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 5960-01-144-5502
NSN 5998-01-656-8287
NSN 6135-01-301-8776
NSN 5905-01-618-4274
NSN 6110-00-937-5800
NSN 5920-00-407-0310
NSN 5925-01-026-0891
NSN 7035-01-506-9957
NSN 6110-01-606-9749
NSN 5999-01-411-5135
NSN 5990-00-902-7764
NSN 5975-01-464-1826