AMSC7438 7.9-1/4-40(5052N)CL1: CORE MATERIAL,CELLULAR,STRUCTURA.
CORE MATERIAL,CELLULAR,STRUCTURA. Key specifications include material: ALUMINUM ALLOY 5052 OVERALL, cell_size: 0.025, cell_condition: EXPANDED, cell_perforation: NOT INCLUDED, special_features: CLASS 1, GRADE B, nominal_density_rating: 7.9 POUNDS PER CUBIC FOOT LBS. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-727-9183, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | ALUMINUM ALLOY 5052 OVERALL |
| cell_size | 0.025 |
| cell_condition | EXPANDED |
| cell_perforation | NOT INCLUDED |
| special_features | CLASS 1, GRADE B |
| nominal_density_rating | 7.9 POUNDS PER CUBIC FOOT LBS |
| end_item_identification | B-52 AIRCRAFT |
| maximum_service_temp_limit | 350.0 DEG FAHRENHEIT |
| material_document_and_classification | AMS-A-81596 AEROSPACE MATERIAL SPEC STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | HONEYCOMB CORE MATERIAL |
| NSN | 1560-01-727-9183 |
| CELL SIZE | 0.025 |
| CELL PERFORATION | NOT INCLUDED |
| NOMINAL DENSITY RATING | 7.9 POUNDS PER CUBIC FOOT LBS |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-A-81596 AEROSPACE MATERIAL SPEC STD SINGLE MATERIAL RESPONSE OVERALL |
| SPECIAL FEATURES | CLASS 1, GRADE B |
| MAXIMUM SERVICE TEMP LIMIT | 350.0 DEG FAHRENHEIT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HONEYCOMB CORE MATERIAL |
| END ITEM IDENTIFICATION | B-52 AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 5052 OVERALL |
| CELL CONDITION | EXPANDED |
No substitute or cross-reference records for this part.