← FAA Federal Register actions

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

airworthiness · Rule · Final rule. · Published 2016-02-09 · Effective 2016-03-15 · 81 FR 6755

Document

Document number
2016-02476
Federal Register citation
81 FR 6755
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Rolls-Royce plc Turbofan
Publication date
2016-02-09
Effective date
2016-03-15
FAA docket
Docket No. FAA-2015-3778

Abstract

We are adopting a new airworthiness directive (AD) for all Rolls-Royce plc (RR) RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4- C-37 turbofan engines. This AD requires recalculating the cyclic life for certain engine life-limited rotating parts and removing those parts that have exceeded their cyclic life limit within specified compliance times. This AD was prompted by a review of operational data that determined certain RR RB211-535E4-37 engines have been operated to a more severe flight profile than is consistent with the flight profile used to establish the cyclic life limits for the rotating parts. We are issuing this AD to prevent failure of life-limited rotating parts, uncontained parts release, damage to the engine, and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown