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 6320-01-458-1853
NSN 6620-00-955-6122
NSN 6320-00-116-3658
NSN 5930-01-026-0597
NSN 5985-01-227-2646
NSN 2925-01-156-9570
NSN 6685-00-446-9272
NSN 6610-01-281-7536
NSN 6220-00-260-9390
NSN 5965-01-643-1951
NSN 7035-01-151-0265
NSN 5965-00-791-0964