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 6320-01-216-1678
NSN 6105-00-045-3700
NSN 6150-01-497-2857
NSN 6135-01-084-1609
NSN 5835-01-350-0566
NSN 5996-00-816-9320
NSN 6220-01-570-2197
NSN 5960-00-784-6103
NSN 5930-01-447-2837
NSN 5985-00-793-5021
NSN 5925-00-769-6869
NSN 6685-01-211-6590