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2840-01-347-2185
Aircraft Gas Turbine Engine Turbine Disk
2840013472185 013472185 3097000-2
An item having provisions on the outer periphery for attaching a designated number of BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Disk
January 2023
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Restrictions 2840-01-347-2185
2840-01-347-2185 is a Aircraft Gas Turbine Engine Turbine Disk 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.
Import and Export 2840-01-347-2185
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-347-2185
- Taiwan, Province of China (YE01)
- Effective Date:
- 1 Feb 2015
Approved Sources 2840-01-347-2185
- Part Number
- Manufacturer
- Status
- 3097000-2
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-347-2185
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Pacer Dawn
- Criticality Code Justification [CRTL]
- Agav
- Engine Section Location [CZBJ]
- Low Pressure Turbine
- Material [MATT]
- Steel Disk
- Material Document And Classification [MDCL]
- Ems55424 Assn Std Single Material Response Disk
- Overall Length [ABHP]
- 3.160 Inches Minimum And 3.180 Inches Maximum
NATO Stock Numbers Related to 2840-01-347-2185
Freight Information 2840-01-347-2185
2840-01-347-2185 has freight characteristics managed by the Department of Energy (DOE).. 2840-01-347-2185 has a variance between NMFC and UFC when transported by rail and the description should be consulted.