AD 2000-22-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | International | Aero | Airworthiness Directives; International Aero Engines AG (IAE) V2500-A5 and -D5 Series Turbofan Engines |
Unsafe Condition
Engines assembled with an improper High Pressure Turbine (HPT) module configuration, which could cause a Low Cycle Fatigue (LCF) life reduction of the HPT stage 1 disk, potentially leading to 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
Remove engines with improper HPT module configurations from service as specified in Table 1 and restore the HPT module to type design in accordance with IAE All Operators Wire (AOW) 1053, Issue 2, dated June 20, 2000.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before accumulating 5,100 or 7,600 cycles in the improper configuration, or at the next shop visit, depending on the HPT module configuration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
International Aero Engines AG (IAE) V2500-A5 and -D5 series turbofan engines, specifically those listed by serial number in the AD, installed on Airbus Industries A319, A320, A321 series, and McDonnell Douglas MD-90 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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