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2840-01-528-6890
Aircraft Gas Turbine Engine Front Frame
2840015286890 015286890 9521M93G02
A frame used for and part of the front section of an aircraft gas turbine engine. May include struts with or without variable guide vanes. View more Aircraft Gas Turbine Engine Front Frame
January 2023
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Related Documents 2840-01-528-6890 2+ Documents (More...)
/fsc-2840/us 2840-01-528-6890 Aircraft Gas Turbine Engine Front Frame 9521M93G02 A frame used for and
Restrictions 2840-01-528-6890 DEMIL: D | DEMILI : 1 | CRITICALITY : X | HMIC : N | PMIC : A | EDC
Aircraft Gas Turbine Engine Front Frame vendors Request Updated Every Day 2840-01-528-6890 https
Restrictions 2840-01-528-6890
2840-01-528-6890 is a Aircraft Gas Turbine Engine Front Frame 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 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 2840-01-528-6890
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2840-01-528-6890
- Greece (ZU01)
- Effective Date:
- 1 Mar 2005
Approved Sources 2840-01-528-6890
- Part Number
- Manufacturer
- Status
- 9521M93G02
- Manufacturer
- 07482 - General Electric Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2840-01-528-6890
- Characteristic
- Specifications
- FIIG
- Specifications
- A522Q0
- End Item Identification [AGAV]
- Aircraft Engine, Model F100-Ge-100
NATO Stock Numbers Related to 2840-01-528-6890
Freight Information 2840-01-528-6890
2840-01-528-6890 has freight characteristics.. 2840-01-528-6890 has a variance between NMFC and UFC when transported by rail and the description should be consulted.