Strainer assembly for an aircraft engine oil system

An engine oil system for an aircraft engine, the engine oil system comprising:

• a conduit forming a portion of an oil flow path through the engine oil system, the conduit including a first conduit body and a second conduit body, the first conduit body mounted to the second conduit body at a flange interface, the first conduit body and the second conduit body forming an internal passage of the conduit for the oil flow path;
• and
• a strainer assembly disposed within the conduit at the flange interface, the strainer assembly including a tubular body, a first packing ring, a second packing ring, and a strainer member, the tubular body extending between and to a first axial end and a second axial end, the tubular body further forming the internal passage between the first axial end and the second axial end, the first axial end disposed within the first conduit body, the second axial end disposed at the second conduit body, the first packing ring and the second packing ring disposed at the tubular body and isolating the flange interface from fluid communication with the internal passage, the strainer member mounted to the tubular body within the oil flow path.