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 6110-00-498-2739
NSN 5996-00-631-5001
NSN 6645-01-295-9995
NSN 5910-00-203-2119
NSN 5996-01-075-5184
NSN 5935-01-371-2568
NSN 5985-00-370-3379
NSN 5950-00-336-9088
NSN 5945-00-635-7263
NSN 5960-01-491-9916
NSN 6645-01-615-1052
NSN 6645-00-959-6502