Descripción del Accidente ASN 18 MAY 2005 Airbus A320-211 JY-JAR - Leeds/Bradford Airport (LBA)
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Estado:Accident investigation report completed and information captured
Fecha:miércoles 18 mayo 2005
Hora:11:43
Tipo:Silhouette image of generic A320 model; specific model in this crash may look slightly different
Airbus A320-211
Operado por:LTE International Airways
Alquilado a :Jordan Aviation
Registración: JY-JAR
Numéro de série: 234
Año de Construcción: 1991-07-12 (13 years 10 months)
Horas Totales de la Célula:28957
Ciclos:16321
Motores: 2 CFMI CFM56-5A3
Tripulación:Fatalidades: 0 / Ocupantes: 7
Pasajeros:Fatalidades: 0 / Ocupantes: 171
Total:Fatalidades: 0 / Ocupantes: 178
Daños en la Aeronave: Menor
Consecuencias: Repaired
Ubicación:Leeds/Bradford Airport (LBA) (   Reino Unido)
Fase: Aterrizaje (LDG)
Naturaleza:Vuelo Internacional No Programado
Aeropuerto de Salida:Puerto del Rosario Airport, Canary Islands/Fuerteventura Island (FUE/GCFV), España
Aeropuerto de Llegada:Leeds/Bradford Airport (LBA/EGNM), Reino Unido
Descripción:
While landing on runway 14 at Leeds Bradford Airport the aircraft touched down just beyond the end of the marked touchdown zone with low autobrake selected. Manual wheel braking commenced shortly after mainwheel touchdown. At a groundspeed of around 70 kt the brakes ceased operating, for about 17 seconds. A pronounced dip in the runway surface initially prevented the pilots from seeing the runway end. When it became apparent to the commander that it would not be possible to stop before the end of the
runway, he deliberately did not select alternate braking, as this would have caused loss of nosewheel steering, but instead used nosewheel steering to turn the aircraft sharply to the right. The aircraft skidded sideways and came to a halt with its nosewheels off the runway, shortly before the end of the paved surface and the start of a steep down slope.

Probable Cause:

Causal factors:
1. Excessive wheel tachometer signal noise, caused by a bent tachometer driveshaft on each main landing gear assembly, resulted in loss of braking using the Normal system.
2. Inadequate fault tolerance within the brake control system led to the sustained loss of Normal braking during the landing ground roll.
3. There was no flight deck indication of brake system malfunction, and this delayed the crewÂ’s recognition of the loss of braking.
4. There was a lack of effective action to fully rectify brake system anomalies apparent from previous incidents and accidents.

Accident investigation:

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Investigating agency: AAIB (U.K.)
Status: Investigation completed
Duration: 2 years and 7 months
Accident number: AAR 6/2007
Download report: Final report

Fuentes:
» AAIB Formal: AAR 6/2007


Subsiguiente / acciones de seguridad

AAIB issued 7 Safety Recommendations

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Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does not display the exact flight path.
Distance from Puerto del Rosario Airport, Canary Islands/Fuerteventura Island to Leeds/Bradford Airport as the crow flies is 2976 km (1860 miles).

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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