2840-00-115-9506

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840001159506 001159506 323727 623782

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

2840-00-115-9506 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840001159506 001159506

Managed by United States
NSN Created on 23 Sep 1968
Data Last Changed
November 2023
NATO Update Count
9
NATO Data Quality
2840-00-115-9506 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840001159506 001159506 1/1
NSN 2840-00-115-9506 (Generic Image) 1/1

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2840-00-115-9506 Related Documents Related Documents 2840-00-115-9506 5+ Documents (More...)

323727 623782 A stationary arched metal segment used to establish clearance and a seal for the tip of
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2840-00-115-9506 Demil Restrictions 2840-00-115-9506

DEMIL: A | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-00-115-9506 is a Aircraft Gas Turbine Engine Turbine Shroud Segment that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. 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.

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