AD 2020-01-55

final rule
Data completeness: 80%

Airworthiness Directives; General Electric Company Turbofan Engines

AD Number
2020-01-55
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2020-0063
FR Citation
85 FR 8386

Applicability

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

Unsafe Condition

An uncontained high-pressure turbine (HPT) failure that resulted in an aborted takeoff, which could result in uncontained HPT failure, release of high-energy debris, damage to the engine, damage to the airplane, and possible loss of the airplane.

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

Required Actions

Remove from service the interstage seal, part number 2505M72P01 or 2448M33P01, from the affected engines.

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

Compliance Time

Within 5 flight cycles from the effective date of AD 2020-01-55.

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

Affected Aircraft

General Electric Company (GE) GE90-110B1 and 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 4, 2026

Rights: U.S. Government Public Domain

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