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5680-01-535-7100

Structural Cellular Core Material

5680015357100 015357100 MIL-C-7438B2-4.3-1/4J-20N5052

A light durable material having a cellular core of uniform geometric shapes. It is primarily used for, but not limited to, aircraft structure, such as fuselages, control surfaces, compartments, radomes, and the like. For items with a metallic or nonmetallic facing see PANEL, STRUCTURAL, AIRCRAFT. View more Structural Cellular Core Material

5680-01-535-7100 CORE MATERIAL,CELLULAR,STRUCTURAL 5680015357100 015357100

Managed by United States
NSN Created on 8 Dec 2005
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
5680-01-535-7100 CORE MATERIAL,CELLULAR,STRUCTURAL 5680015357100 015357100 1/1
NSN 5680-01-535-7100 (Generic Image) 1/1

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5680-01-535-7100 Demil Restrictions 5680-01-535-7100

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: P | PMIC: A | EDC: A | ADPEC: 0

5680-01-535-7100 is a Structural Cellular Core Material 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 considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). 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.

5680-01-535-7100 End Users End Users 5680-01-535-7100

Germany (ZG01)
Effective Date:
1 Dec 2005

5680-01-535-7100 Manufacturers Approved Sources 5680-01-535-7100

Part Number
Manufacturer
Status
MIL-C-7438B2-4.3-1/4J-20N5052
81349 - Military Specifications (Active)
Definitive Standard

5680-01-535-7100 Technical Data Datasheet 5680-01-535-7100

Characteristic
Specifications
FIIG
T232-F
End Item Identification [AGAV]
Pc-3C-Orion Aircraft
Basic Material [AMSP]
Aluminum
Cell Perforation [AZRQ]
Not Included
Cell Size [AZRJ]
1/4 In
Cell Condition [AZRE]
Expanded
Nominal Density Rating [AZRR]
4.3 Pounds Per Cubic Foot
Part Name Assigned By Controlling Agency [CXCY]
Core Material,Aluminum,For Sandwich Construction
Specification/Standard Data [ZZZK]
81349-Mil-C-7438G Government Specification
Supplementary Features [SUPP]
Aircraft Material

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5680-01-535-7100 Freight Data Freight Information 5680-01-535-7100

5680-01-535-7100 has freight characteristics.. 5680-01-535-7100 has a variance between NMFC and UFC when transported by rail and the description should be consulted.