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 5965-00-281-0319
NSN 5835-01-373-9506
NSN 5895-01-408-1462
NSN 5920-00-923-5048
NSN 4140-01-410-8938
NSN 5920-00-554-0437
NSN 6620-00-278-7313
NSN 6320-01-652-3806
NSN 5895-01-179-9693
NSN 5996-01-024-9976
NSN 5975-01-023-3081
NSN 6685-01-451-0154