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2840-01-338-1152
Aircraft Gas Turbine Engine Turbine Shroud Segment
2840013381152 013381152 6071T80P01
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
November 2023
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RQST NE Updated Every Day 2840-01-338-1152 RQST Updated Every Day 2840-01-338-1152 RQST NE Related Documents
seal for the tip of a RQST NE Updated Every Day 2840-01-338-1152 RQST Updated Every Day 2840-01-338-1152
Restrictions 2840-01-338-1152
2840-01-338-1152 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 is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. The precious metals content of this item is unknown.
Import and Export 2840-01-338-1152
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-338-1152
- Australia (ZA01)
- Effective Date:
- 1 Apr 1991
Approved Sources 2840-01-338-1152
- Part Number
- Manufacturer
- Status
- 6071T80P01
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-338-1152
- Characteristic
- Specifications
- End Item Identification [AGAV]
- Specifications
- F18 Simulator
NATO Stock Numbers Related to 2840-01-338-1152
Freight Information 2840-01-338-1152
2840-01-338-1152 has freight characteristics managed by Australia.. 2840-01-338-1152 has a variance between NMFC and UFC when transported by rail and the description should be consulted.