Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE

2840-01-120-1966 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: 9687M93G49, 2840-01-120-1966, 01-120-1966, 2840011201966, 011201966

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

Supply Group (FSG) NSN Assign. NIIN
28 01-120-1966

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Technical Data | NSN 2840-01-120-1966

Characteristic Specifications
DIAMETER 52.313 INCHES MINIMUM AND 52.373 INCHES MAXIMUM
CRITICALITY CODE JUSTIFICATION ABMZ AND AGAV
III END ITEM IDENTIFICATION ACFT ENG TF39
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE 9687M93G49

Restrictions/Controls & Freight Information | NSN 2840-01-120-1966

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