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 6145-01-443-3282
NSN 4140-00-715-9946
NSN 6150-00-812-1965
NSN 5996-01-367-4209
NSN 5930-00-378-7005
NSN 5950-01-627-6473
NSN 5960-00-735-8721
NSN 2925-01-101-4655
NSN 5960-00-579-0298
NSN 5960-01-265-0354
NSN 6105-01-391-5285
NSN 6320-01-225-9963