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2840-01-418-2158
Aircraft Gas Turbine Engine Turbine Case And Nozzle Assembly
2840014182158 014182158 4000T02G10
A NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE with a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Case And Nozzle Assembly
January 2023
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Related Documents 2840-01-418-2158 1+ Documents (More...)
RQST NE Updated Every Day 2840-01-418-2158 RQST Updated Every Day 2840-01-418-2158 RQST NE Related Documents
(3), TURBINE, AIRCRAFT RQST NE Updated Every Day 2840-01-418-2158 RQST Updated Every Day 2840-01-418-
Restrictions 2840-01-418-2158
2840-01-418-2158 is a Aircraft Gas Turbine Engine Turbine Case And Nozzle Assembly that does not have a nuclear hardened feature or any other critical feature 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 2840-01-418-2158
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-418-2158
- Spain (YB01)
- Effective Date:
- 1 Aug 1995
Approved Sources 2840-01-418-2158
- Part Number
- Manufacturer
- Status
- 4000T02G10
- Manufacturer
- 76823 - Northrop Grumman Systems Corporation (Active)
- Original Design
- Original Design
- 4000T02G10
- 0JRC1 - Northrop Grumman Technical Services, (Active)
- Advisory Reference
- Advisory Reference
Datasheet 2840-01-418-2158
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- F-5 Acft
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Freight Information 2840-01-418-2158
2840-01-418-2158 has freight characteristics.. 2840-01-418-2158 has a variance between NMFC and UFC when transported by rail and the description should be consulted.