T.O. 2j-tf39-4; goes on the turbine nozzle assembly
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 6220-01-630-5354
NSN 6645-01-509-3221
NSN 5998-01-494-6651
NSN 6620-01-015-2470
NSN 2925-01-345-5463
NSN 5915-01-271-3028
NSN 6135-01-264-7261
NSN 5835-01-485-0210
NSN 5998-01-162-5250
NSN 5999-00-449-7860
NSN 5920-01-271-9140
NSN 6685-00-160-1313