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 7035-01-227-2546
NSN 5855-01-221-4076
NSN 6105-01-460-5496
NSN 5925-01-578-8889
NSN 5999-01-098-7403
NSN 5925-00-882-2892
NSN 5998-00-759-8159
NSN 6620-01-077-7364
NSN 6610-00-262-9146
NSN 5999-01-123-8286
NSN 6610-01-489-0071
NSN 5998-00-618-0235