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 5960-01-449-5726
NSN 6135-00-416-2898
NSN 5950-00-081-9226
NSN 5998-01-274-0150
NSN 6610-00-468-1958
NSN 2925-00-912-3993
NSN 6645-01-633-1852
NSN 5998-01-063-6619
NSN 6150-01-006-3235
NSN 6135-00-274-4037
NSN 5910-01-334-9759
NSN 5835-01-205-6614