AD 2017-10-25

final rule
Data completeness: 80%

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Turbofan Engines

AD Number
2017-10-25
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-0186
FR Citation
82 FR 24236

Applicability

TypeManufacturerModelDetails
aircraft Rolls-Royce Deutschland Ltd & Co KG Turbofan Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Turbofan Engines

Unsafe Condition

Failure to replace an affected HPC stage 12 rotor disk before exceeding the revised life limits could lead to an uncontained engine failure, possibly resulting in damage to, and/or reduced control of, the aeroplane.

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

Required Actions

Recalculate the consumed and remaining service life for HPC stage 12 rotor disks P/N EU25917, P/N EU56963, P/N JR10242, and P/N JR18449. Implement the reduced life limits as necessary based on the recalculated service life.

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 Deutschland Ltd & Co KG Spey 506-14A, Spey 555-15, Spey 555-15H, Spey 555-15N, and Spey 555-15P turbofan engines with HPC stage 12 rotor disks P/N EU25917, P/N EU56963, P/N JR10242, or P/N JR18449 installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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