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 6110-01-400-4207
NSN 5950-01-209-3822
NSN 5999-01-221-1935
NSN 6320-01-352-5653
NSN 6145-01-108-2617
NSN 4140-00-122-6422
NSN 5920-00-156-9230
NSN 5895-00-452-0333
NSN 5935-01-403-2844
NSN 5855-01-350-5131
NSN 5998-01-529-6739
NSN 6620-00-946-4864