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 5960-00-656-2451
NSN 6620-00-068-2503
NSN 7035-01-227-7492
NSN 6135-00-917-1894
NSN 2925-00-035-5633
NSN 6145-00-625-0714
NSN 6110-01-171-3268
NSN 6220-01-031-3263
NSN 6105-01-494-1234
NSN 5920-01-142-5750
NSN 6150-01-408-5878
NSN 6645-01-577-2306