2840-14-569-2103

Aircraft Turbine Engine Turbine Blade Damper

2840145692103 145692103 303-151-109-0

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

2840-14-569-2103 DAMPER,TURBINE BLADE,AIRCRAFT TURBINE ENGINE 2840145692103 145692103

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NSN Created on 23 Aug 2011
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-569-2103 DAMPER,TURBINE BLADE,AIRCRAFT TURBINE ENGINE 2840145692103 145692103 1/1
NSN 2840-14-569-2103 (Generic Image) 1/1

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303-151-109-0 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE
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2840-14-569-2103 Demil Restrictions 2840-14-569-2103

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2840-14-569-2103 is a Aircraft Turbine Engine Turbine Blade Damper

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