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 6610-00-222-1393
NSN 5920-00-057-5934
NSN 6145-01-442-6436
NSN 6685-00-628-5305
NSN 5835-01-228-8666
NSN 5905-01-571-6499
NSN 7035-00-922-5700
NSN 6320-00-674-1361
NSN 5920-00-670-4674
NSN 5895-01-168-9635
NSN 5915-01-244-6629
NSN 5950-00-391-8663