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2840-01-502-2162
Aircraft Gas Turbine Engine Turbine Blade Retainer
2840015022162 015022162 23070177-102
An item specifically designed to position and/or restrain the movement of one or more BLADE, or BLADE SET, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may be the full 360 degrees required for one turbine stage or a segment thereof. View more Aircraft Gas Turbine Engine Turbine Blade Retainer
January 2023
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Related Documents 2840-01-502-2162 1+ Documents (More...)
RQST NE Updated Every Day 2840-01-502-2162 RQST Updated Every Day 2840-01-502-2162 RQST NE Related Documents
RQST NE Updated Every Day 2840-01-502-2162 RQST Updated Every Day 2840-01-502-2162 RQST NE Restrictions
Restrictions 2840-01-502-2162
2840-01-502-2162 is a Aircraft Gas Turbine Engine Turbine Blade Retainer 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.
Import and Export 2840-01-502-2162
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-502-2162
- Italy (ZR01)
- Effective Date:
- 1 Oct 2002
Approved Sources 2840-01-502-2162
- Part Number
- Manufacturer
- Status
- 23070177-102
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-502-2162
- Characteristic
- Specifications
- FIIG
- Specifications
- A522S0
- End Item Identification [AGAV]
- Used On Aircraft Engine Gas Generating Turbine 1St Stage, Models Ae2100a And C; Ae2100d2 And D3 And J
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Freight Information 2840-01-502-2162
2840-01-502-2162 has freight characteristics.. 2840-01-502-2162 has a variance between NMFC and UFC when transported by rail and the description should be consulted.