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 5905-01-609-4470
NSN 6220-01-360-2532
NSN 6240-01-351-6729
NSN 6610-01-657-1773
NSN 5990-00-296-4825
NSN 5990-01-483-7313
NSN 5910-00-088-2952
NSN 6240-00-342-9756
NSN 5945-01-298-9525
NSN 5999-00-810-0176
NSN 5935-01-493-3206
NSN 6650-01-448-4996