2840-12-378-7025
Aircraft Turbine Engine Turbine Blade Damper
2840123787025 123787025 BRR24590
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 5 May 2009
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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Related Documents 2840-12-378-7025 1+ Documents (More...)
BRR24590 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE
RQST NE Updated Every Day 2840-12-378-7025 RQST Updated Every Day 2840-12-378-7025 RQST NE Related Documents
,BRR24590 BRR24590 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS
RQST NE Updated Every Day 2840-12-378-7025 RQST Updated Every Day 2840-12-378-7025 RQST NE Related Documents
,BRR24590 BRR24590 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS
Restrictions 2840-12-378-7025
End Users 2840-12-378-7025
- United Kingdom (ZK)
Approved Sources 2840-12-378-7025
- Part Number
- Manufacturer
- Status
- BRR24590
- Manufacturer
- D0272 - Rolls-Royce Deutschland Ltd & Co Kg (Active)
- Primary Buy
- Primary Buy
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