12554711: BRACKET,VEHICULAR COMPONENTS.
The BRACKET,VEHICULAR COMPONENTS is a the manufacturer industrial component. Key specifications include shape: IRREGULAR, material: ALUMINUM ALLOY 5086 OR ALUMINUM ALLOY 5052, document_type: MILITARY DRAWING, overall_width: 16.00 INCHES NOMINAL IN, heat_treatment: H-32 STRAIN HARDENED, STABILIZED TO 1/4 HARD OR H-34 STRAIN HARDENED, STABILIZED TO 1/2 HARD OR H-112 AS ROLLED, overall_length: 13.69 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 2590-01-698-3497, 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.
| shape | IRREGULAR |
| material | ALUMINUM ALLOY 5086 OR ALUMINUM ALLOY 5052 |
| document_type | MILITARY DRAWING |
| overall_width | 16.00 INCHES NOMINAL IN |
| heat_treatment | H-32 STRAIN HARDENED, STABILIZED TO 1/4 HARD OR H-34 STRAIN HARDENED, STABILIZED TO 1/2 HARD OR H-112 AS ROLLED |
| overall_length | 13.69 INCHES NOMINAL IN |
| document_source | 19207 |
| mounting_method | SCREW |
| color_chip_number | 24533 |
| mounting_position | INTERIOR |
| overall_thickness | 0.190 INCHES NOMINAL IN |
| component_quantity | 3 |
| NSN | 2590-01-698-3497 |
| COMPONENT QUANTITY | 3 |
| MOUNTING HOLE QUANTITY | 8 |
| DOCUMENT TYPE | MILITARY DRAWING |
| COLOR CHIP NUMBER | 24533 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL DTL 53072 MIL STD SINGLE TREATMENT RESPONSE AND MIL DTL 5541, TYPE II, CLASS 1A MIL STD 1ST TREATMENT RESPONSE AND MIL DTL 53022 MIL STD 1ST TREATMENT RESPONSE OR MIL DTL 53030 MIL STD 1ST TREATMENT RESPONSE AND MIL PRF 22750 MIL STD 2ND TREATMENT RESPONSE AND AMS 595 INTERNATIONAL STD/SPEC SINGLE TREATMENT RESPONSE A |
| MOUNTING METHOD | SCREW |
| MOUNTING POSITION | INTERIOR |
| HEAT TREATMENT | H-32 STRAIN HARDENED, STABILIZED TO 1/4 HARD OR H-34 STRAIN HARDENED, STABILIZED TO 1/2 HARD OR H-112 AS ROLLED |
| OVERALL THICKNESS | 0.190 INCHES NOMINAL IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | ASTM B209 AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) 1ST MATERIAL RESPONSE OR ASTM B221 AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) 2ND MATERIAL RESPONSE OR AMS 4016 AEROSPACE MATERIAL SPEC STD 3RD MATERIAL RESPONSE OR AMS 4017 AEROSPACE MATERIAL SPEC STD 4TH MATERIAL RESPONSE |
No substitute or cross-reference records for this part.