2840-12-028-7042

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840120287042 120287042

Cancelled - Replaced by NSN 2840-00-489-1652

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

2840-12-028-7042 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840120287042 120287042

Managed by Germany
Data Last Changed
January 2024
NATO Update Count
1
NATO Data Quality
2840-12-028-7042 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840120287042 120287042 1/1
NSN 2840-12-028-7042 (Generic Image) 1/1

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2840120287042 120287042 Gas Turbine Engine Turbine Shroud Segment2840120287042 120287042 Cancelled
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Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Germany (DE)
-042-1504 Eye Bolt 2840-12-095-1684 Sleeve Bearing Half 2840-12-095-1682 Toroid Sealing Ring 2840-12-028-7042

2840-12-028-7042 Demil Restrictions 2840-12-028-7042

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

2840-12-028-7042 is a Aircraft Gas Turbine Engine Turbine Shroud Segment

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