2840-14-518-3730
Aircraft Gas Turbine Engine Turbine Shroud Segment
2840145183730 145183730 307-251-505-0
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
Managed by France
NSN Created on 2 Feb 2000
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-14-518-3730
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307-251-505-0 A stationary arched metal segment used to establish clearance and a seal for the tip of
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Restrictions 2840-14-518-3730
End Users 2840-14-518-3730
- France (ZF)
Approved Sources 2840-14-518-3730
- Part Number
- Manufacturer
- Status
- 307-251-505-0
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
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