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 6610-00-011-9991
NSN 5945-00-079-9429
NSN 5998-00-289-9092
NSN 6150-01-208-9873
NSN 6240-01-657-6037
NSN 5945-01-178-8380
NSN 5930-00-914-5620
NSN 5915-00-321-1662
NSN 6150-01-553-4097
NSN 7035-00-922-5700
NSN 6220-00-828-4209
NSN 6105-01-153-8864