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 5999-01-515-0334
NSN 6145-01-189-7622
NSN 5965-00-333-3359
NSN 5925-00-856-8103
NSN 6130-01-605-1266
NSN 6150-00-146-9714
NSN 5915-01-048-7252
NSN 4140-01-341-1841
NSN 5915-01-589-4976
NSN 5910-00-276-8592
NSN 6150-00-771-3904
NSN 6685-01-303-6220