A rigid item designed to complete the circumference when the nozzle,augmenter exhaust,aircraft gas turbine engine is in the open position allowing the nozzle to maintain control of the hot exhaust gases. it is situated between the augmentor nozzle section,outer,aircraft gas turbine engine and the augmentor nozzle section,outer,aircraft gas turbine engine and the augmentor nozzle section,convergent,aircraft gas turbine engine; augmentor nozzle section,inner,aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5895-01-514-0010
NSN 5996-01-656-2461
NSN 5950-01-473-4708
NSN 6240-01-221-1378
NSN 6220-01-041-6559
NSN 6620-00-914-6818
NSN 5985-01-143-3798
NSN 6220-00-548-1999
NSN 6320-01-521-1764
NSN 5945-01-258-5042
NSN 5960-01-475-7428
NSN 6610-01-221-2606