7 fatalities

2008-11-27: Airbus A320 (D-AXLA) — XL Airways — Saint-Cyprien, France

Saint-Cyprien, FranceLanding (descent or approach)

On November 27, 2008, an Airbus A320 (registration D-AXLA) operated by XL Airways was involved in an aviation accident near Saint-Cyprien, France during landing or approach. 7 people were killed. Investigators recorded the probable cause as: The accident was caused by the loss of control of the airplane by the crew following the improvised demonstration of the functioning of the angle of attack protections, while the blockage of the angle of attack sensors made it impossible for these protections… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781197043Data APIEditorial standards
Aircraft registered D-AXLA
Aircraft registered D-AXLA. Photo: Andrei Dimofte / CC BY 2.0, via Wikimedia Commons

Flight GXL888T from Perpignan-Rivesaltes crashed after the crew lost control during an improvised demonstration of angle of attack protections, while the sensors were blocked.

Flight Details

Flight GXL888T, operated from Perpignan-Rivesaltes aerodrome, was conducted as part of the end of a leasing agreement, prior to the return of aircraft D-AXLA to its owner. The planned checks could not be performed in general air traffic, so the flight was shortened. In level flight at FL320, angle of attack sensors 1 and 2 stopped moving and their positions did not change until the end of the flight.

Sequence of Events

After about an hour of flight, the airplane returned to the departure aerodrome airspace and the crew was cleared to carry out an ILS procedure to runway 33, followed by a go around and a departure towards Frankfurt/Main (Germany). Shortly before overflying the initial approach fix, the crew carried out the check on the angle of attack protections in normal law. They lost control of the airplane, which crashed into the sea.

Probable Cause and Contributing Factors

The accident was caused by the loss of control of the airplane by the crew following the improvised demonstration of the functioning of the angle of attack protections, while the blockage of the angle of attack sensors made it impossible for these protections to trigger. The crew was not aware of the blockage of the angle of attack sensors. They did not take into account the speeds mentioned in the program of checks available to them and consequently did not stop the demonstration before the stall.

Contributing factors included: the decision to carry out the demonstration at a low height; the crew's management, during the thrust increase, of the strong increase in the longitudinal pitch, the crew not having identified the pitch-up stop position of the horizontal stabilizer nor acted on the trim wheel to correct it, nor reduced engine thrust; the crew having to manage the conduct of the flight, follow the program of in-flight checks, adapted during the flight, and the preparation of the following stage, which greatly increased the workload and led the crew to improvise according to the constraints encountered; the decision to use a flight program developed for crews trained for test flights, which led the crew to undertake checks without knowing their aim; the absence of a regulatory framework in relation to non-revenue flights in the areas of air traffic management, operations and operational aspects; and the absence of consistency in the rinsing task in the airplane cleaning procedure, and in particular the absence of protection of the AOA sensors during rinsing with water of the airplane three days before the flight. This led to the blockage of the AOA sensors through freezing of the water that was able to penetrate inside the sensor bodies.

Other factors that probably contributed included inadequate coordination between an atypical team composed of three airline pilots in the cockpit, and the fatigue that may have reduced the crew's awareness of the various items of information relating to the state of the systems.