Spanair Flight 5022
EC-HFP, the aircraft involved in the accident, in Star Alliance livery a month before the crash.
|Date||20 August 2008|
|Summary||Crashed on take-off due to improper flaps and slats selection, Pilot error|
Madrid–Barajas Airport, Madrid, Spain|
|Aircraft type||McDonnell Douglas MD-82|
|Flight origin||Barcelona–El Prat Airport|
|Destination||Gran Canaria Airport|
Spanair Flight 5022 (JK5022) was a scheduled domestic passenger flight from Barcelona–El Prat Airport to Gran Canaria Airport, Spain, via Madrid–Barajas Airport that crashed just after take-off from runway 36L at Madrid Airport at 14:24 CEST (12:24 UTC) on 20 August 2008. The aircraft was a McDonnell Douglas MD-82, registration EC-HFP. Of the 172 passengers and crew on board, 154 died and 18 survived.
It was the only fatal accident for Spanair (part of the SAS Group) in the 25-year history of the company, and the 14th fatal accident and 24th hull loss involving McDonnell Douglas MD-80 series aircraft. It was Spain's deadliest accident since the 1983 crash of Avianca Flight 011.
The accident further worsened Spanair's already negative image at the time, which was plagued by poor customer service, frequent breakdowns, and delays.[not in citation given] The crash exacerbated financial difficulties at Spanair, which ceased operations on 27 January 2012.
- 1 Flight and aircraft
- 2 Victims
- 3 Investigation
- 4 In popular culture
- 5 Similar accidents
- 6 See also
- 7 Notes
- 8 References
- 9 External links
Flight and aircraft
There were 166 passengers and six crew members on board, including the 39-year-old captain and the 31-year-old first officer.
This was the flight's second attempted take-off: over an hour earlier, the pilots had attempted and aborted a departure because a sensor reported excessive temperatures in an air intake; the aircraft was then taken to a maintenance area. There maintenance workers tried to repair the faulty sensor, but were unsuccessful. As a result, the sensor was de-activated on the ground (reportedly an established procedure, as the sensor was redundant for that flight).[not in citation given] Another takeoff was then attempted, during which the accident occurred.[not in citation given]
The accident occurred during the second attempt, at 14:24 local time, due to the pilot's failure to deploy the flaps and slats as required for takeoff. Without the use of these "high-lift" devices, the wings could not generate enough lift to keep the aircraft airborne.[Note 1] The MD-80 has a warning system (the take-off warning system or TOWS) that should have alerted the pilots that the aircraft was not correctly configured for take-off. However, the warning did not sound, and the pilots continued with the attempt. The aircraft left the ground momentarily, rolled to the right, and impacted the ground next to the runway. The wings separated from the aircraft and the fuselage broke into two main parts; the wings and the rear two-thirds of the fuselage were engulfed by fire.
Of the 172 people on board, 146, including all crew members, perished in the crash or immediately after in the fire; of the twenty-six passengers rescued alive from the crash site, six died before arriving at hospital, and two more died in hospital, bringing the total number of fatalities to 154.
Most of the deceased and 16 of the survivors were Spanish nationals; nineteen of the deceased and two survivors were of other nationalities.
The crash flung some of the survivors clear of the wreckage and into a stream, lessening the severity of their burns. A 30-year-old woman with British and Spanish dual citizenship survived with a punctured lung and broken left arm but no burns, as she was flung from row 6, still attached to her seat, into the stream.
Nationalities of passengers and crew
The accident was investigated by the Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Representatives from the US National Transportation Safety Board, the aircraft manufacturer Boeing (as successor to McDonnell Douglas, the original aircraft manufacturer), and the engine manufacturer Pratt and Whitney supported the investigation.
A preliminary report on the accident was released by CIAIAC on 6 October 2008. Information extracted from the Flight data recorder showed that the aircraft had taken off with flaps at 0°, and that the alarm for that abnormal takeoff configuration had not sounded. The report hinted at no other cause of the accident. Both the engines and thrust reversers were excluded as causes of the accident.
On 17 August 2009, CIAIAC released an interim report on the incident. The interim report confirmed the preliminary report's conclusion that the crash was caused by an attempt to take off with the flaps and slats retracted, which constituted an improper configuration, and noted that safeguards that should have prevented the crash failed to do so. The cockpit recordings revealed that the pilots omitted the "set and check the flap/slat lever and lights" item in the After Start checklist. In the Takeoff Imminent verification checklist the copilot had simply repeated the correct flap and slat position values without actually checking them, as shown by the physical evidence. All three safety barriers provided to avoid the takeoff in an inappropriate configuration were defeated: the configuration checklist, the confirm and verify checklist, and the Take-off Warning System (TOWS). The report also made a number of safety recommendations intended to prevent accidents like this from happening again.
CIAIAC published a further progress note in August 2010, and its final report in July 2011.
Fire or explosion
Some early eye-witness accounts suggested that the aircraft suffered an engine fire or explosion before crashing, but the Spanish airport authority AENA released a video showing that the engines neither exploded nor caught fire during take-off. Manuel Bautista, Director General of Spain's civil aviation authority, went as far as to state: "The engine is not the cause of the accident", surmising that a chain of events combining together was more likely than a single cause.
There has been considerable interest in the faulty air temperature probe (the total air temperature sensor,[Note 2] located on the front of the aircraft near the cockpit) that initially caused the pilot to turn the aircraft back for maintenance before the second takeoff attempt. The mechanic simply deactivated the probe because the aircraft's Minimum Equipment List allowed it to be left inoperative. On 22 August investigators interviewed the mechanic, who defended his action by saying that it had nothing to do with the crash. Spanair has supported the mechanic's view that deactivation of the probe is an accepted procedure. On 1 September a report, quoting Spanair, stated that the problem detected on the first takeoff attempt was overheating caused by a temperature gauge's de-icing system, rather than a malfunction of the temperature gauge itself, and that since icing was not a risk on that flight, the de-icing system had been deactivated by the mechanic with the captain's approval.
On 11 May 2010, leaked details from the cockpit voice recorder (CVR) were released by Spanish media. The recording showed that both pilots were concerned about a repair job performed earlier on the day of the crash, in which mechanics used an ice pack to cool an overheating temperature sensor and removed a fuse. The BBC reported that the judge investigating the crash was to question three mechanics on suspicion of manslaughter.[needs update] These were the head of maintenance for Spanair at Barajas and the two mechanics who checked the aircraft before take-off.
One theory was that the thrust reverser of the No. 2 (right side) engine activated during the climb, since one of the thrust reversers was seen to be in the deployed position in the wreckage. The investigation concluded that the position of the thrust reverser was a result of the accident, not a cause of it. If the reverser deployed during takeoff, and not as a result of impact, it has been suggested that the aircraft would have yawed suddenly to the right. Aircraft engineer Alberto Garcia dismissed this suggestion, pointing out that the MD-82 has tail-mounted engines positioned close to each other and to the aircraft's longitudinal axis, so that any yaw from asymmetric thrust would be small. Thrust reversers are normally employed just after touch down to reduce braking distances. Examination of the aircraft's maintenance logs showed that the thrust reverser on the right-side engine had been deactivated pending repair. It had been wired shut, and tape placed over the cockpit control to alert the crew. The MD-82 is permitted to fly with just one operable thrust reverser.
Flaps and slats
El Mundo reported that the CVR showed that the pilot had said "Flaps OK, Slats OK" to the co-pilot. The article confirmed that the flaps had not been extended and that the alarm for that condition had not sounded. The final report concluded that the failure to deploy flaps was the cause of the accident.
The maintenance logbook of the aircraft has comments, two days before the crash, for an "autoslats failure" visual alarm occurring on slats extension; however autoslats are not used on takeoff,[not in citation given] and it cannot be inferred that the slats system had a defect.
In an article published on 7 September, El Mundo suggested that during the flight preparation and takeoff attempts, the aircraft had some of its systems in flight mode rather than ground mode. Investigators noted that one particular ground-sensing relay (relay R2-5) was responsible for de-energizing the Total Air Temperature probe heater when on the ground, and for inhibiting TOWS when in the air. They theorized that a fault in this relay could explain both the overheating of the probe and why the flaps and slats alarm had not sounded. When the R2-5 relay was recovered from the wreckage it was subjected to detailed examination. Two stuck contacts within the relay were identified, which would explain the overheating both on the day of the accident and the intermittent incidents recorded over the previous few days. That fault, however, would not have affected the operation of the TOWS system, and no fault was found that would have affected TOWS.
James W. Hudspeth, an investigator of a previous near accident (an MD-83, starting from Lanzarote) that was similar in its details, pointed out that the fuse of the so-called "left ground control relay" at position K-33 of the control panel might have been the actual culprit in the erroneous flight mode: Hudspeth found out during a 2-week investigation at Lanzarote that it is customary in normal maintenance routine to temporarily remove this circuit-breaker to engage flight mode, but the circuit-breaker is afterwards sometimes not replaced correctly. Because of the frequent handling of this circuit-breaker, it is also not easy to visually check that it is set properly (as is customary for the pilots to do when they enter the cockpit). The CIAIAC team on the case of JK 5022 discounted this possibility because if the circuit-breaker had been left open it would also have affected the operation of the stall warning system, and the CVR recording showed that the stall warning system was functioning normally.
Spanish daily El Pais reported that, as revealed in an internal report issued by Spanair, malware which had infected the airline's central computer system used to monitor technical problems with its aircraft may have resulted in a failure to raise an alarm over multiple problems with the aircraft. A judge ordered the airline to provide all the computer system's logs from the days before and after the crash.
The CIAIAC published its final report into the accident on 26 July 2011.
It determined that the cause of the accident was:
- The crew lost control of the aircraft as a result of a stall immediately after takeoff, which was caused by an incorrect configuration for take-off (i.e. not deploying the flaps and slats, following a series of errors and omissions), coupled with the absence of any warning of the incorrect configuration.
- The crew did not recognize the indications of stall, and did not correct the situation after takeoff, and – by momentarily retarding the engine power and increasing the pitch angle – brought the aircraft closer to a stall condition.
- The crew did not detect the configuration error because they did not properly use the checklists to select and check the position of the flaps and slats during flight preparation, specifically:
- they failed to select the flaps/slats lever during the corresponding step in the "After Start" checklist;
- they did not cross-check the position of the lever and the state of the flaps/slats indicator lights during the "After Start" checklist;
- they omitted the flaps/slats check on the 'Take Off Briefing' (taxi) checklist;
- no visual inspection of the flaps and slats was carried out in execution of the "Final Items" step of the "Take Off Imminent" checklist.
The CIAIAC determined the following contributory factors:
- The absence of any warning of the incorrect take-off configuration because the TOWS did not work. It was not possible to determine conclusively why the TOWS system did not work.
- Inadequate crew resource management (CRM), which did not prevent the deviation from procedures and omissions in flight preparation.
In popular culture
- Northwest Airlines Flight 255
- Delta Air Lines Flight 1141
- Mandala Airlines Flight 091.
- Lufthansa Flight 540
- LAPA Flight 3142
- British European Airways Flight 548
- The basic shape of all aircraft wings is designed for optimum speed and fuel-efficiency during cruise flight (at around 500mph/430 knots IAS [indicated airspeed] in the MD-82). At lower speeds, such as those associated with take-offs and landings (typically 160mph), the lift generated by the wings is much less than at cruise speed – or would be were it not for the use of high-lift devices such as flaps and slats. For low-speed flight, the pilot alters the shape of the wing by deploying the flaps and slats. For take-off, this is done during the pre-takeoff checks, before entering the runway; on the MD-82, flaps and slats are controlled by a single lever on the cockpit's central console. The flaps are located at the trailing edge of the wings and, when deployed, extend backward and downward from the wing. The slats extend forward from the leading edge of the wing. The effect of both flaps and slats is to increase the surface area and "camber" of the wing, thereby increasing the amount of lift produced. See flaps and slats for more information.
- The aircraft's computer uses total air temperature to help calculate the ambient air temperature, which in turn is needed to calculate the aircraft's true airspeed. True airspeed is needed for high altitude navigation, but is not so important for maintaining stable flight. Ground Speed is calculated directly from GPS position change (or Inertial navigation position change on earlier models). When TAS (true airspeed) is compared with Groundspeed, however, the actual wind direction and speed at that altitude can be calculated and presented to the pilot. Indicated airspeed, a measure of the relative wind over the aircraft's surfaces, is a more important measure for ensuring stable, safe flight. The aircraft's stall speed closely relates to indicated airspeed, for example.
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|Wikimedia Commons has media related to Spanair Flight JK 5022.|
- Spanair Last Official Notice (Archive)
- Press release 1 (Archive), 20 August 2008
- Press release 2 (Archive), 20 August 2008
- Press release 3 (Archive)
- Security camera video of the accident
- Photos of the crashed airliner from AirDisaster.com
- Pre-crash photos of the airliner at airliners.net
- Civil Aviation Accident and Incident Investigation Commission Progress Note A-032/2008 (in English), August 2010
- Civil Aviation Accident and Incident Investigation Commission Interim Report A-032/2008 (in English), August 2009
- Civil Aviation Accident and Incident Investigation Commission Safety Recommendation REC 0/19 (in English), February 2009
- Civil Aviation Accident and Incident Investigation Commission Preliminary Report A-32/2008 (in English), October 2008
- Civil Aviation Accident and Incident Investigation Commission Final Report A-032/2008 (in English)
- Civil Aviation Accident and Incident Investigation Commission Final Report A-032/2008 (in Spanish)