2840-12-379-0581
Aircraft Turbine Engine Turbine Blade Damper
2840123790581 123790581 BRR24588
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
Managed by Germany
NSN Created on 18 Jun 2009
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-12-379-0581 1+ Documents (More...)
BRR24588 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE
RQST NE Updated Every Day 2840-12-379-0581 RQST Updated Every Day 2840-12-379-0581 RQST NE Related Documents
,BRR24588 BRR24588 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS
RQST NE Updated Every Day 2840-12-379-0581 RQST Updated Every Day 2840-12-379-0581 RQST NE Related Documents
,BRR24588 BRR24588 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS
Restrictions 2840-12-379-0581
End Users 2840-12-379-0581
- United Kingdom (ZK)
Approved Sources 2840-12-379-0581
- Part Number
- Manufacturer
- Status
- BRR24588
- Manufacturer
- D0272 - Rolls-Royce Deutschland Ltd & Co Kg (Active)
- Primary Buy
- Primary Buy
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