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 5960-00-436-6269
NSN 5999-01-308-8033
NSN 6645-00-602-5968
NSN 5996-01-144-7621
NSN 5950-01-189-3194
NSN 6150-01-432-2376
NSN 6135-01-367-6203
NSN 6135-01-647-0386
NSN 4140-01-511-0286
NSN 5920-00-229-8444
NSN 4140-01-217-4783
NSN 5999-00-186-0058