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British European Airways Flight 706

British European Airways Flight 706 (BE706/BEA706) was a scheduled international passenger flight from United Kingdom to Salzburg, Austria. On 2 October 1971, whilst en route at 19,000 feet (5,791 m),[1] the Vickers Vanguard suffered a failure with its rear cabin pressure bulkhead. The resulting depressurisation of the tail section caused the surfaces of the tailplanes to separate. The aircraft entered an uncontrollable dive and crashed near Aarsele, Belgium, killing all 63 passengers and crew on impact.[2] A piece of debris from the aircraft struck a passing car, causing minor injuries to one of its occupants.

BEA Flight 706
G-APEC, the aircraft involved in the accident, a few weeks prior
Accident
Date2 October 1971 (1971-10-02)
SummaryExplosive decompression, leading to structural failure and loss of control
SiteAarsele, Belgium
Aircraft
Aircraft typeVickers Vanguard
OperatorBritish European Airways
RegistrationG-APEC
Flight originHeathrow Airport, London, UK
DestinationSalzburg Airport, Austria
Occupants63
Passengers55
Crew8
Fatalities63
Survivors0
Ground casualties
Ground injuries1

United Kingdom AAIB concluded that the failure of the rear pressure bulkhead had been caused by undetected corrosion located at the rear of the aircraft.[3] The corrosion couldn't be noticed by crew due to the inspection technique that had been applied by BEA. Numerous pressurization cycles caused the crack to grow, weakening the rear pressure bulkhead until the structure was unable to withstand further repeated stress.[4]

Aircraft

The aircraft involved in the crash was a Vickers Vanguard type 951, registered in United Kingdom as G-APEC. The aircraft was built in 1959 with a serial number of 706. It was delivered to BEA in 1961.[5]

Flight

Flight 706 took off from Runway 28L (now 27L) of London Heathrow Airport at 09:34 local time with 55 passengers and 8 crew members.[5] After take off, Flight 706 was routed via Epsom, Biggin and Detling in accordance to the "Dover One" standard instrument departure clearance. The crew of Flight 706 later reported over the Dover VOR at 09:54 local time. At the time, Flight 706 was climbing through 14,200 feet (4,328 m). At 10:01, the communication was handed over to Brussels Air Traffic Control.[6]

  • 10:01 BEA706: "Goodmorning Brussels Bealine seven oh six is passing one eight for one nine zero and estimating Wulpen at zero hour"
  • 10:01 ATC: "Seven oh six cleared er Salzburg green one to maintain flight level one nine zero on reaching "
  • 10:01 BEA706: "Bealine seven oh six"

The crew then reported passing over the Wulpen VOR with the aircraft level at FL190 (about 19,000 feet (5,791 m).[5]

  • 10:05 BEA706: "Brussels Bealine seven oh six checked Wulpen zero four we're now level one nine zero estimating Mackel one zero"
  • 10:05 ATC: "Seven oh six roger"

Five minutes after this transmission, the crew of Flight 706 transmitted "we're going down, seven oh six, we are going down" to Brussels Tower. The crew later declared emergency and called "mayday, mayday" several times. The crew also stated the phrase "out of control" several times. At one point, they stated that there was no rudder control. Their calls were accompanied by several background voices.[5][6]

  • 10:09:46 BEA706: "We're going down, seven oh six, we're going down Mayday Mayday Mayday"
  • 10:09 BEA706: "Mayday Mayday Mayday we're going down vertically"
  • 10:09:55 BEA706: "Bealine seven zero six (inaudible) out of control"
  • 10:09:58 BEA706: "No rudder-- (inaudible)"
  • 10:10:11 BEA706: "AAH! This is it--"

The last transmission from Flight 706 was recorded at 10:10:30. Brussels Tower immediately attempted contacting Flight 706 several times. However, there were no answers from Flight 706.[5] Witnesses on the ground saw the tailplane of Flight 706 detached and subsequently Flight 706 entered a nose-dive. The flight kept diving and crashed into farm land near Aarsele, Belgium and exploded on impact. All 55 passengers and 8 crew members were killed. At least one person on the ground was injured after pieces of the debris struck a passing car.[5]

Rescue services were immediately dispatched. Investigators were deployed and immediately searched the aircraft's black box. A crisis center was set up in Salzburg for the relatives of the victims of Flight 706. Searchers stated that most of the bodies were not intact. One searcher said "as for the bodies, what we have found so far is barely enough to reconstitute one body."[7]

Passengers and crews

The aircraft was carrying 55 passengers and 8 crew members. News report stated that there were 37 British passengers on board the aircraft. At least 4 Japanese and 11 Americans were also on board the aircraft. Further reports also confirmed the presence of 8 Austrians on board the flight.[8][9] Two notable fatalities among the passengers were the British hat designer Otto Lucas and an Austrian academic, René Marcic [de].[10]

The Captain was identified as 40 year old Captain E.T Probert. At the time of the accident, he had accumulated a total flying hours of 9,260 hours, in which 1,927 hours were on the type. The co-pilot was 38 year old J.M Davies, who held a Vickers Vanguard rating. He had a total flying hours of 3,386 hours, in which 764 hours were on the type. The aircraft was also carrying a third pilot, identified as 27 year old B.J.S Barnes with a total flying hours of 2,237 hours, in which 1,903 hours were on the type and a supernumerary, identified as Captain G. Partridge.[5]

Investigation

Witnesses on the ground recalled that the Vanguard suddenly exploded in mid-air, lost one of its wings, and plunged onto the ground, with smoke pouring out from one of its wings. They stated that they heard strange noises during the crash. According to them, the aircraft touched down in one field, jumped a road, and plowed through grassland for 500 yards (1,500 ft; 460 m). It gouged into the ground and burst into flames in a pit 15 feet (4.6 m) deep. One of the witness stated, "The fire spread from the wreckage like waves." Police said eyewitness reports indicated that Captain Probert had tried to execute an emergency landing.[8]

There was considerable suspicion that the aircraft had been sabotaged by extremists. A BEA spokesman claimed that the aircraft was sabotaged by Northern Ireland extremists. The Vanguard had been used on the LondonBelfast route, though he said the aircraft had not been on Belfast service for at least 48 hours and was stored in Edinburgh on Friday. However, after a preliminary investigation by William Trench, one of the investigators from AIB, stated that at the time there was no hint that sabotage played a part in the crash.[10]

Structural failure

Observation of the aircraft's wreckage revealed that about two thirds of the tail and the left elevator had already detached from the aircraft prior to its impact with the ground, indicating a structural breakup. These parts were found trailing before the crash site and major portions of the parts were recovered several kilometres away from the main wreckage area. By taking the prevailing wind drift into account, the result of the drift plot indicated that the components had separated from the aircraft at a height of approximately 18,000 feet (5,500 m). The hypothesis was also supported by recordings from the flight recorder and the transcript of conversation between the flight crew and the controller in Brussels. The flight data recorder was abruptly cut off while the aircraft was flying on cruising altitude, while in the ATC recording the crew could be heard stating that they were going down vertically with no rudder control.[5][6]

The examination on the recovered parts revealed that both the left and right horizontal stabilizer and the elevator had detached in a near similar manner. The nature of the separation sparked strong suspicion that the separation had been caused from the inside of the aircraft rather than from external environment. The upper skin of the tail had been blown outwards, strongly suggesting that difference in internal pressure from the aircraft had caused the separation of the components.[5]

Reconstruction on the aircraft wreckage indicated that the rear pressure bulkhead had suffered a corrosion at the lower part of the bulkhead. Beneath the double curvature peripheral doubler plate, the bulkhead material had corroded and the bond between materials had decreased. At the end of each corroded area, a tear could be seen spreading upwards and outwards to a rivet line which was located at the lower edge of the bulkhead. The tear on the left side was particularly noted for the "step" marks. The marks ran for at least 60 centimetres (24 in) and the distance of each "steps" progressively increased.[5]

A simulation with similar scenario was conducted by AAIB. An UV tracer was used in the simulation to show the movement of the tear. The right horizontal stabilizer was taken from another aircraft of similar age and flying time with the involved aircraft. Differential pressure was introduced during the simulation. During the test, the bulkhead failed, creating a burst of force that blew the skin of the tail outwards. The force was violent enough that a rivet line managed to blow through the skin of the elevator hinge. The right horizontal stabilizer and the elevator were severely damaged by the explosion. Comparison between the pattern that had been created by the explosion in the simulation showed that the pattern was similar with the pattern that was found in the wreckage.[5]

The result clearly showed that corrosion within the rear pressure bulkhead had caused the component to fail inflight, resulting in an explosion that caused the rapid separation of the horizontal stabilizers and the vertical stabilizer. The loss of the aircraft parts caused the aerodynamic forces to be compromised, causing the crew to lose control of the aircraft.[5]

Cause of failure

From the extent and severity of the corrosion, it was deemed likely that the corrosion had taken a long period of time to develop, although investigators could not determine on how much time that was needed for such corrosion to develop. Due to the radiographic technique that had been applied by BEA, the crack on the aircraft couldn't be detected in a timely manner as the radiographic data could not be properly interpreted. Eventually, the crack continued to grow due to repeated pressurization until it became visible from the outside. This was corroborated by evidence of nicotine stain and signs of spilt sewage around the corroded area.[5]

Though the cracks were visible from the outside, the aircraft visual inspection was not regularly conducted by staffs. The inspection was instead conducted at long intervals, causing the corrosion attack to intensify. After numerous times of flying, a considerable amount of sewage fluid had been retained on the corroded area, creating visible stain. The area with the stain was always cleaned before an inspection. This practice caused the aircraft inspector to not notice on corrosion and possible fluid leakage in the area.[5]

Conclusion

Investigators finally concluded the cause of the accident, and stated,[5]

"The accident was caused by the rupture of the rear pressure bulkhead, which led to the separation of both tailplanes in flight and in turn caused the aircraft to dive into the ground,"

Aftermath

British European Airways immediately implemented a new technique in detecting corrosion. It was later revealed that eight Vanguards of their fleets suffered the same crack as G-APEC.[5]

After the release of the final report, a new technique to detect corrosion and crack was introduced by AAIB. They also ordered a modification to provide better access for ground engineers into difficult to reach areas within the aircraft.[5]

See also

References

  1. ^ "BEA Vanguard Lost." Flight International. 7 October 1971. p. 557.
  2. ^ "63 persons are killed in fiery air accident". Star-News. Vol. 42, no. 5. United Press International. 3 October 1971. pp. 1A. Retrieved 19 May 2014 – via Google News.
  3. ^ Aviation Safety Network Aircraft accident Vickers 951 Vanguard G-APEC Aarsele
  4. ^ "Vanguard Report Issued." Flight International. 11 January 1973. p. 51
  5. ^ a b c d e f g h i j k l m n o p q "British European Airways Vanguard G-APEC. Report on the accident which occurred at Aarsele, Belgium on 2 October 1971" (PDF). The Kingdom of Belgium Ministry of Communications, Civil Aeronautics Administration.
  6. ^ a b c "Final Report of G-APEC (Appendixes)" (PDF). The Kingdom of Belgium Ministry of Communications, Civil Aeronautics Administration.
  7. ^ "Desert Sun, Number 51, 2 October 1971". Desert Sun.
  8. ^ a b "All 63 on British Airliner Killed in Crash in Belgium". The New York Times. 3 October 1971. ISSN 0362-4331.
  9. ^ "1971, News: British European Airways Flight 706 crashes near Aarsele, Belgium". 31 October 2014.
  10. ^ a b "Tail pieces found 3 miles from Belgium air crash". Bangor Daily News. UPI. 4 October 1971. Retrieved 22 September 2014.

External links

  • British European Airways Vanguard G—APEC. Report on the accident which occurred at Aarsele, Belgium on 2 October 1971" (). The Kingdom of Belgium Ministry of Communications, Civil Aeronautics Administration. Re-published by the Accidents Investigation Branch, Department of Trade and Industry as Civil Accident Report No EW/A224, Report 15/72. – Official accident report.
    • Appendices ()
  • Video of the crash site, Associated Press

50°59′27″N 3°26′20″E / 50.99083°N 3.43889°E / 50.99083; 3.43889

british, european, airways, flight, be706, bea706, scheduled, international, passenger, flight, from, united, kingdom, salzburg, austria, october, 1971, whilst, route, feet, vickers, vanguard, suffered, failure, with, rear, cabin, pressure, bulkhead, resulting. British European Airways Flight 706 BE706 BEA706 was a scheduled international passenger flight from United Kingdom to Salzburg Austria On 2 October 1971 whilst en route at 19 000 feet 5 791 m 1 the Vickers Vanguard suffered a failure with its rear cabin pressure bulkhead The resulting depressurisation of the tail section caused the surfaces of the tailplanes to separate The aircraft entered an uncontrollable dive and crashed near Aarsele Belgium killing all 63 passengers and crew on impact 2 A piece of debris from the aircraft struck a passing car causing minor injuries to one of its occupants BEA Flight 706G APEC the aircraft involved in the accident a few weeks priorAccidentDate2 October 1971 1971 10 02 SummaryExplosive decompression leading to structural failure and loss of controlSiteAarsele BelgiumAircraftAircraft typeVickers VanguardOperatorBritish European AirwaysRegistrationG APECFlight originHeathrow Airport London UKDestinationSalzburg Airport AustriaOccupants63Passengers55Crew8Fatalities63Survivors0Ground casualtiesGround injuries1United Kingdom AAIB concluded that the failure of the rear pressure bulkhead had been caused by undetected corrosion located at the rear of the aircraft 3 The corrosion couldn t be noticed by crew due to the inspection technique that had been applied by BEA Numerous pressurization cycles caused the crack to grow weakening the rear pressure bulkhead until the structure was unable to withstand further repeated stress 4 Contents 1 Aircraft 2 Flight 3 Passengers and crews 4 Investigation 4 1 Structural failure 4 2 Cause of failure 4 3 Conclusion 5 Aftermath 6 See also 7 References 8 External linksAircraft EditThe aircraft involved in the crash was a Vickers Vanguard type 951 registered in United Kingdom as G APEC The aircraft was built in 1959 with a serial number of 706 It was delivered to BEA in 1961 5 Flight EditFlight 706 took off from Runway 28L now 27L of London Heathrow Airport at 09 34 local time with 55 passengers and 8 crew members 5 After take off Flight 706 was routed via Epsom Biggin and Detling in accordance to the Dover One standard instrument departure clearance The crew of Flight 706 later reported over the Dover VOR at 09 54 local time At the time Flight 706 was climbing through 14 200 feet 4 328 m At 10 01 the communication was handed over to Brussels Air Traffic Control 6 10 01 BEA706 Goodmorning Brussels Bealine seven oh six is passing one eight for one nine zero and estimating Wulpen at zero hour 10 01 ATC Seven oh six cleared er Salzburg green one to maintain flight level one nine zero on reaching 10 01 BEA706 Bealine seven oh six The crew then reported passing over the Wulpen VOR with the aircraft level at FL190 about 19 000 feet 5 791 m 5 10 05 BEA706 Brussels Bealine seven oh six checked Wulpen zero four we re now level one nine zero estimating Mackel one zero 10 05 ATC Seven oh six roger Five minutes after this transmission the crew of Flight 706 transmitted we re going down seven oh six we are going down to Brussels Tower The crew later declared emergency and called mayday mayday several times The crew also stated the phrase out of control several times At one point they stated that there was no rudder control Their calls were accompanied by several background voices 5 6 10 09 46 BEA706 We re going down seven oh six we re going down Mayday Mayday Mayday 10 09 BEA706 Mayday Mayday Mayday we re going down vertically 10 09 55 BEA706 Bealine seven zero six inaudible out of control 10 09 58 BEA706 No rudder inaudible 10 10 11 BEA706 AAH This is it The last transmission from Flight 706 was recorded at 10 10 30 Brussels Tower immediately attempted contacting Flight 706 several times However there were no answers from Flight 706 5 Witnesses on the ground saw the tailplane of Flight 706 detached and subsequently Flight 706 entered a nose dive The flight kept diving and crashed into farm land near Aarsele Belgium and exploded on impact All 55 passengers and 8 crew members were killed At least one person on the ground was injured after pieces of the debris struck a passing car 5 Rescue services were immediately dispatched Investigators were deployed and immediately searched the aircraft s black box A crisis center was set up in Salzburg for the relatives of the victims of Flight 706 Searchers stated that most of the bodies were not intact One searcher said as for the bodies what we have found so far is barely enough to reconstitute one body 7 Passengers and crews EditThe aircraft was carrying 55 passengers and 8 crew members News report stated that there were 37 British passengers on board the aircraft At least 4 Japanese and 11 Americans were also on board the aircraft Further reports also confirmed the presence of 8 Austrians on board the flight 8 9 Two notable fatalities among the passengers were the British hat designer Otto Lucas and an Austrian academic Rene Marcic de 10 The Captain was identified as 40 year old Captain E T Probert At the time of the accident he had accumulated a total flying hours of 9 260 hours in which 1 927 hours were on the type The co pilot was 38 year old J M Davies who held a Vickers Vanguard rating He had a total flying hours of 3 386 hours in which 764 hours were on the type The aircraft was also carrying a third pilot identified as 27 year old B J S Barnes with a total flying hours of 2 237 hours in which 1 903 hours were on the type and a supernumerary identified as Captain G Partridge 5 Investigation EditWitnesses on the ground recalled that the Vanguard suddenly exploded in mid air lost one of its wings and plunged onto the ground with smoke pouring out from one of its wings They stated that they heard strange noises during the crash According to them the aircraft touched down in one field jumped a road and plowed through grassland for 500 yards 1 500 ft 460 m It gouged into the ground and burst into flames in a pit 15 feet 4 6 m deep One of the witness stated The fire spread from the wreckage like waves Police said eyewitness reports indicated that Captain Probert had tried to execute an emergency landing 8 There was considerable suspicion that the aircraft had been sabotaged by extremists A BEA spokesman claimed that the aircraft was sabotaged by Northern Ireland extremists The Vanguard had been used on the London Belfast route though he said the aircraft had not been on Belfast service for at least 48 hours and was stored in Edinburgh on Friday However after a preliminary investigation by William Trench one of the investigators from AIB stated that at the time there was no hint that sabotage played a part in the crash 10 Structural failure Edit Observation of the aircraft s wreckage revealed that about two thirds of the tail and the left elevator had already detached from the aircraft prior to its impact with the ground indicating a structural breakup These parts were found trailing before the crash site and major portions of the parts were recovered several kilometres away from the main wreckage area By taking the prevailing wind drift into account the result of the drift plot indicated that the components had separated from the aircraft at a height of approximately 18 000 feet 5 500 m The hypothesis was also supported by recordings from the flight recorder and the transcript of conversation between the flight crew and the controller in Brussels The flight data recorder was abruptly cut off while the aircraft was flying on cruising altitude while in the ATC recording the crew could be heard stating that they were going down vertically with no rudder control 5 6 The examination on the recovered parts revealed that both the left and right horizontal stabilizer and the elevator had detached in a near similar manner The nature of the separation sparked strong suspicion that the separation had been caused from the inside of the aircraft rather than from external environment The upper skin of the tail had been blown outwards strongly suggesting that difference in internal pressure from the aircraft had caused the separation of the components 5 Reconstruction on the aircraft wreckage indicated that the rear pressure bulkhead had suffered a corrosion at the lower part of the bulkhead Beneath the double curvature peripheral doubler plate the bulkhead material had corroded and the bond between materials had decreased At the end of each corroded area a tear could be seen spreading upwards and outwards to a rivet line which was located at the lower edge of the bulkhead The tear on the left side was particularly noted for the step marks The marks ran for at least 60 centimetres 24 in and the distance of each steps progressively increased 5 A simulation with similar scenario was conducted by AAIB An UV tracer was used in the simulation to show the movement of the tear The right horizontal stabilizer was taken from another aircraft of similar age and flying time with the involved aircraft Differential pressure was introduced during the simulation During the test the bulkhead failed creating a burst of force that blew the skin of the tail outwards The force was violent enough that a rivet line managed to blow through the skin of the elevator hinge The right horizontal stabilizer and the elevator were severely damaged by the explosion Comparison between the pattern that had been created by the explosion in the simulation showed that the pattern was similar with the pattern that was found in the wreckage 5 The result clearly showed that corrosion within the rear pressure bulkhead had caused the component to fail inflight resulting in an explosion that caused the rapid separation of the horizontal stabilizers and the vertical stabilizer The loss of the aircraft parts caused the aerodynamic forces to be compromised causing the crew to lose control of the aircraft 5 Cause of failure Edit From the extent and severity of the corrosion it was deemed likely that the corrosion had taken a long period of time to develop although investigators could not determine on how much time that was needed for such corrosion to develop Due to the radiographic technique that had been applied by BEA the crack on the aircraft couldn t be detected in a timely manner as the radiographic data could not be properly interpreted Eventually the crack continued to grow due to repeated pressurization until it became visible from the outside This was corroborated by evidence of nicotine stain and signs of spilt sewage around the corroded area 5 Though the cracks were visible from the outside the aircraft visual inspection was not regularly conducted by staffs The inspection was instead conducted at long intervals causing the corrosion attack to intensify After numerous times of flying a considerable amount of sewage fluid had been retained on the corroded area creating visible stain The area with the stain was always cleaned before an inspection This practice caused the aircraft inspector to not notice on corrosion and possible fluid leakage in the area 5 Conclusion Edit Investigators finally concluded the cause of the accident and stated 5 The accident was caused by the rupture of the rear pressure bulkhead which led to the separation of both tailplanes in flight and in turn caused the aircraft to dive into the ground Aftermath EditBritish European Airways immediately implemented a new technique in detecting corrosion It was later revealed that eight Vanguards of their fleets suffered the same crack as G APEC 5 After the release of the final report a new technique to detect corrosion and crack was introduced by AAIB They also ordered a modification to provide better access for ground engineers into difficult to reach areas within the aircraft 5 See also EditChina Airlines Flight 611 Japan Airlines Flight 123References Edit BEA Vanguard Lost Flight International 7 October 1971 p 557 63 persons are killed in fiery air accident Star News Vol 42 no 5 United Press International 3 October 1971 pp 1A Retrieved 19 May 2014 via Google News Aviation Safety Network Aircraft accident Vickers 951 Vanguard G APEC Aarsele Vanguard Report Issued Flight International 11 January 1973 p 51 a b c d e f g h i j k l m n o p q British European Airways Vanguard G APEC Report on the accident which occurred at Aarsele Belgium on 2 October 1971 PDF The Kingdom of Belgium Ministry of Communications Civil Aeronautics Administration a b c Final Report of G APEC Appendixes PDF The Kingdom of Belgium Ministry of Communications Civil Aeronautics Administration Desert Sun Number 51 2 October 1971 Desert Sun a b All 63 on British Airliner Killed in Crash in Belgium The New York Times 3 October 1971 ISSN 0362 4331 1971 News British European Airways Flight 706 crashes near Aarsele Belgium 31 October 2014 a b Tail pieces found 3 miles from Belgium air crash Bangor Daily News UPI 4 October 1971 Retrieved 22 September 2014 External links EditBritish European Airways Vanguard G APEC Report on the accident which occurred at Aarsele Belgium on 2 October 1971 Archive The Kingdom of Belgium Ministry of Communications Civil Aeronautics Administration Re published by the Accidents Investigation Branch Department of Trade and Industry as Civil Accident Report No EW A224 Report 15 72 Official accident report Appendices Archive Video of the crash site Associated Press 50 59 27 N 3 26 20 E 50 99083 N 3 43889 E 50 99083 3 43889 Retrieved from https en wikipedia org w index php title British European Airways Flight 706 amp oldid 1164556794, wikipedia, wiki, book, books, library,

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