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 5915-00-089-8063
NSN 5925-01-371-0646
NSN 6130-00-153-1338
NSN 6150-01-014-9231
NSN 6130-00-470-8589
NSN 5998-01-386-6122
NSN 5910-01-564-4903
NSN 6150-00-421-8774
NSN 5990-01-293-4817
NSN 5998-00-468-7998
NSN 6110-00-766-0886
NSN 6645-01-534-5545