List of aircraft structural failures
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File:F-89 Scorpion Crash IAE Detroit 1952.jpg wing failure during flypast.]]
The list of aircraft accidents and incidents caused by structural failures summarizes notable accidents and incidents such as the 1933 United Airlines Chesterton Crash due to a bombing and a 1964 B-52 test that landed after the vertical stabilizer broke off. Loss of structural integrity during flight can be caused by:
- faulty design
- faulty maintenance
- manufacturing flaws
- pilot error
- weather conditions
- sabotage (e.g., an airliner bombing or takeover by a skyjacker).
{{Inc-transport|date=November 2008}}
class="wikitable sortable"
|+ List of aircraft accidents and incidents caused by structural failure |
Date
! Accident/incident ! Location ! Aircraft ! Cause ! Fatalities ! Notes |
---|
1913-08-07
| United Kingdom | "inherent structural weakness" | 2 | Broke up |
1919-08-02
| Italy | Wing flutter followed by wing collapse | 14, 15, or 17 (sources vary) | The crash killed all aboard |
1921-08-23
| Weather combined with weakened hull | 44 | Deformation followed by fire & explosion |
1925-09-03
| Caldwell, Ohio, United States | Severe weather | 14 | Torn apart by turbulence |
1930-07-23
| Overload/metal fatigue | 6 | Tailplane weakened by turbulence and flutter |
1933-10-10
| United Airlines Chesterton Crash |Indiana, United States | Bombing | 7 | Explosion severed tail section |
1935-02-12
| Loss of USS Macon (ZRS-5) | off California, United States | Akron class airship | Weather combined with unrepaired damage | 2 | Wind shear caused structural failure of the tail which damaged gas cells |
1943-08-01
| 1943 Lambert Field CG-4A crash | St. Louis, United States | Waco CG-4{{#tag:ref|Accident aircraft 42-78839 had been built under license by contractor Robertson Aircraft Corporation.|group=N}} | Manufacturing flaw | 10 | Loss of right-hand wing due to failure of defective wing strut fitting{{sfn|Gero|2010|pp=24–25}} |
1947-10-24
| USA: about 1.5 Miles southeast of Bryce Canyon Airport | Pilot error and design flaw | 52 | Fire caused by failure of pilots to stop fuel transfer and design flaw. Fire eventually lead to an in-flight breakup. |
1952-08-30
| 1952 F-89 airshow crash | Detroit, Michigan, United States | Design flaw | 2 | Wing broke off during flypast{{cite web|url=http://www.ejection-history.org.uk/Aircraft_by_Type/F-89/F-89.htm | title=WORK IN PROGRESS – More to add |publisher=Ejection-history.org.uk |date= |accessdate=2010-07-31}} |
1952-09-06
| {{nowrap|1952 Farnborough Airshow DH.110 crash}} |Farnborough, Hampshire, United Kingdom | Design flaw | 31 | Leading edge aeroelastic flutter caused the aircraft to breakup and crash into the crowd |
1953-02-06
| National Airlines Flight 470 | Severe weather | 46 | Loss of control and structural failure in severe turbulence |
1954-01-10
| Design flaw | 35 | Near Elba: roof fatigue fracture lead to decompression |
1954-04-08
| South African Airways Flight 201 | Design flaw | 21 | Near Naples: decompression due to fatigue |
1955-11-01
|Longmont, Colorado, United States |44 |Bomb placed in suitcase caused in-flight breakup |
1957-04-17
| Near Aqaba, Jordan | Severe weather | 27 | Design strength of left-hand wing exceeded during probable loss of control in severe clear-air turbulence{{sfn|Gero|2010|p=75}} |
1957-05-31
| 1957 McNabs Island RCN Banshee crash | Near Halifax, Nova Scotia, Canada | Manufacturing flaw | 1 | Loss of outer starboard wing due to improperly manufactured fittings in folding wing mechanism{{cite book |last=Mills |first=Carl |title=Banshees of the Royal Canadian Navy |location=Willowdale, ON |publisher=Banshee Publication |year=1991 |isbn=978-0-9695200-0-9 |pages=280–281}} |
1958-09-20
| 1958 Vulcan crash at RAF Syerston |RAF Syerston, United Kingdom | Avro Vulcan prototype | Pilot error | 7 | Flew too fast during low pass exceeded g-limit of leading edge structure, aircraft disintegrated[http://news.bbc.co.uk/1/hi/england/7626243.stm "Anniversary of Vulcan crash."] BBC News, 19 September 2008. |
1959-10-01
| 1959 Lightning crash |Irish Sea, United Kingdom | Lightning T.4 (first aircraft) | Fin collapse due to inertia coupling during high speed tests | 0 | first supersonic ejection by a UK pilot (M 1.7){{cite web|url=http://www.ejection-history.org.uk/project/year_pages/1959.htm |title=2005 |publisher=Ejection-history.org.uk |date= |accessdate=2010-07-31}} Fin enlarged |
1963-01-24
| 1963 Elephant Mountain B-52 crash |Maine, United States | Unknowingly exceeded design capability | 7 | Loss of vertical stabilizer |
1963-01-30
| 1963 B-52 crash in New Mexico |New Mexico, United States | Unknowingly exceeded design capability | 2 | Near Mora:{{cite web |url=http://www.ejection-history.org.uk/aircraft_by_type/b52_stratofortress.htm |title=B-52_Stratofortress |publisher=Ejection-history.org.uk |accessdate=2010-07-31 |archive-url=https://web.archive.org/web/20100214105456/http://www.ejection-history.org.uk/aircraft_by_type/b52_stratofortress.htm |archive-date=2010-02-14 |url-status=dead }} loss of vertical stabilizer{{cite web|title=Look mom, I lost my tail! We gotta bring this Buff in anyway |url=http://www.talkingproud.us/HistoryB52NoTail.html |publisher=TalkingProud.us |accessdate=2009-11-16 |url-status=dead |archiveurl=https://web.archive.org/web/20070604193800/http://www.talkingproud.us/HistoryB52NoTail.html |archivedate=June 4, 2007 }} |
1964-01-04
| 1964 B-57 crash |Dayton, United States | NRB-57 Canberra | Mis-management of fuel system, causing CofG to be beyond its safe rearward limit | 2 | Both wings failed |
1964-01-10
| B-52 flight test of vertical stabilizer |New Mexico, United States | Unknowingly exceeded design capability | 0 | Loss of vertical stabilizer, landed safely |
1964-01-13
| 1964 Savage Mountain B-52 crash |Maryland, United States | Unknowingly exceeded design capability | 3 | Loss of vertical stabilizer |
1964-01-04
|Hamilton Field, California, United States | Design flaw | 1 | Spine failure during 6G pitch-up at air show |
1965-07-06
| 1965 Little Baldon Hastings accident | RAF Abingdon, Oxfordshire, United Kingdom | Design flaw | 41 | Right-hand elevator became uncontrollable due to metal fatigue-related failure of two bolts in elevator system{{sfn|Gero|2010|p=95}} |
1966-03-05
|Mount Fuji, Japan | Severe weather | 124 | Severe clear-air turbulence, gust load over design limit lead to in-flight breakup |
1966-08-06
|Nebraska, United States | Severe weather | 42 | Horizontal and vertical stabilizers detached in severe turbulence |
1967-03-05
|Ohio, United States | Propeller manufacturing defect | 38 | Propeller broke apart; one of the blades punctured the fuselage, causing the forward section to break away |
1967-06-23
|Pennsylvania, United States | Mechanical failure | 34 | Valve in the auxiliary power unit suffered a complete failure, spreading fire to the tailplane and causing a loss of pitch control |
1967-11-15
|Edwards AFB, United States | {{nowrap|North American X-15}} | Pilot error | 1 |
1968-05-03
|Near Dawson, Texas, United States |Severe weather |85 |Controlled flight into thunderstorm with severe turbulence causing in-flight breakup |
1970-07-05
| Pilot error | 109 | Hard landing caused by crew error, causing engine No.4 and pylon to separate; further damage to the right wing caused leaking fuel to ignite and explode, causing the wing to break up and lead to the crash |
1971-03-05
| Belgium | Inadequate maintenance: undetected corrosion | 63 | Near Aarsele: rear pressure bulkhead failure caused loss of tailplane |
1972-06-12
|Detroit, Michigan, United States | MD DC-10 | Design flaw | 0 | Cargo door locking mechanism failed causing door to separate from the aircraft and causing further damage; landed safely |
1973-05-18
|Chita, Soviet Union | Terrorist bombing | 81 | Bomb put on board by hijacker |
1974-03-03
|Picardy, France | MD DC-10 | Design flaw | 346 | Cargo door locking mechanism failed allowing door to separate from the aircraft; cabin floor collapsed, control cables severed, crashed into a forest |
1976-04-14
| Yacimientos Petroliferos Fiscales | Argentina: near Cutral-Co | Improper maintenance: undetected metal fatigue | 34 | Starboard wing failed outboard of engine |
1977-05-14
| 1977 Dan-Air Boeing 707 crash | Near Lusaka Airport, Lusaka, Zambia | Metal fatigue and aircraft design flaw | 6 | Structural failure of the right horizontal stabiliser due to metal fatigue and aircraft design flaw |
1978-06-26
| Helikopter Service Flight 165 | North Sea, Norway | Fatigue | 18 | Rotor blade loosened after fatigue to the knuckle joint: crashed into the sea{{cite web |url=http://www.aibn.no/ln-oqs-pdf?pid=Native-ContentFile-File&attach=1 |title=Rapport om luftfartsulykke i Nordsjøen den 26. juni 1978 ca. kl. 1115 med helikopter S-61 LN-OQS, tilhørende K/S Helikopter Service A/S |publisher=Accident Investigation Board Norway |language=Norwegian |format=PDF |date=17 January 1980 |accessdate=19 September 2012 |archivedate=26 August 2014 |archiveurl=https://web.archive.org/web/20140826103126/http://www.aibn.no/ln-oqs-pdf?pid=Native-ContentFile-File&attach=1 |url-status=live }} |
1979-05-25
| American Airlines Flight 191 |Chicago, United States | MD DC-10 | Improper maintenance | 271 + 2 on ground | No.1 engine broke off due to faulty maintenance procedure; slats retracted, leading the plane to stall and crash |
1981-06-02
| Moerdijk, Netherlands | Severe weather | 17 | Starboard wing detached from airframe due to loads exceeding design limits after the aircraft entered a tornado. |
1982-03-11
| Gamvik, Norway | de Havilland Canada Twin Otter | Severe weather | 15 | Vertical stabilizer and rudder failed during clear-air turbulence{{cite web|url=http://www.stortinget.no/Global/pdf/Dokumentserien/2004-2005/dok24-200405.pdf |title=Rapport til Stortingets presidentskap fra Stortingets granskningskommisjon for Mehamn-ulykken |format=PDF |author=Parliament of Norway |author-link=Parliament of Norway |date=20 September 2005 |language=Norwegian |accessdate=20 October 2012 |archivedate=19 January 2016 |archiveurl=https://web.archive.org/web/20160119132351/https://www.stortinget.no/Global/pdf/Dokumentserien/2004-2005/dok24-200405.pdf |url-status=live }} |
1985-06-23
|Atlantic Ocean off County Cork | Terrorist bombing | 329 | Terrorist bomb placed in cargo hold |
1985-08-12
|Mount Osutaka, Japan | Improper maintenance | 520 | Faulty repair after same plane suffered a tailstrike: the rear bulkhead failed which caused the tail fin to fall off and rupture all four hydraulic systems. The crash remains the deadliest single-aircraft accident in aviation history. |
1987-11-28
| South African Airways Flight 295 | Indian Ocean, 134 nautical miles (248 km) north-east of Mauritius, | Fire | 159 | Catastrophic and contained cargo fire in rear cargo deck lead to the separation of tail section, an in-flight break up and a high-speed dive into ocean |
1988-04-28
|Hawaii, United States | Improper adhesive bonding of fuselage lap joints | 1 | Corrosion and fatigue: 18 ft of roof separated from fuselage |
1988-12-21
|Lockerbie, United Kingdom | Terrorist bombing | 259 + 11 on ground | Terrorist bomb in the forward luggage hold |
1989-02-24
|Hawaii, United States | Dirt on microswitch/short circuit | 9 | Cargo door opened (electrical fault), causing surrounding structure to fail leaving large hole; landed safely |
1989-09-08
| 18 km north of Hirtshals, Denmark | Improper maintenance: use of counterfeit aircraft parts | 55 | Highest death toll involving a Convair 580; loosening of vertical stabilizer due to excessive wear on mounting bolts |
1989-09-19
| Sahara Desert, Ténéré, Niger | Terrorist bombing | 170 | Bomb hidden in forward cargo hold detonated at 35,000 feet leading to in-flight break-up scattering debris over a wide area across the Sahara |
1990-04-12
| Værøy, Norway | de Havilland Canada Twin Otter | Severe weather | 5 | Rudder and tailplane cracked during extreme winds{{cite web |url=http://www.aibn.no/aviation/reports/1991-01 |title=Rapport of luftfartsulykke ved Værøy lufthavn den 12. april 1990 med Twin Otter LN-BNS |author=Accident Investigation Board Norway |author-link=Accident Investigation Board Norway |year=1991 |format=pdf |language=Norwegian |url-status=dead |archiveurl=https://archive.today/20120717225719/http://www.aibn.no/aviation/reports/1991-01 |archivedate=2012-07-17 }} |
1990-06-10
| Didcot, United Kingdom | Faulty maintenance | 0 | Window separated from plane causing the pilot to be sucked out. First Officer successfully landed the plane in Southampton |
1991-02-06
|1991 Gulf War Boeing KC-135 accident |Near Jeddah, Saudi Arabia |Severe weather and wake turbulence |0 |Due to excess maneuvering, the airframe was pushed to its limits. Two out of the four engines detached from the aircraft. The plane executed an emergency landing |
1991-05-26
| Phu Toei National Park, Amphoe Dan Chang, Thailand | Manufacturing error: faulty thrust reverser | 223 | Thrust reverser in No.1 engine unexpectedly deployed while cruising at 35,000 ft causing it to bank sharply to the left and enter a high-speed dive and breaking up at roughly 4000 ft scattering wreckage over a wide area |
1991-09-11
| Continental Express Flight 2574 |Texas, United States | Improper maintenance | 14 | Failure of the horizontal stabilizer during flight due to misunderstanding during maintenance |
1992-10-04
|Bijlmermeer, Netherlands | Corrosion in pylon fuse pin leading to metal fatigue | 4 on board, 39 on ground | Engine No.3 separated from its pylon which caused the adjacent engine No.4 to also fall off, taking the slats with them; stall and crash on attempted landing |
1996-07-17
| Moriches Inlet, near East Moriches, New York, United States | Fuel tank explosion | 230 | Exploded, broke up, and crashed off the coast of Long Island 30 minutes after taking off from New York bound for Paris due to a catastrophic central fuel tank explosion resulting in the forward fuselage section, which included the main flight deck first class and a portion of business class, separating and causing the remaining section to climb, abruptly stall, and enter a high speed dive, causing the left wing to also separate and plunge into the Atlantic Ocean in flames |
1997-06-26
| Helikopter Service Flight 451 | Norwegian Sea, Norway | Eurocopter AS 332L1 Super Puma | Fatigue | 12 | The accident was caused by a fatigue crack in the spline, which ultimately caused the power transmission shaft to fail. The helicopter crashed into the sea.{{cite web |url=http://www.aibn.no/ln_opg_eng_total-pdf?pid=Native-ContentFile-File&attach=1 |title=Report on the air accident 8 September 1997 in the Norwegian sea approx. 100 NM west north west of Brønnøysund, involving Eurocopter AS 332L1 Super Puma, LN-OPG, operated by Helikopter Service AS |publisher=Accident Investigation Board Norway |format=PDF |date=November 2001 |accessdate=19 September 2012 |archivedate=27 March 2012 |archiveurl=https://web.archive.org/web/20120327075439/http://www.aibn.no/ln_opg_eng_total-pdf?pid=Native-ContentFile-File&attach=1 |url-status=live }} |
1997-12-19
| Musi River, Palembang, Indonesia | Pilot suicide (disputed by NTSC) | 104 | Entered a high-speed vertical dive and broke up on its way down into the Musi River |
1999-01-31
| Atlantic Ocean, 100 km (62 mi) S of Nantucket | Pilot suicide (disputed) | 217 | Abruptly descended rapidly before rapidly climbing before finally entering a high-speed dive, causing the No.1 engine and portions of the wings to break off on its way down towards the ocean |
2000-01-31
| Pacific Ocean near Anacapa Island | Maintenance intervals extended beyond safe limit | 88 | Lack of lubrication causing structural failure of the jackscrew on the horizontal stabiliser resulting in aircraft descending inverted into sea |
2001-11-12
| American Airlines Flight 587 |Queens, New York City, United States | Pilot error | 265 | Overuse of rudder leading to loss of vertical stabilizer |
2002-04-30
| 2002 Eglin Air Force Base F-15 crash | Undetected corrosion | 1 | Near Eglin AFB: port fin leading edge failed during test dive |
2002-05-25
|Taiwan Strait near Penghu Islands, Taiwan | Faulty maintenance, metal fatigue | 225 | Tailstrike leading to faulty repair: tail section broke off, causing aircraft to disintegrate |
2003-02-01
| Space Shuttle Columbia disaster |Texas, United States | Design flaw | 7 | Damaged TPS during launch, breakup during reentry |
2005-12-19
| Chalk's Ocean Airways Flight 101 |Miami Beach, Florida, United States | Improper maintenance | 20 | In-flight wing failure due to metal fatigue |
2007-01-01
| Makassar Strait off Majene, Sulawesi, Indonesia | Pilot error | 102 | Spatial disorientation, inertial reference system (IRS) malfunction gradually banked to the left and entered a high-speed dive and broke up on its way down |
2008-05-30
|Spain | 2 | Wing failure |
2014-10-31
| Near the Mojave Desert, California, United States | Scaled Composites Model 339 SpaceShipTwo | Pilot error and design flaw | 1 | Premature activation of the air brake device used for atmospheric re-entry lead to an in-flight breakup |
2015-10-31
| North Sinai Governorate, Egypt | Airbus A321-200 | Terrorist bombing | 224 | Bomb that was smuggled into rear cargo hold disguised as a soft drink can contained four packs of dynamite, causing the tail section to separate and lead to an in-flight break up, scattering the wreckage in the Sinai Desert |
2016-05-19
| Mediterranean Sea | Airbus A320-200 | Explosion/fire caused by oxygen leak | 66 | Accident was caused by oxygen leak in the cockpit; the following combustion and explosion ignited by the pilot's cigarette caused a fire and the break-up of the airplane into the Mediterranean Sea |
2017-10-07
|2017 United States Marine Corps KC-130 crash |Leflore County, Mississippi, United States |Improper maintenance |16 |Accident was caused by improper repairs conducted in 2011 on a corroded propeller blade |
See also
References
=Notes=
{{Reflist|group=N}}
=Citations=
{{Reflist}}
=Bibliography=
- {{cite book |last=Gero |first=David B. |title=Military Aviation Disasters: Significant Losses Since 1908 |publisher=Haynes Publishing |year=2010 |isbn=978-1-84425-645-7}}
{{Lists of aviation accidents and incidents}}
{{DEFAULTSORT:Aircraft structural failures}}