Spanair Flight 5022
EC-HFP nicknamed "Sunbreeze", in Star Alliance livery, the aircraft involved in the incident at Barajas Airport in January 2008.
|Date||20 August 2008|
|Summary||Stalled immediately after takeoff and crashed to the right of the runway due to improper wing configuration|
|Site||Barajas Airport, Madrid, Spain
|Aircraft type||McDonnell Douglas MD-82|
|Operator||Spanair in final Star Alliance livery|
|Flight origin||Madrid-Barajas Airport|
|Destination||Gran Canaria Airport|
Spanair Flight 5022 (JK5022) was a scheduled domestic passenger flight from Madrid-Barajas Airport to Gran Canaria Airport, Spain, that crashed just after take-off from runway 36L of Barajas Airport at 14:24 CEST (12:24 UTC) on 20 August 2008. The aircraft was a McDonnell Douglas MD-82, registration EC-HFP. 154 people died; six died en route to hospital, one died overnight and one died in hospital three days later. Only 18 people 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 MD-80 series aircraft. It was the world's deadliest aviation accident in 2008 and Spain's deadliest since the 1983 crash of Avianca Flight 011.
The accident weakened Spanair's image, which at the time was already negative among the public because of frequent breakdowns and delays. The crash exacerbated financial difficulties at Spanair, which ceased operations on 27 January 2012.
- 1 Crash
- 2 Fatalities
- 3 Investigation
- 4 Similar accidents
- 5 See also
- 6 Notes
- 7 References
- 8 External links
The flight was a Star Alliance codeshare (carrying passengers booked by multiple airlines), operated on behalf of Lufthansa as LH 2554. On board at takeoff were 166 passengers and six crew members.
The accident occurred as the aircraft attempted to take off, 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-82 has a warning system (the Take-off warning system or TOWS) that should have alerted the pilots that the plane 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.
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; that sensor was de-activated on the ground (reportedly an established procedure, as that sensor is redundant). Another takeoff was then attempted, during which the accident occurred.
Of the 172 people on board, 146, including all crew members, perished in the crash or immediately after in the fire; of the 26 passengers rescued alive from the crash site, six died before arriving at hospital, and two more in hospital, bringing the total number of fatalities to 154.
135 of the deceased and 16 of the survivors were Spanish nationals; 19 of the deceased and 2 survivors were of other nationalities. The deceased included German, French, Mauritanian, Turkish, Bulgarian, Gambian, Italian, Indonesian and Brazilian citizens.
The crash flung some of the survivors 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. Flight data recorders 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 just repeats the flaps' and slats' correct 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 incidents 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 plane 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 dysfunction 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 captain's approval.
On 11 May 2010, details from the cockpit voice recorder were leaked to the public and 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. These were the two mechanics who checked the plane before take-off and the head of maintenance for Spanair at Barajas.
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 plane 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 plane'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, citing a source in the investigation team,[who?] reported that the cockpit voice recorder 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 warning signal that the flaps were not set failed to sound for unknown reasons.
The maintenance logbook of the airplane has comments, 2 days before the crash, for an "autoslats failure" visual alarm occurring on slats extension; however autoslats are not used on takeoff, 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. If true, this might explain why de-icing of the Total Air Temperature probe activated on the ground, causing overheating, since in flight the heater would activate only when there was no air flow in the probe, a sign of icing.[not in citation given] This might also explain why the flaps and slats alarm had not sounded, since this alarm is disabled in flight mode.
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 fuse to engage flight mode, but the fuse is afterwards sometimes not replaced correctly. Because of the frequent handling of this fuse, it is also not easy to visually check that the fuse is functioning properly (as is customary for the pilots to do when they enter the cockpit). Hudspeth speculates that this may have happened with both JK 5022 and Northwest Airlines Flight 255.
Spanish daily El Pais reported that, as revealed in an internal report issued by Spanair, malware which had infected their central computer system used to monitor technical problems with their aircraft may have resulted in a failure to raise an alarm over multiple problems with the plane. A judge ordered the airline to provide all the computer'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 the incorrect plane 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 about a deterioration in the flight 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.
CIAIAC's interim report specifically mentioned three other fatal accidents caused by the failure to deploy flaps and slats prior to take-off: Northwest Airlines Flight 255, Delta Air Lines Flight 1141, and Mandala Airlines Flight 091.
In the case of Northwest Airlines Flight 255, also an MD-82, the crew had similarly been disrupted from routine operation before the fatal takeoff, and the alarm similarly had not sounded. In that accident, the reason for the lack of TOWS alarm was a tripped (or pulled) circuit breaker. However, examination of the alarm and its circuit breaker in Spanair 5022 had not revealed any fault.
- 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)
- List of passengers (Archive) (Spanish)
- Press release 1 (Archive), 20 August 2008
- Press release 2 (Archive), 20 August 2008
- Press release 3 (Archive)
- Video of the accident, which had been examined by the official investigating team. The video, from an airport security camera, showed the aircraft gaining very little altitude, returning to the ground, apparently just to the right of the runway, continuing forward for some distance beyond the end of the runway and then dropping into the river-bed and catching fire.
- Photos of the crashed airliner from AirDisaster.com
- Pre-crash photos of the airliner at airliners.net
- Progress Note A-032/2008 (English), August 2010
- Interim Report A-032/2008 (English), August 2009
- Safety Recommendation REC 0/19 (English), February 2009
- Preliminary Report A-32/2008 (English), October 2008
- Final Report A-032/2008 (English)
- Final Report A-032/2008 (Spanish)