Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE

2840-01-016-3859 A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.

Part Alternates: 5025T38G09, 5025T38G10, 2840-01-016-3859, 01-016-3859, 2840010163859, 010163859

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

Supply Group (FSG) NSN Assign. NIIN
28 01-016-3859

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Technical Data | NSN 2840-01-016-3859

Characteristic Specifications
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION ENGINE,ACFT,TURBOFAN,MODEL NO. T34-GE-100
MANUFACTURERS CODE 99207
DESIGN CONTROL REFERENCE 5025T38G10

Restrictions/Controls & Freight Information | NSN 2840-01-016-3859

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