Airworthiness Directives; Rolls-Royce plc (RR) RB211-535 Series Turbofan Engine
airworthiness · Rule · Final rule. · Published 2012-01-31 · Effective 2012-03-06 · 77 FR 4648
Document
Document number
2012-1954
Federal Register citation
77 FR 4648
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Rolls-Royce plc (RR) RB211-535 Series Turbofan
Publication date
2012-01-31
Effective date
2012-03-06
FAA docket
Docket No. FAA-2009-0994
Abstract
We are superseding an existing airworthiness directive (AD) for all RR RB211-535E4-37, -535E4-B-37, -535E4-B-75, and -535E4-C-37 turbofan engines. That AD currently requires performing initial and repetitive visual and fluorescent penetrant inspections (FPI) of the low-pressure (LP) turbine stage 1, 2, and 3 discs to detect cracks in the discs. This new AD continues to require those inspections and changes the definition of a shop visit to be less restrictive. This AD was prompted by our finding that the definition of shop visit in the existing AD was too restrictive. We are issuing this AD to revise the definition of shop visit and to detect cracks in the LP turbine stage 1, 2, and 3 discs, which could result in an uncontained release of LP turbine blades and damage to the airplane.