VERFAHREN UND VORRICHTUNG ZUM WECHSELN EINER DICHTUNGSPLATTE IN EINEM FLUGZEUGTRIEBWERK

摘要

According to the present invention, there is provided a method for removing a front seal plate 11 from an aircraft engine 1, a) separating the partial engine unit 5 including the core engine 6 and the low-pressure turbine 7 of the aircraft engine 1 from the aircraft engine 1, b) removing the front seal plate nut (10) from the partial engine unit (5) and c) removing the front seal plate (11) from the partial engine unit (5). A method of removing a front seal plate from an aircraft engine is provided.