AD 2025-02-14

Recurring final rule
Data completeness: 70%

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

AD Number
2025-02-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2024-2414
FR Citation
90 FR 10590

Applicability

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

Unsafe Condition

Reports of cracked intermediate pressure compressor (IPC) shaft assembly front air seals. Such cracking could lead to IPC stage 1 disk burst with consequent release of high energy debris and damage to the airplane or failure of the IPC front seal and release of debris, which could lead to an engine in-flight shutdown (IFSD) and in the case of a dual IFSD could result in reduced control of the airplane.

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Required Actions

Inspect the affected IPC shaft assembly for cracking and, depending on the results of the inspection, repetitive inspections or replacement of the IPC shaft assembly front air seals, as specified in EASA AD 2024-0178, which is incorporated by reference.

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Compliance Time

Within 50 flight hours

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Affected Aircraft

Rolls-Royce Deutschland Ltd & Co KG Model Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3, Trent 7000-72, and Trent 7000-72C 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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