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2840-01-481-8853
Aircraft Gas Turbine Engine Turbine Shroud Segment
2840014818853 014818853 3070023-4
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
2
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United States (US) 4. 2840-01-481-8853 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 2840-01-481-8853
2840-01-481-8853 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 2840-01-481-8853
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-481-8853
- Spain (YB01)
- Effective Date:
- 1 Jan 2001
- Republic of Korea (ZH01)
- Effective Date:
- 1 May 2004
Approved Sources 2840-01-481-8853
- Part Number
- Manufacturer
- Status
- 3070023-4
- Manufacturer
- 99193 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-481-8853
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- C101 Gas Turbine Engine
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Freight Information 2840-01-481-8853
2840-01-481-8853 has freight characteristics.. 2840-01-481-8853 has a variance between NMFC and UFC when transported by rail and the description should be consulted.