Matl steel per ams 5540; o.D. 11.44-11.52 in. Dia; center bore 1.64-1.65 in. Dia; five grommets required 0.365-0.385 in. I.D. By 0.615 in. O.D. Min
A flexible covering, fabricated from appropriate insulating materials, designed to reduce thermal radiation in the hot section of an engine, gas turbine, aircraft. see also shield, heat, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5996-01-395-2879
NSN 5975-00-249-5063
NSN 5915-01-460-7176
NSN 6150-01-429-8315
NSN 6145-00-027-5955
NSN 5895-00-192-2414
NSN 5935-00-989-7091
NSN 6130-01-047-5153
NSN 6110-01-618-5291
NSN 5855-01-406-7237
NSN 6110-01-487-6003
NSN 5998-00-060-3333