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federal_register: 04-28145

All Federal Register documents (rules, proposed rules, notices, presidential documents) from 1994 to present.

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document_number title type abstract publication_date pub_year pub_month html_url pdf_url agency_names agency_ids excerpts
04-28145 Airworthiness Directives; Rolls-Royce plc RB211 Trent 800 Series Turbofan Engines Proposed Rule The FAA proposes to adopt a new airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 800 series turbofan engines. This proposed AD would require initial and repetitive borescope inspections of the high pressure-and-intermediate pressure (HP-IP) turbine internal and external oil vent tubes for coking and carbon buildup, and cleaning or replacing the vent tubes if necessary. This proposed AD results from a report of an RB211 Trent 700 series engine experiencing a disk shaft separation, overspeed of the IP turbine rotor, and multiple blade release of IP turbine blades. Preliminary findings suggest these events resulted from an internal oil fire in the HP-IP turbine oil vent tubes due to coking and carbon buildup. This fire led to a second fire in the internal air cavity below the IP turbine disk drive shaft. We are proposing this AD to prevent internal oil fires in RB211 Trent 800 series turbofan engines due to coking and carbon buildup, that could cause uncontained engine failure and damage to the airplane. 2004-12-27 2004 12 https://www.federalregister.gov/documents/2004/12/27/04-28145/airworthiness-directives-rolls-royce-plc-rb211-trent-800-series-turbofan-engines https://www.govinfo.gov/content/pkg/FR-2004-12-27/pdf/04-28145.pdf Transportation Department; Federal Aviation Administration 492,159 The FAA proposes to adopt a new airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 800 series turbofan engines. This proposed AD would require initial and repetitive borescope inspections of the high pressure-and-intermediate pressure...

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