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 6135-01-201-5858
NSN 6650-01-277-8273
NSN 5960-00-552-0517
NSN 2925-01-136-2551
NSN 5895-01-206-1834
NSN 6620-00-179-9079
NSN 5855-01-100-3272
NSN 5985-01-367-7167
NSN 5985-00-071-1401
NSN 5945-01-106-0272
NSN 5930-01-224-5795
NSN 6135-00-062-5080