EASA AD 2022-0113
Jun 17, 2022Engine — Stages 6-10 Compressor Rotor Spools and High Pressure Turbine Rotor Stage 1 Disks — Replacement
EASA Airworthiness Directive 2022-0113 is an airworthiness directive addressing CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. It mandates the replacement of specific compressor rotor spools (Stages 6-10) and high pressure turbine rotor stage 1 disks identified as affected parts due to potential manufacturing defects. The directive aims to ensure continued airworthiness and prevent engine part failure.
- CFM International LEAP-1A
- CFM International LEAP-1C
- Airbus A319
- Airbus A320
- Airbus A321