Turbine blade fatigue endurance limit
Date issue released
Safety Issue Description

High service time stage-2 LP turbine blades were susceptible to a reduction in fatigue endurance as a result of vibratory stresses sustained during operation at speeds close to the maximum.

Issue number
AO-2010-066-SI-01
Transport Function
Aviation: Air transport
Issue Owner
Rolls Royce
Mode of Transport
Aviation
Issue Status Justification

Will ultimately reduce the likelihood of LP2 blade failures. In the meantime, the risk of another complex failure is very low.

Proactive action
Action number
AO-2010-066-NSA-033
Organisation
Rolls Royce
Action date
Action Status
Closed
Action description

The manufacturer is recommending that operators replace high service time stage-2 LP turbine blades.

ATSB Response

Replacment of high time blades should reduce the likelihood of blade failure.