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 6135-01-167-7604
NSN 6105-00-565-9450
NSN 6105-01-485-1846
NSN 6150-00-455-1331
NSN 6620-01-655-7664
NSN 5835-01-085-9591
NSN 6150-01-485-0301
NSN 6220-01-153-1937
NSN 5915-00-271-2321
NSN 5999-00-174-2776
NSN 5910-00-035-5534
NSN 5998-00-541-8792