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 6220-00-078-6021
NSN 6610-01-254-4196
NSN 5835-00-269-2232
NSN 5996-00-466-9781
NSN 5945-01-435-8204
NSN 5998-00-615-9251
NSN 5985-00-318-7879
NSN 6110-01-447-2770
NSN 6240-01-254-6019
NSN 6620-01-330-8802
NSN 5915-00-853-3962
NSN 5895-01-491-5738