Airworthiness Directives; Rolls-Royce Corporation (RRC) AE 3007A Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2010-09-22 · Effective 2010-10-27 · 75 FR 57660
Document
Document number
2010-22370
Federal Register citation
75 FR 57660
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Rolls-Royce Corporation (RRC) AE 3007A Series Turbofan
Publication date
2010-09-22
Effective date
2010-10-27
FAA docket
Docket No. FAA-2009-0811
Abstract
The FAA is superseding an existing airworthiness directive (AD) for RRC AE 3007A series turbofan engines. That AD currently requires performing an eddy current inspection (ECI) or surface wave ultrasonic test (SWUT) inspection on each affected high-pressure turbine (HPT) wheel. This AD requires removing or performing initial and repetitive ECIs or SWUT inspections on HPT stage 2 wheels for cracks. This AD also reduces the approved life limits of certain HPT stage 2 wheels. This AD results from reports of cracked HPT stage 2 wheels. We are issuing this AD to prevent uncontained failure of the HPT stage 2 wheel and damage to the airplane.