22.300-23.540 in. Radius up to the thermal coating
An item designed to sustain flame and assist combustion stability in the conbustion section of a turbine engine afterburner by creating turbulence which provides even fuel and air mixture to assure continuous burnig.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5920-01-351-5536
NSN 5930-00-530-5193
NSN 5985-00-627-9001
NSN 5990-01-251-7313
NSN 5999-01-014-0872
NSN 5835-01-447-2544
NSN 5990-01-579-2711
NSN 4140-01-100-1223
NSN 5835-01-555-8963
NSN 6320-01-299-6367
NSN 6145-00-824-8522
NSN 6110-01-517-7905