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 5960-01-536-9763
NSN 5965-01-350-5105
NSN 5960-01-481-8051
NSN 5855-01-481-0819
NSN 5960-01-034-2937
NSN 5935-01-455-9120
NSN 2925-00-805-6481
NSN 6130-00-939-8011
NSN 5975-01-546-0848
NSN 5925-01-549-9760
NSN 6240-01-210-1927
NSN 5999-00-309-4265