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 6145-01-172-5630
NSN 5935-01-139-4403
NSN 5910-01-586-9010
NSN 5990-01-040-6358
NSN 6610-01-163-5484
NSN 6240-00-275-1950
NSN 5990-00-753-8870
NSN 6650-01-588-4687
NSN 5910-01-441-8640
NSN 5965-01-372-9578
NSN 6645-01-400-1383
NSN 6135-00-686-4777