Structural assembly for a gas turbine engine

A structural subassembly, which has:

• a bearing which has a statically arranged outer ring, a rotatably arranged inner ring and a plurality of rolling elements arranged therebetween, wherein the inner ring is at least one chosen from connected for conjoint rotation to a component that is rotatable about a longitudinal axis or is part of the component, wherein the longitudinal axis defines an axial direction of the bearing,
• a housing flange of a support structure, the statically arranged outer ring being connected to the housing flange,
• the outer ring including a first part and a second part, the first part including a first connecting element connected to the housing flange and the second part including a second connecting element connected to the housing flange, wherein the housing flange is arranged between the first and second connecting elements in the axial direction;
• wherein one of the first part and the second part includes an integral axially extending portion having an inner surface engaging the plurality of rolling elements and forming an outer running surface for the plurality of rolling elements.