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 5960-01-579-1661
NSN 6650-00-316-4889
NSN 5965-01-032-9146
NSN 4140-00-985-0182
NSN 6620-01-329-6497
NSN 6240-01-078-0351
NSN 5835-01-116-2369
NSN 5965-01-295-9842
NSN 5925-01-189-7268
NSN 7035-01-449-4668
NSN 5945-01-245-8635
NSN 6130-01-306-9201