2835-14-518-2021

Nonaircraft Gas Turbine Engine Turbine Shroud Segment

2835145182021 145182021 RU41568

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

2835-14-518-2021 SHROUD SEGMENT,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835145182021 145182021

Managed by France
NSN Created on 26 Jan 2000
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2835-14-518-2021 SHROUD SEGMENT,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835145182021 145182021 1/1
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2835-14-518-2021 2835145182021 145182021,RU41568
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,RU41568 RU41568 A stationary arched metal segment used to establish clearance and a seal for the tip
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Gas Turbines and Jet Engines; Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and Components from France (FR)
Nonaircraft Gas Turbine Engine Compressor Rotor 156316RNCC: 3 | RNVC: 2 | DAC: 4 14 Aug 2004 2835-14-518-2021

2835-14-518-2021 Demil Restrictions 2835-14-518-2021

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

2835-14-518-2021 is a Nonaircraft Gas Turbine Engine Turbine Shroud Segment

2835-14-518-2021 End Users End Users 2835-14-518-2021

France (ZF)

2835-14-518-2021 Manufacturers Approved Sources 2835-14-518-2021

Part Number
Manufacturer
Status
RU41568
K0680 - Rolls-Royce Airlines (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 2

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