AD 2000-05-12

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc RB211-524 Series Turbofan Engines

AD Number
2000-05-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2000-NE-02-AD
FR Citation
65 FR 14207

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc RB211-524 Series Airworthiness Directives; Rolls-Royce plc RB211-524 Series Turbofan Engines

Unsafe Condition

Reports of fan blade failures due to dovetail root cracks.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Initial and repetitive ultrasonic inspections for cracks in fan blade dovetail roots. Replacement with serviceable parts if necessary. Option to install improved design fan blades or rework current fan blades as terminating action.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Not specified in the provided text.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Rolls-Royce plc RB211-524 series turbofan engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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