180 deg. 7.998-8.002 in. Id based on 360 deg; 21 slots 0.352-0.354 in. Wide by 0.477-0.481 in deep; 21 holes 0.186-0.187
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 5999-00-431-9230
NSN 5895-01-607-9952
NSN 5975-01-119-3833
NSN 6135-01-450-3781
NSN 5960-00-153-7115
NSN 5985-01-040-0903
NSN 6130-01-285-3387
NSN 6135-01-345-4866
NSN 6620-00-826-7238
NSN 5905-01-393-4413
NSN 5920-00-688-4086
NSN 5915-00-976-3704