T.O. 2j-tf30-24; attaches to the support, combustion chamber and to the combustion cans
A cylindrical shaped item or a segment thereof designed to direct air into or around a chamber, combustion, aircraft gas turbine engine. The internal iar is divided and directed to the burning chamber(s). The external air is used for cooling purposes.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6610-00-903-6095
NSN 6610-01-309-1930
NSN 5920-00-233-7366
NSN 6620-01-236-6290
NSN 5996-01-645-9422
NSN 5835-00-894-7374
NSN 5975-01-342-6061
NSN 5935-01-142-2930
NSN 5999-00-264-9504
NSN 5999-01-419-6983
NSN 6610-01-010-4516
NSN 5895-00-437-8187