T.O. 2j-tf39-4; 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 5999-01-600-8915
NSN 6620-01-042-2046
NSN 5999-01-129-2349
NSN 5835-00-233-6327
NSN 6150-01-479-9530
NSN 2925-01-170-1089
NSN 5855-00-361-0167
NSN 2925-01-067-3096
NSN 5895-01-115-2343
NSN 5960-01-599-9821
NSN 2925-00-565-8530
NSN 5895-01-044-3825