Stress area: 0.763 in² · Proof load: 91,560 lbs · Clamp load (75%): 68,670 lbs
| Surface Condition | K Factor | ft·lbs | N·m | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1287.6 | 1745.8 | 15451.2 | 17802.3 |
| Oiled | 0.15 | 965.7 | 1309.3 | 11588.4 | 13351.2 |
| Zinc Plated | 0.18 | 1158.8 | 1571.1 | 13905.6 | 16020.8 |
| Waxed | 0.1 | 643.8 | 872.9 | 7725.6 | 8901.1 |
| MoS₂ | 0.12 | 772.5 | 1047.4 | 9270.0 | 10680.5 |
| Galvanized | 0.25 | 1609.5 | 2182.2 | 19314.0 | 22252.3 |
Stress area: 0.856 in² · Proof load: 102,720 lbs · Clamp load (75%): 77,040 lbs
| Surface Condition | K Factor | ft·lbs | N·m | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 1444.5 | 1958.5 | 17334.0 | 19971.2 |
| Oiled | 0.15 | 1083.4 | 1468.9 | 13000.8 | 14978.7 |
| Zinc Plated | 0.18 | 1300.0 | 1762.6 | 15600.0 | 17973.6 |
| Waxed | 0.1 | 722.2 | 979.2 | 8666.4 | 9985.1 |
| MoS₂ | 0.12 | 866.7 | 1175.1 | 10400.4 | 11982.7 |
| Galvanized | 0.25 | 1805.6 | 2448.1 | 21667.2 | 24963.8 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 120,000 psi × 0.763 in² = 68,670 lbs
Step 2 — Torque (dry): T = 0.20 × 1.125 in × 68,670 lbs ÷ 12 = 1287.6 ft·lbs
Proof stress per SAE J429 Table 3. Stress area per ASME B1.1. K-factor per VDI 2230.
High-strength applications, heavy equipment, critical joints, suspension components, trailer hitches. Equivalent to ISO 10.9.