74R350005-2063: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 1.160 INCHES NOMINAL IN, special_features: 0.255 CENTER HOLE USED FOR F/A-18C CUM 268 SUPPORTING SERVICE BULLETIN 74SB2893, aircraft_location: CANOPY 1 AND 2 PLACE, material_thickness: 0.050 INCHES NOMINAL IN, end_item_identification: BRACKET AND SHIMS CANOPY 1 AND 2 F/A-18C. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-560-8976, 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 |
| overall_width | 1.160 INCHES NOMINAL IN |
| special_features | 0.255 CENTER HOLE USED FOR F/A-18C CUM 268 SUPPORTING SERVICE BULLETIN 74SB2893 |
| aircraft_location | CANOPY 1 AND 2 PLACE |
| material_thickness | 0.050 INCHES NOMINAL IN |
| end_item_identification | BRACKET AND SHIMS CANOPY 1 AND 2 F/A-18C |
| aircraft_mission_design_series | F/A-18C HORNET |
| material_document_and_classification | QQ-A-250/13 COND T6 FED SPEC SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | FILLER |
| NSN | 1560-01-560-8976 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 COND T6 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL WIDTH | 1.160 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.050 INCHES NOMINAL IN |
| SPECIAL FEATURES | 0.255 CENTER HOLE USED FOR F/A-18C CUM 268 SUPPORTING SERVICE BULLETIN 74SB2893 |
| AIRCRAFT LOCATION | CANOPY 1 AND 2 PLACE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FILLER |
| END ITEM IDENTIFICATION | BRACKET AND SHIMS CANOPY 1 AND 2 F/A-18C |
| MATERIAL | ALUMINUM ALLOY 7075 |
| AIRCRAFT MISSION DESIGN SERIES | F/A-18C HORNET |
No substitute or cross-reference records for this part.