AD 2019-16-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | International | Aero | Airworthiness Directives; International Aero Engines AG Turbofan Engines |
Unsafe Condition
cracked turbine exhaust case (TEC)
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
perform an eddy current inspection (ECI) and high sensitivity fluorescent penetrant inspection (FPI) of the TEC front and rear mount stiffener rails for cracking indications, and depending on the results of the inspections, replace the TEC with a part eligible for installation
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 4,000 flight cycles after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
all International Aero Engines AG (IAE) V2525-D5 and V2528-D5 model turbofan engines
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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