2835-14-518-2022

Nonaircraft Gas Turbine Engine Turbine Shroud Segment

2835145182022 145182022 RU41569

A stationary arched metal segment used to establish clearance and a seal for the tip of a BLADE, TURBINE ROTOR, NONAIRCRAFT 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, NONAIRCRAFT GAS TURBINE ENGINE. View more Nonaircraft Gas Turbine Engine Turbine Shroud Segment

2835-14-518-2022 SHROUD SEGMENT,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835145182022 145182022

Managed by France
NSN Created on 26 Jan 2000
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2835-14-518-2022 SHROUD SEGMENT,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835145182022 145182022 1/1
NSN 2835-14-518-2022 (Generic Image) 1/1

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2835145182022 145182022,RU41569 851-0358 2835-99-581-6854 2835-01-557-1998 https//www.nsnlookup.com
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ring, labyrinth, nonaircraft gas turbine engine. https//www.nsnlookup.com /fsg-28/fsc-2835/fr 2835-14-518-2022
2835145182022 145182022,RU41569 2835-14-518-2022 2835145182022 145182022 is a stationary arched
991728880,4711020724 557-1998 2835-01-691-0158 2835-01-539-1004 2835-01-620-2839 2835-01-377-6197 2835145182022
145182022,RU41569 557-1998 2835-01-691-0158 2835-01-539-1004 https//www.nsnlookup.com /fsg-28/fsc-2835
2835145182022 145182022,RU41569 557-1998 2835-01-691-0158 2835-01-539-1004 https//www.nsnlookup.com
145182022,RU41569 557-1998 2835-01-691-0158 2835-01-539-1004 01-620-2839 2835-01-377-6197 2835-01-441
999169827,RUB8422 557-1998 2835-01-691-0158 2835-01-539-1004 2835-01-620-2839 2835-01-377-6197 2835145182022
145182022,RU41569 557-1998 2835-01-691-0158 us 2835-01-362-5030 2835013625030 013625030,ND2707 851-0358

2835-14-518-2022 Demil Restrictions 2835-14-518-2022

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2835-14-518-2022 is a Nonaircraft Gas Turbine Engine Turbine Shroud Segment

2835-14-518-2022 End Users End Users 2835-14-518-2022

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