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 5999-00-086-3585
NSN 5960-00-302-5754
NSN 6240-01-232-4408
NSN 6645-00-106-0140
NSN 4140-01-580-3291
NSN 6110-01-439-1365
NSN 6220-01-634-0660
NSN 5935-01-578-0613
NSN 5935-01-634-0668
NSN 5915-01-194-3652
NSN 5930-01-155-1597
NSN 6150-01-571-7881