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 5945-01-429-0824
NSN 6610-00-331-3460
NSN 6145-00-126-1606
NSN 5835-01-442-6482
NSN 5975-00-405-8787
NSN 6650-00-401-7896
NSN 5895-00-876-9626
NSN 7035-01-633-9537
NSN 6620-00-104-5677
NSN 5996-01-327-6601
NSN 5950-00-290-8090
NSN 5999-01-432-0345