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 5905-00-376-1771
NSN 6105-01-284-5516
NSN 5835-00-494-8419
NSN 6220-00-994-1792
NSN 5905-00-131-9729
NSN 5985-00-909-7195
NSN 6150-00-898-3267
NSN 6145-01-322-0489
NSN 6105-01-603-5263
NSN 6145-01-548-2967
NSN 6685-00-014-6081
NSN 5905-01-558-3657