2840-15-206-7404
Aircraft Turbine Engine Turbine Blade Damper
2840152067404 152067404 3G6405G00531 (241)A01263G6405G00531
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 Italy
NSN Created on 10 Jul 2012
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-15-206-7404
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Related Documents 2840-15-206-7404 1+ Documents (More...)
3G6405G00531 (241)A01263G6405G00531 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR
RQST NE Updated Every Day 2840-15-206-7404 RQST Updated Every Day 2840-15-206-7404 RQST NE Related Documents
152067404,3G6405G00531 3G6405G00531 (241)A01263G6405G00531 A device used to reduce high cycle fatigue
RQST NE Updated Every Day 2840-15-206-7404 RQST Updated Every Day 2840-15-206-7404 RQST NE Related Documents
152067404,3G6405G00531 3G6405G00531 (241)A01263G6405G00531 A device used to reduce high cycle fatigue
Restrictions 2840-15-206-7404
End Users 2840-15-206-7404
- Italy (ZR)
Approved Sources 2840-15-206-7404
- Part Number
- Manufacturer
- Status
- 3G6405G00531
- Manufacturer
- A0126 - Leonardo Spa Helicopters Division - (Active)
- Primary Buy
- Primary Buy
- (241)A01263G6405G00531
- A0126 - Leonardo Spa Helicopters Division - (Active)
- Secondary Buy
- Secondary Buy
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