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 5910-01-123-9850
NSN 6105-01-044-5907
NSN 5990-00-432-0649
NSN 5895-00-878-1288
NSN 5996-01-449-0666
NSN 5998-01-555-0177
NSN 5996-01-534-4963
NSN 5895-01-121-8716
NSN 5895-00-636-4842
NSN 5835-01-535-0948
NSN 6650-01-513-2644
NSN 2925-01-054-3190