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 6145-01-315-7356
NSN 6150-01-445-6602
NSN 5895-01-464-4745
NSN 5990-01-546-1649
NSN 6105-01-443-9028
NSN 6145-00-088-0404
NSN 5910-00-699-6391
NSN 4140-00-072-8692
NSN 5935-01-200-0830
NSN 5985-00-526-3469
NSN 5920-01-323-4525
NSN 6620-00-498-7781