Premium Information is available for this item - Upgrade for $1 a day
2840-01-062-8055
Aircraft Gas Turbine Engine Compressor Blade
2840010628055 010628055 9654M45P09
An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Compressor Blade
May 2023
6
Marketplace 2840-01-062-8055
Request a Quotation from participating marketplace vendors
Related Documents 2840-01-062-8055 1+ Documents (More...)
United States (US) 4. 2840-01-062-8055 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-062-8055 RQST Updated Every Day 2840-01-062-8055 RQST NE Related
Restrictions 2840-01-062-8055
IUID Required
2840-01-062-8055 is a Aircraft Gas Turbine Engine Compressor Blade 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 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 2840-01-062-8055
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-062-8055
- US Air Force (FXX4)
- Effective Date:
- 1 Sep 2000
- Former MOE Rule:
- FEE4
- Spain (YB01)
- Effective Date:
- 1 Sep 2009
Approved Sources 2840-01-062-8055
- Part Number
- Manufacturer
- Status
- 9654M45P09
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-062-8055
- Characteristic
- Specifications
- FIIG
- Specifications
- A10700
- End Item Identification [AGAV]
- Acft Eng Tf39
- Criticality Code Justification [CRTL]
- Agav
- Design Type [APGF]
- Compressor
- Engine Section Location [CZBJ]
- Compressor
- Special Features [FEAT]
- Original Name Blade,Compressor Rotor,Turbine Engine
- Stage Number [CZCJ]
- 12
Management Data 2840-01-062-8055
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2022
- Department of the Air Force (DF)
- EA
- Subscribe
- EA
- Oct 2021
- Department of the Air Force (DF)
- EA
- Subscribe
- EA
- Oct 2020
- Department of the Air Force (DF)
- EA
- Subscribe
- EA
- Oct 2019
- Department of the Air Force (DF)
- EA
- Subscribe
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- L
- R
- Refer To Net Price 44.13
- NET PRICE 44.13
- R
Similar Supply Items to 2840-01-062-8055
Freight Information 2840-01-062-8055
2840-01-062-8055 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. 2840-01-062-8055 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. 2840-01-062-8055 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. 2840-01-062-8055 is not classified as a special type of cargo when transported by water. 2840-01-062-8055 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.