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 6650-00-767-0787
NSN 6220-01-415-1541
NSN 6220-01-065-2171
NSN 5965-01-620-4741
NSN 5950-01-322-4926
NSN 4140-01-647-0707
NSN 6105-00-251-7625
NSN 6150-01-427-3764
NSN 6320-01-442-8604
NSN 5985-01-114-1969
NSN 5999-01-092-3369
NSN 5999-01-511-5049