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1560-01-579-2430
Aircraft Structural Plate
1560015792430 015792430 5HW02182-124
A flat or preformed item of metallic or nonmetallic material. It may vary in shape and its surface may be smooth and/or serrated. Its thickness is small in comparison to both its length and width. It is designed to be mounted upon a surface or between two surfaces. Its primary function is to strengthen, join, or separate aircraft structural parts. Excludes PLATE, MENDING; SHIM; and SPACER, PLATE. View more Aircraft Structural Plate
November 2023
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Related Documents 1560-01-579-2430 1+ Documents (More...)
United States (US) 4. 1560-01-579-2430 Marketplace Restrictions Approved Sources Datasheet Management
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Restrictions 1560-01-579-2430
IUID Required
1560-01-579-2430 is a Aircraft Structural Plate 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 may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
End Users 1560-01-579-2430
- US Air Force (FLL5)
- Effective Date:
- 1 Nov 2009
Approved Sources 1560-01-579-2430
- Part Number
- Manufacturer
- Status
- 5HW02182-124
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-579-2430
- Characteristic
- Specifications
- End Item Identification [AGAV]
- Specifications
- F-22 Raptor
- Aircraft Location [CZDJ]
- Inbd Blade-Vertical Stab Assy
- Aircraft Mission Design Series [CZEK]
- F-22 Acft
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Freight Information 1560-01-579-2430
1560-01-579-2430 has freight characteristics.. 1560-01-579-2430 has a variance between NMFC and UFC when transported by rail and the description should be consulted.