AND10134-1003-707ST6: SUPPORT,STRUCTURAL COMPONENT,AIR.
SUPPORT,STRUCTURAL COMPONENT,AIR. Key specifications include material: ALUMINUM ALLOY 7075, usage_design: AIRCRAFT, overall_width: 1.000 INCHES NOMINAL IN, heat_treatment: T-6511 SOLUTION HEAT TREATED, overall_height: 0.750 INCHES NOMINAL IN, first_tip_style: RIGHT QUARTER RADIUS. This part is cataloged in the U.S.
Government catalog under NSN 9540-00-495-7812, 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 |
| usage_design | AIRCRAFT |
| overall_width | 1.000 INCHES NOMINAL IN |
| heat_treatment | T-6511 SOLUTION HEAT TREATED |
| overall_height | 0.750 INCHES NOMINAL IN |
| first_tip_style | RIGHT QUARTER RADIUS |
| first_tip_radius | 0.063 INCHES NOMINAL IN |
| second_tip_style | UPPER RADIUS |
| basic_shape_style | ANGLE |
| left_inside_angle | 90.0 DEGREES NOMINAL |
| second_tip_radius | 0.063 INCHES NOMINAL IN |
| fabrication_method | EXTRUDED |
| NSN | 9540-00-495-7812 |
| OVERALL HEIGHT | 0.750 INCHES NOMINAL IN |
| BASE FLANGE THICKNESS | 0.063 INCHES NOMINAL IN |
| USAGE DESIGN | AIRCRAFT |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| FIRST TIP RADIUS | 0.063 INCHES NOMINAL IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL WIDTH | 1.000 INCHES NOMINAL IN |
| LEFT SIDE FLANGE THICKNESS | 0.063 INCHES NOMINAL IN |
| SECOND TIP RADIUS | 0.063 INCHES NOMINAL IN |
| BASIC SHAPE STYLE | ANGLE |