T.O. 2j-j85-94; 125.0 microinch finish all surfaces
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 5935-00-163-1811
NSN 5975-01-601-7464
NSN 5960-01-444-2205
NSN 5998-01-476-8968
NSN 5910-01-439-9521
NSN 5930-01-191-3761
NSN 5950-00-982-0183
NSN 5915-00-615-9537
NSN 5915-00-257-0774
NSN 6145-01-467-2396
NSN 5855-01-631-4331
NSN 6130-01-168-9768