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 5905-01-181-6359
NSN 5998-00-596-8869
NSN 6130-01-269-0500
NSN 6620-01-421-6949
NSN 6220-01-391-9531
NSN 5985-00-332-8758
NSN 6105-01-020-8339
NSN 5996-01-459-5310
NSN 6110-01-463-1100
NSN 6135-01-010-0891
NSN 5998-00-067-8102
NSN 5965-00-445-1843