Cres, 19.70 in. Od, 0.51 in lg
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 6105-01-611-6429
NSN 7035-00-403-5340
NSN 6105-01-117-4780
NSN 5965-01-295-4426
NSN 6110-01-185-7696
NSN 6685-01-432-9396
NSN 4140-01-198-5652
NSN 6145-00-847-4104
NSN 6105-00-753-7495
NSN 5930-00-968-4590
NSN 5998-00-168-1262
NSN 6150-01-114-6346