1534AS141: SPRING,HELICAL,EXTENSION.
The SPRING,HELICAL,EXTENSION is a the manufacturer industrial component. Key specifications include material: TITANIUM OVERALL, end_style: MACHINE LOOP BOTH ENDS, design_type: CLOSED, hook_radius: 0.250 INCHES NOMINAL BOTH ENDS IN, load_rating: 20.00 POUNDS NOMINAL LBS, coil_quantity: 20-1/2. This part is cataloged in the U.S.
Government catalog under NSN 5360-01-140-0879, 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 | TITANIUM OVERALL |
| end_style | MACHINE LOOP BOTH ENDS |
| design_type | CLOSED |
| hook_radius | 0.250 INCHES NOMINAL BOTH ENDS IN |
| load_rating | 20.00 POUNDS NOMINAL LBS |
| coil_quantity | 20-1/2 |
| opening_width | 0.335 INCHES NOMINAL BOTH ENDS IN |
| inside_diameter | 0.420 INCHES NOMINAL IN |
| style_designator | CYLINDRICAL |
| spring_free_length | 2.744 INCHES NOMINAL IN |
| coil_helix_direction | RIGHT-HAND OR LEFT-HAND |
| spring_deflection_rate | 16.140 POUNDS PER INCH NOMINAL LBS |
| NSN | 5360-01-140-0879 |
| SPRING FREE OUTSIDE DIAMETER | 0.420 INCHES NOMINAL IN |
| LOAD RATING | 20.00 POUNDS NOMINAL LBS |
| END STYLE | MACHINE LOOP BOTH ENDS |
| DESIGN TYPE | CLOSED |
| STYLE DESIGNATOR | CYLINDRICAL |
| OPENING WIDTH | 0.335 INCHES NOMINAL BOTH ENDS IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | DMS1910 13-11-3,MCDONNELL AIRCRAFT CORP,DOUGLAS AIRCRAFT CO DIV MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| SPRING FREE LENGTH | 2.744 INCHES NOMINAL IN |
| SPRING DEFLECTION RATE | 16.140 POUNDS PER INCH NOMINAL LBS |
| INSIDE DIAMETER | 0.420 INCHES NOMINAL IN |