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 5975-01-201-2909
NSN 6130-01-508-7732
NSN 5920-00-288-5849
NSN 5975-01-205-1074
NSN 6610-01-653-8859
NSN 5835-01-106-1456
NSN 5975-00-167-4898
NSN 6620-00-435-8295
NSN 5945-01-358-8820
NSN 5920-01-132-9395
NSN 6645-00-925-3857
NSN 6110-00-770-2625