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 6130-00-978-9984
NSN 5965-01-490-6704
NSN 5930-01-224-7004
NSN 2925-00-977-9956
NSN 6240-00-353-5753
NSN 5998-01-523-6019
NSN 6220-00-411-1137
NSN 5930-01-395-8692
NSN 7035-01-357-3726
NSN 5996-00-136-1240
NSN 6105-01-289-8025
NSN 5920-01-197-4143