Product Details | AIRCRAFT STRUCTURAL PLATE

1560-01-246-2189 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.

Part Alternates: 75A1302132015, 75A130213-2015, 1560-01-246-2189, 01-246-2189, 1560012462189, 012462189

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 10 DEC 1986 01-246-2189

Cross Reference | NSN 1560-01-246-2189

Part Number Cage Code Manufacturer
75A130213-2015 76301 BOEING COMPANY, THE DBA BOEING

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Technical Data | NSN 1560-01-246-2189

Characteristic Specifications
SPECIAL FEATURES ALUMINUM ALLOY 2024-0 QQ-A-250/4 SHEET,MATL 0.090 IN. THK BY 4.500 IN. W BY 13.000 IN. LG
(NON-CORE DATA) SUPPLEMENTARY FEATURES STRAP-SPLICE OUTBD WING TIP

Restrictions/Controls & Freight Information | NSN 1560-01-246-2189

Category Code Description
Hazardous Material Indicator CodePThere is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product
Demilitarization Code:BMunitions List Item - Mutilation (MUT) to the point of scrap required. (Formerly: Demilitarization not required. Trade Security Controls (TSCs) required at disposition.)
Precious Metals Indicator Code:UPrecious metal type is unknown
Criticality Code:X The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Category Code Description
No Freight Information