1985 Manchester Airport disaster

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Template:Short description Template:Use dmy dates Template:Use British English Template:Infobox aircraft occurrence The 1985 Manchester Airport disaster occurred when British Airtours Flight 28M (also known as Flight 328), an international passenger flight, was en route from Manchester Airport to Corfu International Airport. It caught fire on takeoff on 22 August 1985, resulting in 55 fatalities.

The aircraft, a Boeing 737-236(A), named River Orrin, was flown by British Airtours, a wholly owned subsidiary of British Airways. It had 131 passengers and 6 crew on the manifest. During the takeoff roll, a loud thump was heard, and takeoff was aborted. An engine failure had generated a fire and the captain ordered evacuation. The engine failure was later traced to an incorrectly repaired combustor can, causing it to rupture and its dome to puncture the left wing fuel tank.<ref name="AAIB_8/88" />Template:Rp Most of the deaths were due to smoke inhalation, not burns; 82 people survived.

The accident was described as "a defining moment in the history of civil aviation safety."<ref name=LessonslearnedBBC>Template:Cite news</ref> It brought about industry-wide changes to the seating layout near emergency exits, fire-resistant seat covers, floor lighting, fire-resistant wall and ceiling panels, more fire extinguishers and clearer evacuation rules.

Aircraft

The aircraft involved was a Boeing 737-236(A), registered as G-BGJL with serial number 743. It was manufactured by Boeing Commercial Airplanes in April 1981 and was powered by two Pratt & Whitney JT8D-15A engines. It had logged 12977 airframe hours in 5907 takeoff and landing cycles.<ref name="ASN">Template:Cite web</ref><ref name="AAIB_8/88" />Template:Rp

Accident

Attempted takeoff

Flight 28M (background) as it turns from Runway 24 to Link D. Note the deployment of the right rear escape slide.

The flight crew, Captain Peter Terrington (39), and First Officer Brian Love (52), were seasoned pilots with 8,441 and 12,277 flight hours (including 1,276 and 345 hours on the Boeing 737), respectively.<ref name="AAIB_8/88">Template:Cite book</ref>Template:Rp At 07:13 BST (06:13 UTC), on runway 24 at Manchester Airport during the takeoff phase, the pilots heard a loud thump coming from underneath the plane. Thinking a tyre had burst, the captain ordered an abandoned takeoff and then activated the thrust reversers. The first officer, who was in control of the aircraft at the time, applied "harsh" braking for about five seconds. The captain, concerned about the possible burst tyre, instructed the first officer to use less wheel braking, which was done.<ref name="AAIB_8/88" />Template:Rp Fire warnings sounded in the flight deck nine seconds after the thump was heard (about 36 seconds before the aircraft stopped). Ten seconds later, the tower controller confirmed, "right, there's a lot of fire." Twenty-five seconds after the thud was heard (about 20 seconds before the aircraft stopped), the tower controller suggested evacuating passengers to the right side.<ref name="AAIB_8/88" />Template:Rp The tower controller activated the airport's fire-alarm siren the moment he first saw smoke coming from the aircraft, but firefighters working for the airport's fire service had heard a "bang" and seen the smoke and fire for themselves, and had already initiated a response on their own.<ref name="AAIB_8/88" />Template:Rp

Forward evacuation

Forward section of the aircraft showing left and right escape slides deployed

The aircraft turned off the runway onto a short taxiway called link "D" and came to a full stop facing northwest.<ref name="AAIB_8/88" />Template:Rp Evacuation efforts began immediately, but several difficulties were encountered. Arthur Bradbury, the purser and the crew's senior flight attendant, tried to open the right front exit door about 10 seconds before the aircraft stopped, but it jammed due to a design fault in the emergency slide system and he abandoned attempts to open it.<ref name="AAIB_8/88" />Template:Rp After about 25 seconds, Bradbury opened the left front door and successfully deployed the escape slide. At this time, the first two fire engines arrived. One began showering the fuselage and the open door with foam to prevent the fire from spreading to the door and the slide as passengers were evacuating, and to provide cooling to protect the passengers still inside.

When the second fire engine arrived, the first fire engine concentrated on the burning jet fuel and the left engine. The second sprayed foam over the fuselage and the open door.<ref name="AAIB_8/88" />Template:Rp During this time, the "No. 4 stewardess", Joanna Toff, had kept passengers out of the forward galley area to allow the purser time to open a door. When the left side door was opened, exiting passengers jammed themselves in the narrow Template:Cvt passageway between the two forward galley bulkheads. Toff bodily pulled the passengers out one at a time until she cleared the jam.<ref name="AAIB_8/88" />Template:Rp Meanwhile, the purser had resumed working on the right front door, and he successfully opened the door fully and deployed the escape slide about one minute after the plane had stopped.<ref name="AAIB_8/88" />Template:Rp Sixteen passengers and Toff escaped through the left front door, one of whom was dragged out by Toff while unconscious. The purser and 34 passengers made their escape through the right front door.<ref name="AAIB_8/88" />Template:Rp

Overwing evacuation

Seats relative to the right overwing emergency exit after the accident: The arm rest is partly down. The seat back for the seat closest to the window, seat 10F, was returned to its upright position before this photo was taken.

More difficulties were encountered at the overwing exits. The left overwing exit was blocked by smoke and flames. The passenger seated at the right overwing exit had difficulty understanding how to operate the hatch. At that time, no requirement existed that exit-row passengers receive a briefing on how and when to open the hatch.<ref name="AAIB_8/88" />Template:Rp Once the Template:Cvt hatch was released, it fell inward onto the passenger seated next to it, trapping her. Two passengers lifted the hatch and put it on a seat in the next row back, making the exit available for use 45 seconds after the aircraft had stopped.<ref name="AAIB_8/88" />Template:Rp Once the hatch had been removed, passengers still encountered difficulties in getting to and using this exit. The exit-row seats allowed only Template:Cvt to pass through, the armrests between those seats remained down, and the exit was directly over a seat, requiring passengers to manoeuvre awkwardly to escape.<ref name="AAIB_8/88" />Template:Rp Passengers in the rear of the aircraft were panicking as smoke, and eventually flames, filled the hot cabin at about the same time the right overwing exit was opened. Passengers crawled over seat backs to get to the right overwing exit as well as the two front exits; some survivors told investigators that the aisle had become blocked with bodies.<ref name="AAIB_8/88" />Template:Rp

This caused jamming at all exits, and the seat over which the overwing exit was located failed in such a way that the seat back collapsed forward, causing a further obstruction. A man who had been seated in 16C was found dead lying across this exit, and investigators were unsure whether the seat back collapse had trapped him.<ref name="AAIB_8/88" />Template:Rp A 14-year-old boy was found lying across the top of the man from seat 16C by firefighters 5Template:Frac minutes after the aircraft had stopped. He was alive, suffering only superficial burns to his hands. He was the last of 27 survivors to escape through that exit, and the last evacuee to survive the accident.<ref name="AAIB_8/88" />Template:Rp Most of the 38 bodies were found clustered around the overwing exit.<ref name="AAIB_8/88" />Template:Rp This exit was the first exit available to the 76 passengers seated behind it or even with it, and the nearest exit for 100 passengers.<ref name="AAIB_8/88" />Template:Rp

Fire and loss of aft exits

Orientation of wind, pooling fuel, and flames relative to the aircraft after it stopped on taxiway link D.

Fuel had been spilling from the left wing from the moment the first loud noise was heard. That fuel had ignited on contact with flames from the hole in the engine combustion chamber as the aircraft began to decelerate on the runway. When the aircraft stopped, fuel was still leaking from a Template:Cvt opening at a rate of Template:Nowrap per minute (Template:Nowrap, Template:Nowrap), feeding a growing fire.<ref name="AAIB_8/88" />Template:Rp By about this time, the fire had already penetrated the aluminium alloy skin of the aircraft below the level of the floor in the passenger compartment. The AAIB estimated that between fiveTemplate:Nbspseconds before and 13Template:Nbspseconds after the aircraft stopped were needed for fire to penetrate the fuselage skin.<ref name="AAIB_8/88" />Template:Rp Passengers seated on the left side of the aisle and toward the rear felt intense radiant heat from the fire, and were very impatient to escape, many of them standing and crowding into the aisles while the aircraft was in motion.<ref name="AAIB_8/88" />Template:Rp

As the aircraft began its right turn off the runway, around tenTemplate:Nbspseconds before it stopped, one of the two flight attendants in the rear of the aircraft, probably the No 3 stewardess, opened the right rear door and deployed the emergency chute, but no one escaped through this door because it was blocked by smoke and flames.<ref name="AAIB_8/88" />Template:Rp When the aircraft came to a stop, it was facing the northwest, and a light wind of Template:Convert was blowing from the west, carrying dense smoke, and occasionally flames, in through that door. When the door was first opened, the aircraft had been facing into the wind, and the exit had been clear.<ref name="AAIB_8/88" />Template:Rp When the left front door was opened, this created an airflow from the front of the aircraft to the rear, and out through the right rear door, which likely contained the smoke to the rear of the aircraft.<ref name="AAIB_8/88" />Template:Rp When the right overwing exit and the right front exit were opened, this flow was lost, and the entire cabin rapidly filled with smoke.<ref name="AAIB_8/88" />Template:Rp The left rear exit remained closed.<ref name="AAIB_8/88" />Template:Rp

Fire penetrated into the rear portion of the passenger cabin through the floor and along the left wall within oneTemplate:Nbspminute of the aircraft stopping.<ref name="AAIB_8/88" />Template:Rp Accident investigators said that this quick penetration of fire into the cabin appeared "to conflict markedly with the air transport industry's expectations" for this type of fire, which at that time expected one to threeTemplate:Nbspminutes would be available for evacuation before the fire would be "in a position to directly threaten the occupants".<ref name="AAIB_8/88" />Template:Rp

When firefighters determined that no more passengers would leave the aircraft unassisted, they entered the passenger cabin with fire hoses and attempted to extinguish the blaze inside the aircraft, but fighting the fire inside the aircraft had become futile and unsafe.<ref name="AAIB_8/88" />Template:Rp One firefighter was slightly injured when an explosion threw him out of the door and down to the tarmac.<ref name="AAIB_8/88" />Template:Rp The cause of the explosion was not determined, but heat-induced overpressure and rupture of an aerosol spray can or therapeutic oxygen cylinder are suspected.<ref name="AAIB_8/88" />Template:Rp

Casualties

Toxic smoke and fire caused the deaths of 53Template:Nbsppassengers and two cabin crew, 48 of them from smoke inhalation. Seventy-eight passengers and four crew escaped, with 15Template:Nbsppeople sustaining serious injuries. One passenger, a man rescued 33Template:Nbspminutes after the start of the fire, was found unconscious in the aisle, but died in the hospital sixTemplate:Nbspdays later from injuries to his lungs and the resulting pneumonia.<ref name="AAIB_8/88" />Template:Rp

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Causes

The Air Accidents Investigation Branch (AAIB) report lists a cause for the accident and a separate cause for the fatalities, as well as four contributing factors:<ref name="AAIB_8/88" />Template:Rp

  1. The vulnerability of the wing tank access panels to impact
  2. The lack of any effective provision for fighting major fires inside the aircraft cabin
  3. The vulnerability of the aircraft hull to external fire
  4. The extremely toxic nature of the emissions from the burning interior materials.

Chris Yates, an aviation analyst, later said of the accident, "This was very much a defining moment in the history of civil aviation safety. Specifically, the investigation found that a lot of materials inside the passenger cabin produced highly toxic fumes and required airlines to look again and re-invent the wheel, so to speak."<ref name=LessonslearnedBBC/> It brought about industry-wide changes to the seating layout near emergency exits, fire-resistant seat covers, floor lighting, fire-resistant wall and ceiling panels, more fire extinguishers and clearer evacuation rules.<ref>Template:Cite news</ref>

Accident

The subsequent investigation into the accident said that the No. 9 combustor can on the port engine ruptured, and a section of the can was ejected forcibly into an underwing fuel tank access panel. That panel was fractured, allowing fuel to spill onto hot combustion gases from the engine. The resulting fire developed catastrophically, primarily due to the orientation of the aircraft and the fire to the wind, "even though the wind was light."<ref name="AAIB_8/88" />Template:Rp

Fatalities

The AAIB concluded, "the major cause of the fatalities was rapid incapacitation due to the inhalation of the dense toxic/irritant smoke atmosphere within the cabin, aggravated by evacuation delays caused by a forward right door malfunction and restricted access to the exits."<ref name="AAIB_8/88" />Template:Rp

Previous engine repair

Records showed the engine in question, a Pratt & Whitney JT8D-15, had experienced previous cracks to the No. 9 combustor can that had been repaired in 1983 by fusion welding. The repair did not include solution heat treatment, which was a required procedure for this type of repair.<ref name="AAIB_8/88" />Template:Rp The AAIB evaluated conflicting evidence on the effect of solution heat treatment and "considered that it would not have had a significant effect on the fatigue life of the can."<ref name="AAIB_8/88" />Template:Rp The circumferential edges of the severed forward section of the No. 9 can coincided with some of the cracks that had been welded during that repair. Some of the fracture was in areas where no cracking had been seen at the time of the repair, and the fracture edges were severely damaged during the failure and the ensuing fire.<ref name="AAIB_8/88" />Template:Rp Therefore, the AAIB could not conclude whether the quality of the repair had caused or contributed to the accident.<ref name="AAIB_8/88" />Template:Rp

Aftermath and commemoration

The Civil Aviation Authority was criticised for not implementing stringent safety regulations earlier.<ref>Template:Cite news</ref>

The swift incursion of the fire into the fuselage and the layout of the aircraft impaired passenger evacuation, with areas such as the forward galley area becoming a particular bottleneck.<ref name="AAIB_8/88" />Template:Rp Of those unable to escape, 48 died as a result of incapacitation and subsequently lethal toxic gas and smoke inhalation,<ref name="AAIB_8/88" />Template:Rp some very close to the exits, with six dying from burns. The use of smoke hoods or misting systems was also examined.<ref name="AAIB_8/88" />Template:Rp

The tragedy haunted captain Peter Terrington, who struggled with survivor's guilt for the remainder of his life and discussed the accident with his family "nearly every day."<ref name="captain_Manchester_disaster"/> According to his wife Joan, he was "completely devastated that passengers had lost their lives," and always questioned whether he should have done more. He retired from flying at age 52, after 32 years as a pilot, becoming a counsellor for elderly people dealing with depression and loneliness.<ref name="captain_Manchester_disaster"/> He continuously attended the annual memorial service at Manchester Airport for the flight's victims, remaining concerned that all lessons learned from the accident should be fully implemented in practice. Diagnosed with Parkinson's disease in his later years, Terrington died in February 2016 at age 70 following a brief illness.<ref name="captain_Manchester_disaster">Template:Cite news</ref>

In August 2018, a Template:Cvt memorial commemorating the victims was unveiled near the accident site.<ref>Template:Citation</ref><ref>Template:Cite news</ref>

Awards

The surviving cabin crew, Arthur Bradbury and Joanna Toff, and two members of the Manchester Airport Fire Service, Fireman Samuel Lyttle and Fireman Eric Arthur Westwood, were all awarded the Queen's Gallantry Medal, and the two flight attendants who died, Sharon Ford and Jacqui Urbanski, received the same award posthumously. Their collective citation stated in summary:

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Appearance in media

The accident was the subject of a 1985 World in Action investigation.<ref>Template:Cite episode</ref>

In 2010, this accident was reconstructed for a season-9 episode of Mayday (Air Crash Investigation) entitled "Panic on the Runway" or "Manchester Runway Disaster", showing computer simulations of the accident, as well as interviews with Captain Terrington, survivors, and the air crash investigators.<ref>Template:Cite episode</ref>

See also

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References

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Bibliography

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Template:Aviation accidents and incidents in the United Kingdom in the 1980s Template:Aviation incidents and accidents in 1985