AD 2016-19-05

final rule
Data completeness: 70%

Airworthiness Directives; International Aero Engines AG Turbofan Engines

AD Number
2016-19-05
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2016-5392
FR Citation
81 FR 65265

Applicability

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

Unsafe Condition

Failure of the high-pressure turbine (HPT) stage 2 seals, caused by blockage of the No. 4 bearing seal seat's anti-weep circuit, leading to uncontained HPT seal release, 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

Remove the HPT No. 4 bearing front seal seat, part numbers 2A0066, 2A1998, and 2A3432, and the HPT No. 4 bearing rear seal seat, part numbers 2A0067, 2A1999, and 2A3433, and replace them with parts eligible for installation. Inspect the HPT rotor and stator assembly, and replace them with eligible parts if necessary.

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

International Aero Engines AG (IAE) V2500-A1 turbofan engines with specific serial numbers processed using methods susceptible to seal seat oil blockage.

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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