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2840-01-522-9814
Aircraft Gas Turbine Engine Turbine Shroud Segment
2840015229814 015229814 5066T16G11
A stationary arched metal segment used to establish clearance and a seal for the tip of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a SEAL RING, LABYRINTH, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Shroud Segment
January 2023
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Restrictions 2840-01-522-9814
2840-01-522-9814 is a Aircraft Gas Turbine Engine Turbine Shroud Segment 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 2840-01-522-9814
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-522-9814
- Spain (YB01)
- Effective Date:
- 1 Aug 2004
Approved Sources 2840-01-522-9814
- Part Number
- Manufacturer
- Status
- 5066T16G11
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-522-9814
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- Special Features [FEAT]
- R125 Equiax Material
- End Item Identification [AGAV]
- Cn-235 Transport Aircraft
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Freight Information 2840-01-522-9814
2840-01-522-9814 has freight characteristics.. 2840-01-522-9814 has a variance between NMFC and UFC when transported by rail and the description should be consulted.