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 5990-01-272-4091
NSN 6150-01-278-9265
NSN 7035-01-091-7481
NSN 5985-01-600-0306
NSN 6610-01-238-8712
NSN 6220-01-441-2889
NSN 5920-01-579-5005
NSN 6110-01-032-2899
NSN 6610-00-225-9886
NSN 6610-01-359-5515
NSN 5920-01-529-6525
NSN 6620-01-423-0833