AD 2000-11-10

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines

AD Number
2000-11-10
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 94-ANE-16-AD
FR Citation
65 FR 35814

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc RB211 Series Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines

Unsafe Condition

This amendment supersedes an existing airworthiness directive (AD) applicable to certain Rolls-Royce plc (R-R) RB211 series turbofan engines. That AD currently requires the removal from service of intermediate pressure (IP) compressor stage 6-7 rotor shafts that exceed reduced cyclic life limits. This amendment requires further reduction of cyclic life limits and introduction of new reduced cyclic bands for rework. This action is prompted by additional stress analysis conducted following fail...

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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