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 6610-01-024-5360
NSN 5985-01-085-5573
NSN 5975-00-144-7878
NSN 5945-01-089-8771
NSN 5965-01-449-1101
NSN 5999-01-172-6262
NSN 5835-00-594-4921
NSN 5998-01-524-3530
NSN 6135-01-625-0233
NSN 5985-01-272-7309
NSN 6610-01-582-8181
NSN 6650-00-751-9958