2840-21-846-5206

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840218465206 218465206

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

2840-21-846-5206 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218465206 218465206

Managed by Canada
Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-21-846-5206 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840218465206 218465206 1/1
NSN 2840-21-846-5206 (Generic Image) 1/1

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2840-21-846-5206 Demil Restrictions 2840-21-846-5206

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-21-846-5206 is a Aircraft Gas Turbine Engine Turbine Shroud Segment

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