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

15 airworthiness directives and regulations affecting International Aero Engines Ag V2500-( )5.

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New ADs and bulletins for International Aero Engines Ag V2500-( )5, summarized like the ones below, every Monday.

EASA AD US-2026-17-03

[Correction] Turbine Engine - 3rd-Stage High Pressure Compressor - Replacement

The Correction to Airworthiness Directive 2026-17-03 issued by the Federal Aviation Administration (FAA) addresses certain International Aero Engines AG models V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5. This correction fixes a typographical error in paragraph (g) of the original directive related to the replacement of 3rd stage high-pressure compressor rotor blades. The directive aims to ensure continued airworthiness and safety of these turbine engines by mandating blade replacement under specified conditions.

Airworthiness Directive

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.

Airworthiness Directive

International 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.

Airworthiness Directive

International 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.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
Airbus A320neo
Airbus A321-231

EASA AD US-2022-02-09

Engine - High-Pressure Turbine Disks - Inspection / Replacement

The Federal Aviation Administration's Airworthiness Directive 2022-02-09 supersedes the previous AD 2021-11-15 and applies to International Aero Engines AG V2500 series turbofan engines, including models V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5. This directive mandates ultrasonic inspections of the high-pressure turbine (HPT) 1st-stage and 2nd-stage disks and requires replacement if defects are found. It clarifies inspection compliance times, especially for disks transferred from high-thrust to low-thrust engine models.

Airworthiness Directive

International Aero Engines Ag V2500-( )5

EASA AD US-2021-14-19

Engine - High Pressure Turbine Stage 1/2 Disks - Inspection

Federal Aviation Administration Airworthiness Directive 2021-14-19 is a final rule addressing certain International Aero Engines AG V2500 model turbofan engines installed on aircraft such as the Airbus A321-231. This directive mandates ultrasonic inspections of the high-pressure turbine (HPT) 1st-stage and 2nd-stage disks to detect potential failures that could lead to uncontained disk failure and engine damage.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
Airbus A321-231

EASA AD US-2021-11-51

[Final Rule] Engine - High Pressure Turbine Stage 1/2 Disks - Inspection

[Final Rule] Engine - High Pressure Turbine Stage 1/2 Disks - Inspection is a Federal Aviation Administration (FAA) airworthiness directive addressing certain International Aero Engines AG V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines. It mandates ultrasonic inspections of high-pressure turbine (HPT) 1st-stage and 2nd-stage disks due to an uncontained failure event that caused high-energy debris to penetrate the engine cowling. The directive aims to prevent potential engine and aircraft damage or loss resulting from similar failures.

Airworthiness Directive

International Aero Engines Ag V2500-( )5

EASA AD US-2021-11-15

Superseded by FAA AD 2022-02-09

FAA Airworthiness Directive 2021-11-15 is a final rule addressing certain International Aero Engines AG V2500 model turbofan engines installed on aircraft such as the Airbus A321-231. It mandates ultrasonic inspections of the high-pressure turbine (HPT) 1st-stage and 2nd-stage disks due to an uncontained failure event that caused high-energy debris to penetrate the engine cowling. The directive aims to ensure continued airworthiness and safety of these engines.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
Airbus A321-231

EASA AD US-2021-05-18

Engine - Diffuser Case M-Flange - Inspection

Airworthiness Directive 2021-05-18 is a final rule issued by the Federal Aviation Administration addressing International Aero Engines AG V2500 series turbofan engines, including models V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5. This directive mandates inspections of the M-flange on the diffuser case to detect cracks and requires replacement of the diffuser case M-flange if defects are found. The directive aims to ensure continued airworthiness and safety of these engine models.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
International Aero Engines Ag V2500-A1

EASA AD US-2021-01-03

Engine - High-Pressure Turbine 1st Stage and 2nd Stage Disks - Removal

The Federal Aviation Administration's Airworthiness Directive 2021-01-03 addresses certain International Aero Engines AG V2500 series turbofan engines installed on aircraft such as the Airbus A321-231. This directive mandates the removal from service of specific high-pressure turbine (HPT) 1st-stage and 2nd-stage disks due to an identified unsafe condition following an uncontained disk failure event. The AD aims to prevent potential engine failures that could lead to damage to the engine, aircraft, or loss of the airplane.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
International Aero Engines Ag V2500-A1
Airbus A321-231

EASA AD US-2020-09-03

Engine - Diffuser Case Assembly - Removal / Replacement

The FAA Airworthiness Directive 2020-09-03 is a final rule addressing International Aero Engines AG V2500 series turbofan engines with specific diffuser case assembly serial numbers. It mandates the removal and replacement of affected diffuser case assemblies to prevent potential failure. This directive applies to multiple V2500 engine models including V2500-A1, V2522-A5, V2524-A5, V2525-D5, and others.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
International Aero Engines Ag V2500-A1

EASA AD US-2020-07-51

[Final Rule] Engine - High Pressure Turbine 1st-Stage Disks - Removal

[Final Rule] Engine - High Pressure Turbine 1st-Stage Disks - Removal is a Federal Aviation Administration (FAA) airworthiness directive addressing certain International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. It mandates the removal from service of specific high-pressure turbine (HPT) 1st-stage disks due to an uncontained disk failure event on an Airbus A321-231 powered by an IAE V2533-A5 engine. This directive aims to prevent potential engine damage, aircraft damage, and loss of the airplane caused by high-energy debris from disk failure.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
Airbus A321

EASA AD US-2019-18-01

Turbine - Low-Pressure Turbine Stage 6 Disks - Replacement

The Federal Aviation Administration Airworthiness Directive 2019-18-01 is a final rule addressing certain International Aero Engines AG V2500 model turbofan engines. It targets specific low-pressure turbine (LPT) stage 6 disks identified with material anomalies that could compromise engine safety. This directive mandates the removal and replacement of affected LPT stage 6 disks to prevent potential engine failure and damage to the aircraft.

Airworthiness Directive

International Aero Engines Ag V2500-( )5

EASA AD US-2019-16-01

Engine - Turbine Exhaust Case - Inspection

The Federal Aviation Administration's Airworthiness Directive 2019-16-01 addresses all International Aero Engines AG V2525-D5 and V2528-D5 turbofan engines. This directive mandates inspections of turbine exhaust cases due to reports of cracks, aiming to prevent engine failure and potential loss of the airplane. It requires initial and repetitive inspections and replacement of affected parts if cracks are found.

Airworthiness Directive

International Aero Engines Ag V2500-( )5

EASA AD US-2019-06-06

Superseded by FAA AD 2021-05-18

FAA Airworthiness Directive 2019-06-06 is a final rule addressing all International Aero Engines AG V2500 turbofan engine models. It mandates initial and repetitive borescope inspections of the diffuser case M-flange and requires replacement of the diffuser case if cracks are detected. This directive aims to prevent uncontained diffuser case rupture that could damage the engine and aircraft.

Airworthiness Directive

International Aero Engines Ag V2500-( )5
International Aero Engines Ag V2500-A1