AD 2015-10-04

Recurring final rule
Data completeness: 70%

Airworthiness Directives; International Aero Engines AG Turbofan Engines

AD Number
2015-10-04
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2009-1100
FR Citation
80 FR 30138

Applicability

TypeManufacturerModelDetails
aircraft International Aero Airworthiness Directives; International Aero Engines AG Turbofan Engines

Unsafe Condition

Failure of the high-pressure compressor (HPC) stage 3 to 8 drum, which could result in uncontained drum failure, 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

Perform eddy current inspection (ECI) or fluorescent penetrant inspection (FPI), and initial and repetitive ultrasonic inspections (USIs) of certain HPC stage 3 to 8 drums. Remove affected attachment nuts and any HPC stage 3 to 8 drum found cracked. Add a mandatory terminating action.

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

Compliance Time

Within the compliance times specified in the AD, which vary based on engine serial number groups.

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

Affected Aircraft

International Aero Engines AG (IAE) V2500-A1, V2525-D5, V2528-D5, and certain serial numbers of V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines.

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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