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2840-01-483-1337
Aircraft Gas Turbine Engine Turbine Duct
2840014831337 014831337 802186-5 2840PL0790839
A cylindrical shaped item or a segment thereof designed to direct air into or around a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE for cooling purposes. View more Aircraft Gas Turbine Engine Turbine Duct
January 2023
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Restrictions 2840-01-483-1337
2840-01-483-1337 is a Aircraft Gas Turbine Engine Turbine Duct 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 2840-01-483-1337
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-483-1337
- Poland (WP01)
- Effective Date:
- 1 Apr 2003
- Czech Republic (WZ01)
- Effective Date:
- 1 Dec 2009
- Brazil (YA01)
- Effective Date:
- 1 Oct 2006
- Spain (YB01)
- Effective Date:
- 1 Mar 2001
Approved Sources 2840-01-483-1337
- Part Number
- Manufacturer
- Status
- 802186-5
- Manufacturer
- 73030 - Hamilton Sundstrand Corporation (Active)
- Primary Buy
- Primary Buy
- 2840PL0790839
- 9009H - Jednolity Indeks Materialowy - (Active)
- NATO Reference
- NATO Reference
Datasheet 2840-01-483-1337
- Characteristic
- Specifications
- FIIG
- Specifications
- A530F0
- Overall Length [ABHP]
- 4.410 Inches Nominal
- End Item Identification [AGAV]
- C-295 Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Turbine Outlet Duct
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Freight Information 2840-01-483-1337
2840-01-483-1337 has freight characteristics.. 2840-01-483-1337 has a variance between NMFC and UFC when transported by rail and the description should be consulted.