AD 2022-10-04

final rule
Data completeness: 80%

Airworthiness Directives; Engine Alliance Turbofan Engines

AD Number
2022-10-04
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2022-0512
FR Citation
87 FR 26967

Applicability

TypeManufacturerModelDetails
engine Engine Alliance Turbofan Airworthiness Directives; Engine Alliance Turbofan Engines

Unsafe Condition

The presence of foreign material in the billet may lead to crack formations and premature failure of the HPC stage 8 rotor disk. This condition, if not addressed, could result in failure of the HPC stage 8 rotor disk, uncontained release of the HPC stage 8 rotor disk, damage to the engine, and damage to the airplane.

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

Required Actions

This AD requires the replacement of the affected stages 7-9 compressor rotor spool.

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

Engine Alliance GP7270, GP7272, and GP7277 model turbofan engines.

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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