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 5990-01-241-9472
NSN 6650-01-406-5322
NSN 6610-01-474-4397
NSN 2925-01-121-0761
NSN 5998-01-389-7059
NSN 6650-00-597-7313
NSN 6610-00-614-7943
NSN 4140-01-420-0354
NSN 5945-01-247-0770
NSN 6320-01-353-9753
NSN 6620-01-101-4408
NSN 6685-00-552-2154