T.O. 2j-tf30-24; supports the combustion cans, keeps them in line and helps align the duct, combustion chamberto attach to the 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 6145-00-570-0516
NSN 5935-00-990-7671
NSN 6620-00-900-3986
NSN 6320-01-643-0850
NSN 7035-01-224-5165
NSN 6685-00-172-4242
NSN 5998-00-921-6568
NSN 6610-01-502-7820
NSN 5945-01-281-5072
NSN 2925-01-255-6394
NSN 5925-01-623-1701
NSN 5910-00-392-6822