F1065-102: BRACKET,MOUNTING.
The BRACKET,MOUNTING is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, overall_height: 0.075 INCHES MINIMUM AND 0.076 INCHES MAXIMUM IN, overall_length: 5.390 INCHES MINIMUM AND 5.410 INCHES MAXIMUM IN, special_features: IDENTIFY PART PER MIL-STD-130, surface_treatment: ANODIZE, mounting_hole_type: PLAIN. This part is cataloged in the U.S.
Government catalog under NSN 5340-01-500-1180, 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_height | 0.075 INCHES MINIMUM AND 0.076 INCHES MAXIMUM IN |
| overall_length | 5.390 INCHES MINIMUM AND 5.410 INCHES MAXIMUM IN |
| special_features | IDENTIFY PART PER MIL-STD-130 |
| surface_treatment | ANODIZE |
| mounting_hole_type | PLAIN |
| mounting_hole_quantity | 5 |
| end_item_identification | C-17A AIRCRAFT A |
| material_document_and_classification | QQ-A-250/8 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | END BRACKET - SLIDER |
| surface_treatment_document_and_classification | MIL-A-8625, TYPE 2 CLASS 2 MIL SPEC SINGLE TREATMENT RESPONSE |
| NSN | 5340-01-500-1180 |
| MOUNTING HOLE QUANTITY | 5 |
| OVERALL HEIGHT | 0.075 INCHES MINIMUM AND 0.076 INCHES MAXIMUM IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625, TYPE 2 CLASS 2 MIL SPEC SINGLE TREATMENT RESPONSE |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/8 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 5.390 INCHES MINIMUM AND 5.410 INCHES MAXIMUM IN |
| SPECIAL FEATURES | IDENTIFY PART PER MIL-STD-130 |
| SURFACE TREATMENT | ANODIZE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | END BRACKET - SLIDER |
| END ITEM IDENTIFICATION | C-17A AIRCRAFT A |
| MATERIAL | ALUMINUM ALLOY 5052 |
No substitute or cross-reference records for this part.