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 5945-01-353-2220
NSN 5975-01-232-1007
NSN 5965-01-481-2422
NSN 5965-01-631-6307
NSN 5985-01-433-5992
NSN 5975-01-083-4845
NSN 6240-01-633-9357
NSN 5990-01-344-9118
NSN 2925-01-660-0669
NSN 5935-01-024-3529
NSN 5999-01-425-6748
NSN 5925-00-405-3363