36998-3: PLATE,STRUCTURAL,AIRCRAFT.
The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 5052, first_leg_angle: 90.0 DEGREES NOMINAL, first_leg_style: END RADIUS, first_leg_width: 1.125 INCHES NOMINAL IN, first_leg_length: 1.563 INCHES NOMINAL IN, second_leg_style: SQUARE. This part is cataloged in the U.S.
Government catalog under NSN 1560-00-009-9695, 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 5052 |
| first_leg_angle | 90.0 DEGREES NOMINAL |
| first_leg_style | END RADIUS |
| first_leg_width | 1.125 INCHES NOMINAL IN |
| first_leg_length | 1.563 INCHES NOMINAL IN |
| second_leg_style | SQUARE |
| second_leg_width | 1.125 INCHES NOMINAL IN |
| style_designator | ANGLE |
| second_leg_length | 1.160 INCHES NOMINAL IN |
| first_leg_thickness | 0.125 INCHES NOMINAL IN |
| first_leg_end_radius | 0.563 INCHES NOMINAL IN |
| second_leg_thickness | 0.125 INCHES NOMINAL IN |
| NSN | 1560-00-009-9695 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5,TEMP T3,CLAD FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | CARGO RAMP,SCUFF PLATE |
| MATERIAL | ALUMINUM ALLOY 2024 |
| AIRCRAFT MISSION DESIGN SERIES | C130 |
No substitute or cross-reference records for this part.