Airworthiness Directives; Rolls-Royce plc RB211-524 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 2000-03-16 · Effective 2000-03-31 · 65 FR 14207
Document
Document number
00-5891
Federal Register citation
65 FR 14207
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Rolls-Royce plc RB211-524 Series Turbofan
Publication date
2000-03-16
Effective date
2000-03-31
FAA docket
Docket No. 2000-NE-02-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Rolls-Royce plc RB211-524 series turbofan engines. This action requires initial and repetitive ultrasonic inspections for cracks in fan blade dovetail roots, and, if necessary, replacement with serviceable parts. This action also provides the options of installing improved design fan blades or reworking current fan blades to the improved configuration as terminating action for the inspections. This amendment is prompted by reports of fan blade failures due to dovetail root cracks. The actions specified in this AD are intended to prevent possible multiple fan blade failures, which could result in an uncontained engine failure and damage to the aircraft.