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 5930-00-362-6737
NSN 6105-01-394-5305
NSN 5965-01-376-9305
NSN 5905-01-645-4813
NSN 5835-00-707-6266
NSN 6620-01-641-8741
NSN 5855-01-222-1242
NSN 5910-01-063-9911
NSN 4140-00-827-1821
NSN 6320-00-701-0437
NSN 5950-01-051-9447
NSN 6320-00-139-1090