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Airworthiness directives › 2024-06-02

AD 2024-06-02 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Previously Held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Engines

Superseded. This directive was replaced by AD 2025-18-08. Work to the current one.
2024-04-11
2024-03-27
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Engine
2025-18-08

Models named: M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S, M601F. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to GE Aviation Czech s.r.o. (GEAC) (type certificate previously held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Model M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S, and M601F engines.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Perform all required actions within the compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2024-0040-E, dated February 8, 2024 (EASA AD 2024-0040-E).

Unsafe condition

This AD was prompted by a report of a crack on the centrifugal compressor case mount pad weld area, caused by a non-conforming welding (lack of welding penetration). The FAA is issuing this AD to prevent failure of the centrifugal compressor case. The unsafe condition, if not addressed, could result in crack propagation, possibly resulting in engine separation and reduced control of the airplane.

Affected ADs

None.

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1