3586-4-87: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_length: 9.000 INCHES NOMINAL IN, special_features: USED AS ANGLE,OPPOSITE PN 35-8648-8, aircraft_location: FRAME INSTL,NOSE COWL, aircraft_station_number: 77.80, aircraft_mission_design_series: B-52. This part is cataloged in the U.S.
Government catalog under NSN 5330-00-599-9546, 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_length | 9.000 INCHES NOMINAL IN |
| special_features | USED AS ANGLE,OPPOSITE PN 35-8648-8 |
| aircraft_location | FRAME INSTL,NOSE COWL |
| aircraft_station_number | 77.80 |
| aircraft_mission_design_series | B-52 |
| material_document_and_classification | QQ-A-362-0 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 5330-00-599-9546 |
| CROSS-SECTIONAL HEIGHT | 0.250 INCHES NOMINAL IN |
| CROSS-SECTIONAL WIDTH | 0.250 INCHES NOMINAL IN |
| CROSS-SECTIONAL SHAPE STYLE | SQUARE |
| NONDEFINITIVE SPEC/STD DATA | L TYPE AND 2 CLASS AND 1111 SYMBOL |
| MATERIAL | ASBESTOS AND IRON ALLOY |
| FABRICATION METHOD | BRAIDED AND SOLID |