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 6650-00-782-4624
NSN 6150-01-120-3417
NSN 5990-00-694-4086
NSN 5925-01-634-0664
NSN 6620-00-010-8190
NSN 6650-00-726-4242
NSN 6240-00-340-6977
NSN 5895-01-604-8541
NSN 5910-00-728-9340
NSN 6240-01-115-4549
NSN 5996-00-803-6475
NSN 2925-00-215-4954