T.O. 2j-tf39-4; goes on the turbine mid frame; retaining liner
A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 7035-00-286-6221
NSN 4140-01-215-1125
NSN 6220-01-352-2970
NSN 6240-01-212-9756
NSN 6105-01-598-4528
NSN 6620-00-362-9460
NSN 5990-01-064-4852
NSN 5945-01-103-2980
NSN 5905-01-262-7749
NSN 5950-00-117-3949
NSN 5905-01-503-4888
NSN 5996-01-015-9539