Résumé

During the acceleration for take-off at approx. 95 kt, a high pressure turbine (HPT) disk of the RH engine desintegrated, which resulted in heavy impacts damage, fuel leaks and a fire. The crew carried out an acceleration - stop procedure.

Publication

Pour télécharger le(s) rapport(s), cliquez sur le(s) lien(s) ci-dessous :

• Rapport final (EN) - f-gk820317.pdf (17/03/1982)