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 6645-00-204-4100
NSN 5985-01-450-8230
NSN 6110-01-660-8979
NSN 5935-00-192-9618
NSN 5996-01-045-9105
NSN 5895-01-255-5934
NSN 6150-01-178-5926
NSN 5905-01-509-7518
NSN 5985-00-477-7891
NSN 5905-01-565-4961
NSN 6685-00-572-0771
NSN 6620-01-577-6285