2840-01-009-4085

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840010094085 010094085 756772 756792

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

2840-01-009-4085 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840010094085 010094085

Managed by United States
NSN Created on 11 Sep 1975
Data Last Changed
November 2023
NATO Update Count
13
NATO Data Quality
2840-01-009-4085 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840010094085 010094085 1/1
NSN 2840-01-009-4085 (Generic Image) 1/1

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2840-01-009-4085 Demil Restrictions 2840-01-009-4085

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

2840-01-009-4085 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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