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 5945-01-380-3876
NSN 6110-01-335-0580
NSN 7035-01-317-4227
NSN 6610-00-969-6947
NSN 5910-01-324-1567
NSN 5998-00-895-9564
NSN 6620-01-085-8688
NSN 6135-01-180-9611
NSN 6105-00-212-0592
NSN 2925-00-193-2402
NSN 5999-00-336-9147
NSN 5925-01-116-5462