and transported to the Royal Aircraft Establishment, Farnborough, for investigation. Upon examination of the wreckage it became obvious that the aircraft had broken up in mid-air, and initially it was thought that the aircraft might have been brought down by a bomb. Suspicion then shifted to the possibility of an engine turbine explosion and modifications were put in hand to encase the turbine ring in other Comets with armour plate, to contain a possible disintegrating turbine disk. In the meantime, all Comets were to be grounded until these modifications had been carried out. The possibility of failure of the pressure cabin had been considered but then discounted due to the Comet's cabin having been designed to a considerably higher strength than was considered necessary at the time.

[edit] Metal fatigue

The recovered (shaded) parts of the wreckage of G-ALYP and the site (arrowed) of the failure.
The recovered (shaded) parts of the wreckage of G-ALYP and the site (arrowed) of the failure.

Initial examination and reconstruction of the wrecakge 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

After extensive testing of the Comet 1 G-ALYU ("Yoke Uncle") which had been donated for testing by BOAC, investigators at the RAE concluded that the crash had been due to failure of the pressure cabin at the forward ADF window in the roof - this 'window' was in fact one of two apertures for the aerials of an electronic navigation system, opaque fibreglass panels taking the place of the window 'glass' - as a result of metal fatigue caused by the repeated pressurisation and de-pressurisation of the aircraft cabin.

The Comet's pressure cabin had been designed to a safety factor comfortably in excess of that required by British Civil Airworthiness Requirements (2.5x P as opposed to the requirement of 1.33x P and an ultimate load of 2x P, P being the cabin 'Proof' pressure) and the accident caused a revision in the estimates of 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 appreciated, especially around sharp-cornered cut-outs, such as windows. As a result, future jet airliners would feature windows with rounded corners, the curve eliminating a stress concentration. This was a noticeable distinguishing feature of all later marks of the Comet.

[edit] Trivia

  • An episode of Seconds from Disaster, "Crash of the Comet," focused on this and several other Comet crashes.
  • One of the crash victims was Chester Wilmot, a noted Australian radio personality

[edit] See also

[edit] References

  • Air Disasters by Stanley Stewart - Arrow Books (UK) 1986/89 - ISBN 0-09-956200-6
  • Report of the Public Inquiry into the causes and circumstances of the accident which occurred on the 10th January, 1954, to the Comet aircraft G‐ALYP - Official Report - 1955
  • "Seconds From Disaster" " Crash of the Comet" on National Geographic Channel.


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