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 6645-01-400-2119
NSN 5960-01-057-7096
NSN 6220-00-610-0968
NSN 6240-01-657-6037
NSN 5945-00-600-2527
NSN 5925-00-307-4015
NSN 6645-01-023-8020
NSN 5835-01-235-7821
NSN 5920-01-258-5775
NSN 5835-00-104-2511
NSN 5999-01-502-5532
NSN 4140-01-034-9806