2840-15-207-0122

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840152070122 152070122 6068T35G16 (241)A34606068T35G16

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

2840-15-207-0122 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840152070122 152070122

Managed by Italy
NSN Created on 8 Aug 2012
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-15-207-0122 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840152070122 152070122 1/1
NSN 2840-15-207-0122 (Generic Image) 1/1

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6068T35G16 (241)A34606068T35G16 A stationary arched metal segment used to establish clearance and a
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152070122,6068T35G16 6068T35G16 (241)A34606068T35G16 A stationary arched metal segment used to establish

2840-15-207-0122 Demil Restrictions 2840-15-207-0122

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2840-15-207-0122 is a Aircraft Gas Turbine Engine Turbine Shroud Segment

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