EASA AD 2022-0009R1
Engine — High Pressure Turbine Rotor Stage 1 Blade — Inspection
EASA Airworthiness Directive 2022-0009R1 is an updated safety directive addressing inspection requirements for high pressure turbine rotor stage 1 blades on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive mandates repetitive borescope inspections of specific turbine blades to detect cracks and prevent potential in-flight engine failures. It applies to multiple LEAP-1A engine variants and specifies affected part numbers for inspection.