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 6105-01-365-9476
NSN 5855-00-586-6255
NSN 5895-00-873-2626
NSN 6610-01-582-6098
NSN 6130-01-634-0603
NSN 2925-01-170-1089
NSN 6240-01-027-4751
NSN 6130-01-069-5689
NSN 5930-00-418-4972
NSN 5905-01-408-4572
NSN 5905-00-358-1512
NSN 5965-01-621-6012