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Airworthiness Directives; Rolls-Royce plc (RR) RB211-Trent 768-60 and Trent 772-60 Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 2011-04-12 · Effective 2011-04-27 · 76 FR 20229

Document

Document number
2011-8469
Federal Register citation
76 FR 20229
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce plc (RR) RB211-Trent 768-60 and Trent 772-60 Turbofan
Publication date
2011-04-12
Effective date
2011-04-27
FAA docket
Docket No. FAA-2011-0233

Abstract

We are superseding an existing airworthiness directive (AD) for RR RB211-Trent 700 series turbofan engines. That AD currently requires, for the step aside gearbox (SAGB), repositioning of the oil metering jet up into the oil distributor within the bevel gearshaft, followed by initial and repetitive visual inspections of the magnetic chip detector (MCD). Since we issued that AD, RR has demonstrated that the repositioning of the oil metering jet eliminates the need for the repetitive inspections. This AD changes the applicability from RB211- Trent 700 series turbofan engines, to RB211-Trent 768-60 and Trent 772- 60 turbofan engines. This AD also eliminates the visual inspections of the MCD from the AD requirements. This AD was prompted by RR demonstrating that the repositioning of the oil metering jet eliminates the need for the repetitive inspections, by the need to correct the AD applicability, and by the need to eliminate the visual inspections of the MCD. We are issuing this AD to prevent in-flight engine shutdowns caused by SAGB driving bevel gearshaft ball bearing failure.

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Federal Register document
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