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 5930-00-244-2742
NSN 5935-01-622-7800
NSN 6610-01-048-2870
NSN 5998-01-644-9463
NSN 6105-01-494-3848
NSN 5960-01-364-1318
NSN 6620-01-227-4380
NSN 5965-01-187-0941
NSN 2925-01-517-8544
NSN 5960-00-512-9121
NSN 6685-01-618-7131
NSN 5855-01-054-9014