Matlinconel foil per ams 5540, 0.0025 in. Min 0.0035 in. Max thk w/thermal insulation, 7.700 in. Min 7.750 in. Max o/l lg, 4.700 in. Min 0.750 in. Max o/a w
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 6105-01-152-2800
NSN 5945-01-622-1988
NSN 5990-01-487-0871
NSN 5930-01-415-5103
NSN 6620-00-128-3201
NSN 5910-01-088-0879
NSN 5975-01-532-7450
NSN 6220-01-197-7680
NSN 6130-00-291-4877
NSN 5990-00-574-4301
NSN 5855-01-439-1838
NSN 5990-01-395-4194