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2840-01-054-1334
Aircraft Gas Turbine Engine Compressor Vane
2840010541334 010541334 515D748G10
A component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction. View more Aircraft Gas Turbine Engine Compressor Vane
January 2023
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Restrictions 2840-01-054-1334
2840-01-054-1334 is a Aircraft Gas Turbine Engine Compressor Vane that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-054-1334
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-054-1334
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR01)
- Effective Date:
- 1 Dec 2007
- Greece (ZU01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Dec 1995
Approved Sources 2840-01-054-1334
- Part Number
- Manufacturer
- Status
- 515D748G10
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-054-1334
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- J79-15/17 Eng
- Criticality Code Justification [CRTL]
- Agav
- Engine Section Location [CZBJ]
- Compressor
- Material [MATT]
- Steel Overall
- Overall Length [ABHP]
- 1.770 Inches Nominal
- Special Features [FEAT]
- Original Name Vane,Compressor Stator,Turbine Engine
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Freight Information 2840-01-054-1334
2840-01-054-1334 has freight characteristics.. 2840-01-054-1334 has a variance between NMFC and UFC when transported by rail and the description should be consulted.