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2840-01-462-3954
Aircraft Gas Turbine Engine Turbine Rotor Blade
2840014623954 014623954 4086361 2840PL0728530
An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Turbine Rotor Blade
January 2023
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Related Documents 2840-01-462-3954 1+ Documents (More...)
United States (US) 4. 2840-01-462-3954 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Related Documents 2840-01-462-3954 1+ Documents ( More... ) https//www.nsnlookup.com /fsg
Restrictions 2840-01-462-3954
2840-01-462-3954 is a Aircraft Gas Turbine Engine Turbine Rotor Blade that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2840-01-462-3954
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-462-3954
- US Air Force (FXX5)
- Effective Date:
- 1 Jan 2008
- Former MOE Rule:
- FXX4
- Poland (WP01)
- Effective Date:
- 1 Jun 2011
- Singapore (YJ01)
- Effective Date:
- 1 Apr 2001
- Republic of Korea (ZH01)
- Effective Date:
- 1 Mar 2002
- Greece (ZU01)
- Effective Date:
- 1 May 2008
Approved Sources 2840-01-462-3954
- Part Number
- Manufacturer
- Status
- 4086361
- Manufacturer
- 77445 - Rtx Corporation (Active)
- Primary Buy
- Primary Buy
- 2840PL0728530
- 9009H - Jednolity Indeks Materialowy - (Active)
- NATO Reference
- NATO Reference
Datasheet 2840-01-462-3954
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Acft Eng F100299
- Criticality Code Justification [CRTL]
- Agav
- Design Type [APGF]
- Axial Compressor
- Engine Section Location [CZBJ]
- Turbine
- Part Name Assigned By Controlling Agency [CXCY]
- Blade Set Turbine Rotor, 1 Stage
- Special Features [FEAT]
- Blade Set 4086361 Supersedes 4087101 (2840014456144Pt) By Attrition, Notechinical Order Data Available, 2 Blades Required And Must Be Same Moment Wt Within 0.050 Oz. In.
- Stage Number [CZCJ]
- 1
NATO Stock Numbers Related to 2840-01-462-3954
Freight Information 2840-01-462-3954
2840-01-462-3954 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. 2840-01-462-3954 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 2840-01-462-3954 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 671 for ocean manifesting and military sealift. 2840-01-462-3954 is not classified as a special type of cargo when transported by water. 2840-01-462-3954 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.