EASA AD 2026-0143
Engine – Intermediate Pressure Compressor Shaft Assembly / Front Air Seal – Inspection
The document titled 'Engine – Intermediate Pressure Compressor Shaft Assembly / Front Air Seal – Inspection' is a technical directive concerning Rolls-Royce Deutschland Ltd & Co KG Trent 1000 and Trent 7000 engine models. It addresses inspection requirements for the intermediate pressure compressor shaft assembly and the front air seal components. This directive is intended to ensure the continued airworthiness and safety of affected engines installed on various aircraft.