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 6220-01-236-7825
NSN 5960-01-658-9538
NSN 7035-01-361-8821
NSN 6220-01-484-9193
NSN 5935-01-360-0657
NSN 6150-00-904-0359
NSN 6135-01-498-7945
NSN 5996-01-369-9209
NSN 5998-01-383-0567
NSN 4140-01-236-0112
NSN 6685-01-442-4985
NSN 5915-01-170-4308