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 6620-01-373-7978
NSN 5965-01-035-4975
NSN 6320-01-513-9166
NSN 6145-01-364-7837
NSN 5835-00-368-4182
NSN 6610-01-541-5034
NSN 5895-00-585-2038
NSN 5915-00-726-1204
NSN 5935-01-335-2964
NSN 6110-00-196-0625
NSN 7035-01-513-2501
NSN 5905-00-854-3680