Premium Information is available for this item - Upgrade for $1 a day
1560-01-444-4122
Aircraft Structural Plate
1560014444122 014444122 348190
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
![]()
January 2023
4

Marketplace 1560-01-444-4122
Request a Quotation from participating marketplace vendors
Related Documents 1560-01-444-4122 2+ Documents (More...)
United States (US) 4. 1560-01-444-4122 Marketplace Restrictions Approved Sources Datasheet Management
1 EA NS Request Quotation Updated Every Day 1560-01-444-4122 RQST NE Updated Every Day 1560-01-444-4122
www.nsnlookup.com /fsg-51/fsc-5180/de 5180-12-339-5198 https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-01-444-4122
Aircraft Structural Plate 1560014444122 Documents 1560-01-444-4122 1+ Documents ( More... ) https
Restrictions 1560-01-444-4122
1560-01-444-4122 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. This item is a US Munitions List Item and must be mutilated to scrap. 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.
Import and Export 1560-01-444-4122
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-444-4122
- United Kingdom (ZK01)
- Effective Date:
- 1 May 1997
Approved Sources 1560-01-444-4122
- Part Number
- Manufacturer
- Status
- 348190
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-444-4122
- Characteristic
- Specifications
- FIIG
- Specifications
- A11400
- Material [MATT]
- Aluminum Alloy 2024
- Material Document And Classification [MDCL]
- Qq-A-362 Cond T3 Fed Spec Single Material Response
- Aircraft Location [CZDJ]
- Cargo Floor
- Aircraft Mission Design Series [CZEK]
- C130-J
- Overall Length [ABHP]
- 9.000 Inches Nominal
- Overall Width [ABMK]
- 2.000 Inches Nominal
- Material Thickness [ABPX]
- 0.051 Inches Nominal
Similar Supply Items to 1560-01-444-4122


















Freight Information 1560-01-444-4122
1560-01-444-4122 has freight characteristics managed by the Bureau of Accounts.. 1560-01-444-4122 has a variance between NMFC and UFC when transported by rail and the description should be consulted.