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2840-01-510-1825
Aircraft Gas Turbine Engine Turbine Nozzle Assembly
2840015101825 015101825 5035T26G03
A 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. The assembled item forms a complete circle. View more Aircraft Gas Turbine Engine Turbine Nozzle Assembly
January 2023
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Restrictions 2840-01-510-1825
2840-01-510-1825 is a Aircraft Gas Turbine Engine Turbine Nozzle Assembly that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 2840-01-510-1825
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-510-1825
- Spain (YB01)
- Effective Date:
- 1 Jul 2003
Approved Sources 2840-01-510-1825
- Part Number
- Manufacturer
- Status
- 5035T26G03
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-510-1825
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Cold Section Module Ct7 Turboprop
- Part Name Assigned By Controlling Agency [CXCY]
- Air Nozzle Assembly, No. 1 Bearing
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Freight Information 2840-01-510-1825
2840-01-510-1825 has freight characteristics.. 2840-01-510-1825 has a variance between NMFC and UFC when transported by rail and the description should be consulted.