T.O. 2j-f108-4; high pressure turbine shroud and 1st stage l.P. Turbine nozzle; u-shaped clips
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 5975-01-260-7968
NSN 4140-01-392-4664
NSN 5985-01-264-5467
NSN 5998-01-517-0924
NSN 5998-01-481-3907
NSN 5935-01-094-6780
NSN 5925-01-182-3286
NSN 6220-01-299-6790
NSN 5835-00-987-9341
NSN 5965-00-518-0958
NSN 5855-01-642-7607
NSN 6320-01-618-7800