AD 2002-01-29

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce, plc. Models Tay 650-15 and 651-54 Turbofan Engines

AD Number
2002-01-29
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NE-02-AD
FR Citation
67 FR 4652

Applicability

TypeManufacturerModelDetails
aircraft Rolls-Royce, plc. Models Tay 650-15 and 651-54 Turbofan Airworthiness Directives; Rolls-Royce, plc. Models Tay 650-15 and 651-54 Turbofan Engines

Unsafe Condition

Cracked HPC stage 11/12 disc spacers caused by HPC outlet guide vane (OGV) retaining bolt failure, potentially leading to an uncontained failure.

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

Required Actions

Inspect the high pressure compressor (HPC) stage 12 disc assembly using a borescope to detect damage. Replace unserviceable parts with serviceable parts. Incorporate a new design retention arrangement for the HPC OGV as a terminating action.

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

Compliance Time

Before further flight

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

Affected Aircraft

Rolls-Royce, plc models Tay 650-15 and 651-54 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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