35-8642-12: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 0.071 INCHES NOMINAL IN, overall_length: 28.00 INCHES NOMINAL IN, special_features: OPPOSITE PN 35-8462-11; USED AS WEB, aircraft_location: FRAM INSTL,CANTED NOSE COWL, special_test_features: DIMENSIONS: .071 X 10.4 X 28.0"; CLAD 2024-T3 SHEET QQ-A-362 T3 TEMPER; FINISH: F-2115. This part is cataloged in the U.S.
Government catalog under NSN 1560-01-152-6419, 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 2024 |
| overall_width | 0.071 INCHES NOMINAL IN |
| overall_length | 28.00 INCHES NOMINAL IN |
| special_features | OPPOSITE PN 35-8462-11; USED AS WEB |
| aircraft_location | FRAM INSTL,CANTED NOSE COWL |
| special_test_features | DIMENSIONS: .071 X 10.4 X 28.0"; CLAD 2024-T3 SHEET QQ-A-362 T3 TEMPER; FINISH: F-2115 |
| aircraft_station_number | 70.000 |
| end_item_identification | B-52 |
| part_name_assigned_by_controlling_agency | WEB |
| NSN | 1560-01-152-6419 |
| AIRCRAFT STATION NUMBER | 70.000 |
| SPECIAL TEST FEATURES | DIMENSIONS: .071 X 10.4 X 28.0"; CLAD 2024-T3 SHEET QQ-A-362 T3 TEMPER; FINISH: F-2115 |
| OVERALL LENGTH | 28.00 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.071 INCHES NOMINAL IN |
| SPECIAL FEATURES | OPPOSITE PN 35-8462-11; USED AS WEB |
| AIRCRAFT LOCATION | FRAM INSTL,CANTED NOSE COWL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | WEB |
| END ITEM IDENTIFICATION | B-52 |
| MATERIAL | ALUMINUM ALLOY 2024 |
No substitute or cross-reference records for this part.