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2840-01-448-3442

Aircraft Gas Turbine Engine Turbine Rotor

2840014483442 014483442 3091788-2 3091788-02

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Rotor

2840-01-448-3442 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014483442 014483442

Managed by United States
NSN Created on 27 Aug 1997
Data Last Changed
January 2023
NATO Update Count
5
NATO Data Quality
2840-01-448-3442 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014483442 014483442 1/1
NSN 2840-01-448-3442 (Generic Image) 1/1

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2840-01-448-3442 Related Documents Related Documents 2840-01-448-3442 1+ Documents (More...)

3091788-2 3091788-02 A single or multistage assembly designed to receive thermal energy from the combustion
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2840-01-448-3442 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-448-3442

2840-01-448-3442 Demil Restrictions 2840-01-448-3442

DEMIL: A | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

2840-01-448-3442 is a Aircraft Gas Turbine Engine Turbine Rotor that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-448-3442 HTS and ScheduleB Import and Export 2840-01-448-3442

2840-01-448-3442 End Users End Users 2840-01-448-3442

Taiwan, Province of China (YE01)
Effective Date:
1 Feb 2015

2840-01-448-3442 Manufacturers Approved Sources 2840-01-448-3442

2840-01-448-3442 Technical Data Datasheet 2840-01-448-3442

Characteristic
Specifications
FIIG
A10700
Design Type [APGF]
Axial Compressor
Engine Section Location [CZBJ]
High Pressure Turbine
Criticality Code Justification [CRTL]
Agav
End Item Identification [AGAV]
Acft Eng Pacer Dawn
Part Name Assigned By Controlling Agency [CXCY]
Turbine Rotor Assembly Hpt

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2840-01-448-3442 Freight Data Freight Information 2840-01-448-3442

2840-01-448-3442 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-448-3442 has a variance between NMFC and UFC when transported by rail and the description should be consulted.