74A314701-2006: BRACKET,STRUCTURAL COMPONENT,AIR.
BRACKET,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, hole_quantity: 16, overall_width: 6.400 INCHES NOMINAL IN, overall_length: 6.600 INCHES NOMINAL IN, special_features: NHA: 74A310007, aircraft_location: CANOPY DECK. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-633-4151, 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 7075 |
| hole_quantity | 16 |
| overall_width | 6.400 INCHES NOMINAL IN |
| overall_length | 6.600 INCHES NOMINAL IN |
| special_features | NHA: 74A310007 |
| aircraft_location | CANOPY DECK |
| material_thickness | 0.160 INCHES NOMINAL IN |
| supplementary_features | HEAT TREAT TO COND T76 PER PS15552 |
| end_item_identification | F/A-18A AIRCRAFT A |
| aircraft_mission_design_series | F/A-18 |
| material_document_and_classification | 7075, COND-O PER QQ-A-250/12 NATIONAL SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | BRACKET - SPLICE, UPR LONG, ML, Y374.80 |
| NSN | 1560-01-633-4151 |
| SUPPLEMENTARY FEATURES | HEAT TREAT TO COND T76 PER PS15552 |
| MATERIAL DOCUMENT AND CLASSIFICATION | 7075, COND-O PER QQ-A-250/12 NATIONAL SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 6.600 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.400 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.160 INCHES NOMINAL IN |
| SPECIAL FEATURES | NHA: 74A310007 |
| AIRCRAFT LOCATION | CANOPY DECK |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET - SPLICE, UPR LONG, ML, Y374.80 |
| END ITEM IDENTIFICATION | F/A-18A AIRCRAFT A |
| MATERIAL | ALUMINUM ALLOY 7075 |
No substitute or cross-reference records for this part.