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 5910-00-845-6324
NSN 6145-01-611-1985
NSN 5910-00-168-9650
NSN 5965-01-188-7267
NSN 5855-01-610-3506
NSN 6610-00-186-8229
NSN 6105-00-156-9084
NSN 5935-01-466-0076
NSN 5960-00-341-5948
NSN 6105-01-434-8231
NSN 5996-00-237-5146
NSN 6685-00-179-9068