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 5975-00-593-9767
NSN 5835-01-399-5820
NSN 2925-01-170-1089
NSN 5965-01-017-8741
NSN 2925-01-022-8332
NSN 6320-01-466-4175
NSN 6645-01-018-1799
NSN 5935-01-432-0222
NSN 6685-00-522-4076
NSN 5925-01-608-3822
NSN 6240-01-214-0308
NSN 6135-00-973-5632