Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT

2840-00-896-4124 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.

Part Alternates: 2840-00-896-4124, 00-896-4124, 2840008964124, 008964124

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 00-896-4124

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Technical Data | NSN 2840-00-896-4124

Characteristic Specifications
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION COMPRESSOR
SPECIAL FEATURES T.O. 2J-J75-4; COMPRESSOR-VANE,OUTER; CASE DIFFUSER; SUPPORTS FUEL MANIFOLD
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION J75 AIRCRAFT ENGINE
MANUFACTURERS CODE 77445
DESIGN CONTROL REFERENCE 423065

Restrictions/Controls & Freight Information | NSN 2840-00-896-4124

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Category Code Description
No Freight Information