2840-99-911-2305

Aircraft Gas Turbine Engine Turbine Shroud Segment

2840999112305 999112305 AH10404G01

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

2840-99-911-2305 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840999112305 999112305

Managed by United Kingdom
NSN Created on 17 Dec 2007
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-99-911-2305 SHROUD SEGMENT,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840999112305 999112305 1/1
NSN 2840-99-911-2305 (Generic Image) 1/1

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,AH10404G01 AH10404G01 A stationary arched metal segment used to establish clearance and a seal for the
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fsc-2840/fr 2840-14-464-6485 2840144646485 144646485,307-033-404-0 2840-14-464-6485 -921-6148 2840-99-911-2305
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2840999112305 999112305,AH10404G01 2840001159506 001159506,323727,623782 361-8861 2840-14-464-6485

2840-99-911-2305 Demil Restrictions 2840-99-911-2305

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2840-99-911-2305 is a Aircraft Gas Turbine Engine Turbine Shroud Segment

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