EASA Regulations for Airbus A321-231

6 airworthiness directives and regulations affecting Airbus A321-231.

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New ADs and bulletins for Airbus A321-231, summarized like the ones below, every Monday.

EASA AD US-2024-11-03

Jun 20, 2024

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 2023-0074

Apr 5, 2023

Wings — Centre Wing Box Rear Lower Spar and Slanted Beam — Inspection

EASA Airworthiness Directive 2023-0074 is an airworthiness directive issued by EASA affecting Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, and A321-232 aeroplanes. It mandates a one-time inspection of the centre wing box rear lower spar junction area and the slanted beam connection at fuselage frame 42 to detect potential fatigue cracks. The directive aims to ensure structural integrity by addressing high fatigue stress identified during certification and stress analysis.

Airworthiness Directive
  • Airbus A321111112131211212213231232

EASA AD US-2022-02-05

Jan 12, 2022

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

The Federal Aviation Administration's Airworthiness Directive 2022-02-05 addresses certain Pratt & Whitney PW1500G and PW1900G model turbofan engines installed on aircraft such as the Airbus A321-231. This directive mandates the removal and replacement of specific high-pressure turbine (HPT) 1st-stage and 2nd-stage disks due to a risk of uncontained disk failure. The directive aims to prevent engine damage and potential loss of the airplane caused by high-energy debris from disk failures.

Airworthiness Directive
  • Pratt & Whitney PW1500G
  • Pratt & Whitney PW1900G
  • Airbus A321-231

EASA AD US-2021-14-19

Jul 22, 2021

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-2021-11-15

Jun 9, 2021

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-2021-01-03

Jan 7, 2021

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