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2840-01-345-4796

Aircraft Gas Turbine Engine Turbine Shaft

2840013454796 013454796 3097269-3

An item designed to transfer rotary motion from a ROTARY, TURBINE, AIRCRAFT GAS TURBINE ENGINE to a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE. It may include the HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may include provisions for mounting bearings and/or seals. View more Aircraft Gas Turbine Engine Turbine Shaft

2840-01-345-4796 SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013454796 013454796

Managed by United States
NSN Created on 19 Sep 1991
Data Last Changed
January 2023
NATO Update Count
9
NATO Data Quality
2840-01-345-4796 SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840013454796 013454796 1/1
NSN 2840-01-345-4796 (Generic Image) 1/1

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United States (US) 4. 2840-01-345-4796 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-345-4796 Demil Restrictions 2840-01-345-4796

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

2840-01-345-4796 is a Aircraft Gas Turbine Engine Turbine Shaft 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.

2840-01-345-4796 HTS and ScheduleB Import and Export 2840-01-345-4796

2840-01-345-4796 End Users End Users 2840-01-345-4796

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

2840-01-345-4796 Manufacturers Approved Sources 2840-01-345-4796

2840-01-345-4796 Technical Data Datasheet 2840-01-345-4796

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
Pacer Dawn
Criticality Code Justification [CRTL]
Agav
Diameter [ABMZ]
2.460 Inches Minimum And 2.470 Inches Maximum
Engine Section Location [CZBJ]
Fan
Material [MATT]
Steel Shaft
Overall Length [ABHP]
11.006 Inches Minimum And 11.016 Inches Maximum
Special Features [FEAT]
Internal Spline Data: 39 Teeth; Pressure Angle 20 Degrees
Surface Treatment Document And Classification [STDC]
Ams2488 Assn Std Single Treatment Response Shaft
Surface Treatment [SFTT]
Anodize Shaft

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2840-01-345-4796 Freight Data Freight Information 2840-01-345-4796

2840-01-345-4796 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-345-4796 has a variance between NMFC and UFC when transported by rail and the description should be consulted.