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2840-01-629-0833

Aircraft Turbine Engine Turbine Blade Damper

2840016290833 016290833 A3363-5

A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also acts as a seal. It may be of various shapes and cross sections. View more Aircraft Turbine Engine Turbine Blade Damper

2840-01-629-0833 DAMPER,TURBINE BLADE,AIRCRAFT TURBINE ENGINE 2840016290833 016290833

Managed by United States
NSN Created on 18 Jun 2014
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
2840-01-629-0833 DAMPER,TURBINE BLADE,AIRCRAFT TURBINE ENGINE 2840016290833 016290833 1/1
NSN 2840-01-629-0833 (Generic Image) 1/1

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2840-01-629-0833 Related Documents Related Documents 2840-01-629-0833 4+ Documents (More...)

,A3363-5 United States (US) 4. 2840-01-629-0833 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-629-0833 RQST Updated Every Day 2840-01-629-0833 RQST NE Restrictions
Blade Damper2840016290833 016290833 A3363 (Active) Primary Buy RNCC 3 RNVC 2 DAC 3 A3363-5 D0272 - Rolls-Royce
2840016290833 016290833,A3363-5 Account Upgrade 2840-01-629-0833Aircraft Turbine Engine Turbine
Blade Damper2840016290833 016290833 A3363 Bouchon Avec Anode 5340143327228143327228 7937Corrosion Preventive
Anode5340142957937 142957937 A3363 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-629-0833 2840016290833016290833
www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-629 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-629-0833
2840016290833 016290833,A3363-5 -332-7228 Bouchon Avec Anode 5340143327228 143327228 7937Corrosion
Preventive Anode5340142957937 142957937 143327228 A3363 ) Primary Buy RNCC 3 RNVC 2 DAC 3 A3363-5 7937Corrosion
2602Corrosion Preventive Anode5340144042602 144042602 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-629-0833
2840016290833 016290833,A3363-5 Account Upgrade 2840-01-629-0833Aircraft Turbine Engine Turbine
Blade Damper2840016290833 016290833 A3363 https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-629-0833

2840-01-629-0833 Demil Restrictions 2840-01-629-0833

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-629-0833 is a Aircraft Turbine Engine Turbine Blade Damper that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-629-0833 End Users End Users 2840-01-629-0833

United Kingdom (ZK01)
Effective Date:
1 Jun 2014

2840-01-629-0833 Manufacturers Approved Sources 2840-01-629-0833

2840-01-629-0833 Technical Data Datasheet 2840-01-629-0833

Characteristic
Specifications
Part Name Assigned By Controlling Agency [CXCY]
Damping Strut Fan Cowl

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2840-01-629-0833 Freight Data Freight Information 2840-01-629-0833

2840-01-629-0833 has freight characteristics.. 2840-01-629-0833 has a variance between NMFC and UFC when transported by rail and the description should be consulted.