EASA Regulations for International Aero Engines Ag V2500-( )5

3 airworthiness directives and regulatory documents affecting International Aero Engines Ag V2500-( )5.

EASA AD US-2025-19-13

Engine - High-Pressure Turbine 1st-stage and 2nd-stage Hubs - Replacement

The Federal Aviation Administration's Airworthiness Directive 2025-19-13 addresses certain International Aero Engines AG Model V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines. This directive mandates the removal and replacement of specific high-pressure turbine (HPT) 1st-stage and 2nd-stage hubs due to a quality escape identified during angled ultrasonic inspections. The AD aims to prevent potential uncontained failures that could lead to engine and aircraft damage.

Sep 26, 2025

Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5

EASA AD US-2025-17-16

Turbine Engine - Airworthiness Limitations Section - Revision

The Turbine Engine - Airworthiness Limitations Section - Revision is a final rule airworthiness directive issued by the FAA that applies to certain International Aero Engines AG models including V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5. This directive addresses an unsafe condition caused by an uncontained failure of a high-pressure turbine 1st-stage hub in the V2533-A5 engine. It mandates revisions to the airworthiness limitations section of maintenance manuals and inspection programs to include new inspections of critical rotating parts.

Sep 8, 2025

Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5

EASA AD US-2024-11-03

Engine - 1st-Stage Hubs and 2nd-Stage Hubs - Inspection / Replacement

The Federal Aviation Administration's Airworthiness Directive 2024-11-03 addresses certain International Aero Engines, AG Model V2500 engines installed on aircraft such as the Airbus A320neo and A321-231. This directive requires angled ultrasonic inspections and accelerated replacement of specific high-pressure turbine 1st-stage and 2nd-stage hubs due to a risk of failure caused by a nickel powdered metal anomaly. The AD aims to prevent unsafe conditions resulting from hub failures that could lead to engine shutdowns or uncontained engine debris.

Jun 20, 2024

Airworthiness DirectiveMaintenanceSafety MgmtInternational Aero Engines Ag V2500-( )5Airbus A320neoAirbus A321-231