Product Details | AIRCRAFT GAS TURBINE ENGIN TURBINE NOZZLE ASSEMBLY

2840-01-224-2158 A 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. The assembled item forms a complete circle.

Part Alternates: 9687M93G53, 2840-01-224-2158, 01-224-2158, 2840012242158, 012242158

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

Supply Group (FSG) NSN Assign. NIIN
28 01-224-2158

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Technical Data | NSN 2840-01-224-2158

Characteristic Specifications
SPECIAL FEATURES FOR STAGE 1
CRITICALITY CODE JUSTIFICATION FEAT AND AGAV
III END ITEM IDENTIFICATION ACFT.ENG. TF39
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE 9687M93G53

Restrictions/Controls & Freight Information | NSN 2840-01-224-2158

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