AD 2019-21-51

final rule
Data completeness: 70%

Airworthiness Directives; General Electric Company Turbofan Engines

AD Number
2019-21-51
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2019-0894
FR Citation
84 FR 64195

Applicability

TypeManufacturerModelDetails
engine General Electric Company Airworthiness Directives; General Electric Company Turbofan Engines

Unsafe Condition

An uncontained high-pressure turbine (HPT) failure, resulting in an aborted takeoff and debris penetrating the airplane's fuselage and the other engine.

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

Required Actions

Remove the Interstage Seal, part number 2505M72P01, from the affected engines.

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

Compliance Time

Within 25 flight cycles from the effective date of this AD.

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

Affected Aircraft

GE GE90-115B model turbofan engines with certain engine serial numbers.

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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