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2840-01-481-6644
Aircraft Gas Turbine Engine Turbine Shroud Segment
2840014816644 014816644 6047T94G03
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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RQST NE Updated Every Day 2840-01-481-6644 RQST Updated Every Day 2840-01-481-6644 RQST NE Related Documents
Datasheet Management RQST NE Updated Every Day 2840-01-481-6644 RQST Updated Every Day 2840-01-481-6644
Restrictions 2840-01-481-6644
2840-01-481-6644 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. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-481-6644
- Schedule B
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- HTS Code
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End Users 2840-01-481-6644
- Denmark (ZS01)
- Effective Date:
- 1 Jan 2001
Approved Sources 2840-01-481-6644
- Part Number
- Manufacturer
- Status
- 6047T94G03
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-481-6644
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Cf 34 Aircraft Engine
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Freight Information 2840-01-481-6644
2840-01-481-6644 has freight characteristics.. 2840-01-481-6644 has a variance between NMFC and UFC when transported by rail and the description should be consulted.