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 6645-01-633-1852
NSN 5920-00-285-2245
NSN 5905-01-543-5824
NSN 6110-00-906-2540
NSN 6110-00-786-6169
NSN 6150-01-098-9609
NSN 6145-00-419-0550
NSN 6320-01-388-3125
NSN 5960-01-313-0681
NSN 6650-01-181-6037
NSN 5925-01-364-9184
NSN 5835-01-316-3255