T.O. 2j-f100-4; goes on the augmentor convergent nozzle segment; metallic hardness dph 353 min or equivalent
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 2925-00-707-6770
NSN 6150-00-428-6494
NSN 6220-01-051-2989
NSN 6240-00-886-6615
NSN 5910-01-043-5265
NSN 5998-01-567-4006
NSN 5998-01-006-0186
NSN 5996-00-466-7857
NSN 2925-01-624-5647
NSN 5915-01-511-6546
NSN 5935-01-518-1579
NSN 6610-01-149-1465