AD Amdt-39-11446

Recurring final rule
Data completeness: 70%

Airworthiness Directives; International Aero Engines AG V2500-A1 Series Turbofan Engines

AD Number
Amdt-39-11446
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 98-ANE-76-AD Amendment 39-11446
FR Citation
64 FR 67708

Applicability

TypeManufacturerModelDetails
aircraft International Aero Airworthiness Directives; International Aero Engines AG V2500-A1 Series Turbofan Engines

Unsafe Condition

High pressure turbine (HPT) disk fracture, which could result in an uncontained engine failure and damage to the airplane.

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

Required Actions

Perform initial and repetitive ultrasonic inspections of HPT stage 1 and 2 disks for subsurface anomalies. Remove disks from service if a subsurface anomaly is found, and replace with serviceable parts. HPT stage 1 disks with specific part numbers and serial numbers may return to service following a successful inspection.

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

Compliance Time

Within the next shop visit after the effective date of this AD, regardless of the planned maintenance or the reason for engine removal.

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

Affected Aircraft

International Aero Engines AG V2500-A1 series turbofan engines, installed on but not limited to Airbus Industrie A320 series airplanes.

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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