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2840-01-502-1140
Aircraft Gas Turbine Engine Air Seal
2840015021140 015021140 23036890
A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an ENGINE, GAS TURBINE, AIRCRAFT. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal. View more Aircraft Gas Turbine Engine Air Seal
January 2023
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2840-01-502-1140 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-502-1140
NE Updated Every Day 2840-01-502-1140 RQST Updated Every Day 2840-01-502-1140 RQST NE Restrictions 2840
Restrictions 2840-01-502-1140
2840-01-502-1140 is a Aircraft Gas Turbine Engine Air Seal 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 2840-01-502-1140
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-502-1140
- Italy (ZR01)
- Effective Date:
- 1 Oct 2002
Approved Sources 2840-01-502-1140
- Part Number
- Manufacturer
- Status
- 23036890
- Manufacturer
- 63005 - Rolls-Royce Corporation (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-502-1140
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- T406-Ad-400 Engine, Ae2100a, C Engine, Ae2100d2, D3, J Engine
- Part Name Assigned By Controlling Agency [CXCY]
- Heat-Seal No. 7 Shield
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Freight Information 2840-01-502-1140
2840-01-502-1140 has freight characteristics.. 2840-01-502-1140 has a variance between NMFC and UFC when transported by rail and the description should be consulted.