Znickel alloy ams 5665; segment subtends 180 degrees arc; 0.859 in. Min 0.869 in. Max w; 0.875 in. Min 0.895 in. Max h; honeycomb core nickel alloy ams 5540; 0.003 in. Min 0.004 in. Max thk stock which is brazed to shroud; color coded red
A stationary arched metal segment used to establish clearance and a seal for the tip of a blade, turbine rotor, aircraft gas turbine engine. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a seal ring, labyrinth, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5925-01-361-7096
NSN 6130-01-506-6422
NSN 6240-01-560-6424
NSN 7035-01-388-6943
NSN 5925-01-608-4702
NSN 5925-00-156-0680
NSN 5930-01-578-6075
NSN 6645-01-495-5553
NSN 5925-01-263-2794
NSN 5905-01-186-6796
NSN 7035-01-526-5393
NSN 6145-00-635-9957