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 6110-01-116-5057
NSN 5925-01-545-6008
NSN 5945-01-188-5268
NSN 6110-00-123-7953
NSN 5998-00-960-8513
NSN 7035-00-890-7649
NSN 5998-01-568-7716
NSN 5905-01-558-3657
NSN 2925-00-293-6543
NSN 6150-01-649-4045
NSN 6130-01-131-9369
NSN 5895-00-464-8713