01AA100D010105: ANGLE,STRUCTURAL.
The ANGLE,STRUCTURAL is a the manufacturer industrial component. Key specifications include length: 12.000 FEET NOMINAL FT, material: ALUMINUM ALLOY 7075, usage_design: AIRCRAFT, overall_width: 1.500 INCHES NOMINAL IN, overall_height: 1.500 INCHES NOMINAL IN, first_tip_style: SQUARE END. This part is cataloged in the U.S.
Government catalog under NSN 9540-01-480-6121, 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.
| length | 12.000 FEET NOMINAL FT |
| material | ALUMINUM ALLOY 7075 |
| usage_design | AIRCRAFT |
| overall_width | 1.500 INCHES NOMINAL IN |
| overall_height | 1.500 INCHES NOMINAL IN |
| first_tip_style | SQUARE END |
| basic_shape_style | ANGLE |
| left_inside_angle | 90.0 DEGREES NOMINAL |
| fabrication_method | EXTRUDED |
| base_flange_thickness | 0.125 INCHES NOMINAL IN |
| end_item_identification | STRUCASSY, FCS; AIRCRAFT, B-2 BOMBER (ATB) |
| left_side_flange_thickness | 0.125 INCHES NOMINAL IN |
| NSN | 9540-01-480-6121 |
| OVERALL HEIGHT | 1.500 INCHES NOMINAL IN |
| LENGTH | 12.000 FEET NOMINAL FT |
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL IN |
| USAGE DESIGN | AIRCRAFT |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/18 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL WIDTH | 1.500 INCHES NOMINAL IN |
| LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL IN |
| BASIC SHAPE STYLE | ANGLE |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ALUMINUM ALLOY ANGLE- EXTRUDED |
No substitute or cross-reference records for this part.