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2840-01-364-4448

Aircraft Gas Turbine Engine Compressor Vane

2840013644448 013644448 3091326-14

A component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction. View more Aircraft Gas Turbine Engine Compressor Vane

2840-01-364-4448 VANE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840013644448 013644448

Managed by United States
NSN Created on 19 Sep 1992
Data Last Changed
January 2023
NATO Update Count
8
NATO Data Quality
2840-01-364-4448 VANE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840013644448 013644448 1/1
NSN 2840-01-364-4448 (Generic Image) 1/1

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2840-01-364-4448 Related Documents Related Documents 2840-01-364-4448 1+ Documents (More...)

3091326-14 A component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
RQST NE Updated Every Day 2840-01-364-4448 RQST Updated Every Day 2840-01-364-4448 RQST NE Related Documents
2840-01-364-4448 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-364-4448

2840-01-364-4448 Demil Restrictions 2840-01-364-4448

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

2840-01-364-4448 is a Aircraft Gas Turbine Engine Compressor Vane 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.

2840-01-364-4448 HTS and ScheduleB Import and Export 2840-01-364-4448

2840-01-364-4448 End Users End Users 2840-01-364-4448

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

2840-01-364-4448 Manufacturers Approved Sources 2840-01-364-4448

2840-01-364-4448 Technical Data Datasheet 2840-01-364-4448

Characteristic
Specifications
FIIG
A10700
Criticality Code Justification [CRTL]
Agav
Design Type [APGF]
Axial Compressor
End Item Identification [AGAV]
Tfe1042-70 Turbo-Fan Engine
Engine Section Location [CZBJ]
Compressor
Material [MATT]
Steel Overall
Overall Length [ABHP]
1.358 Inches Minimum And 1.381 Inches Maximum
Special Features [FEAT]
Vane,Compressor,2Nd Stage
Stage Number [CZCJ]
2

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2840-01-364-4448 Freight Data Freight Information 2840-01-364-4448

2840-01-364-4448 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-364-4448 has a variance between NMFC and UFC when transported by rail and the description should be consulted.