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 5910-00-212-5969
NSN 6135-00-078-9931
NSN 7035-01-518-4418
NSN 5895-01-320-2175
NSN 6135-01-390-7364
NSN 6135-01-077-5705
NSN 5925-00-050-8501
NSN 6240-01-381-1072
NSN 6130-01-571-7700
NSN 6130-01-400-6123
NSN 6110-00-895-0826
NSN 6130-01-351-5436