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2840-00-853-6904
Aircraft Gas Turbine Engine Rear Frame
2840008536904 008536904 4009T25G01
A frame used for and part of the rear section of an aircraft gas turbine engine. May include struts. View more Aircraft Gas Turbine Engine Rear Frame
January 2023
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United States (US) 4. 2840-00-853-6904 Marketplace Restrictions Approved Sources Datasheet Management
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Aircraft Gas Turbine Engine Rear Frame www.nsnlookup.com /fsg-28/fsc-2840/us 2840-00-853-6904 https

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Aircraft Gas Turbine Engine Rear Frame www.nsnlookup.com /fsg-28/fsc-2840/us 2840-00-853-6904 https

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Aircraft Gas Turbine Engine Rear Frame www.nsnlookup.com /fsg-28/fsc-2840/us 2840-00-853-6904 https
Restrictions 2840-00-853-6904
IUID Required
2840-00-853-6904 is a Aircraft Gas Turbine Engine Rear Frame 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-00-853-6904
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-00-853-6904
- US Air Force (FXX4)
- Effective Date:
- 1 Sep 2000
- Austria (WB)
- Austria (WB01)
- Effective Date:
- 1 Feb 2005
- Republic of Korea (ZH)
- Republic of Korea (ZH01)
- Effective Date:
- 1 Aug 1995
- United States of America (ZZ)
Approved Sources 2840-00-853-6904
- Part Number
- Manufacturer
- Status
- 4009T25G01
- Manufacturer
- 99207 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-00-853-6904
- Characteristic
- Specifications
- FIIG
- Specifications
- A522Q0
- End Item Identification [AGAV]
- Acft Eng J85
- Criticality Code Justification [CRTL]
- Abhp And Abkv And Aarx
- Material [MATT]
- Nickel Alloy
- Number Of Variable Guide Vanes [CZLB]
- 6
- Outside Diameter [ABKV]
- 17.000 Inches Nominal
- Inside Diameter [AARX]
- 15.515 Inches Nominal
- Overall Length [ABHP]
- 4.524 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Original Name Mainframe And Brack
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Freight Information 2840-00-853-6904
2840-00-853-6904 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 114215. A Sub NMFC of Z. It has a NMFC Description of ASSEMBLIES JET AIRCRAFT ENGINE. 2840-00-853-6904 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 2840-00-853-6904 is rated as class 85 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 2840-00-853-6904 is not classified as a special type of cargo when transported by water. 2840-00-853-6904 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.