Stress area: 0.462 in² · Proof load: 55,440 lbs · Clamp load (75%): 41,580 lbs
| Surface Condition | K Factor | ft·lbs | N·m | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 606.4 | 822.2 | 7276.8 | 8384.1 |
| Oiled | 0.15 | 454.8 | 616.6 | 5457.6 | 6287.6 |
| Zinc Plated | 0.18 | 545.7 | 739.9 | 6548.4 | 7544.9 |
| Waxed | 0.1 | 303.2 | 411.1 | 3638.4 | 4192.1 |
| MoS₂ | 0.12 | 363.8 | 493.2 | 4365.6 | 5029.3 |
| Galvanized | 0.25 | 758.0 | 1027.7 | 9096.0 | 10479.7 |
Stress area: 0.509 in² · Proof load: 61,080 lbs · Clamp load (75%): 45,810 lbs
| Surface Condition | K Factor | ft·lbs | N·m | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 668.1 | 905.8 | 8017.2 | 9236.6 |
| Oiled | 0.15 | 501.0 | 679.3 | 6012.0 | 6927.0 |
| Zinc Plated | 0.18 | 601.3 | 815.3 | 7215.6 | 8313.8 |
| Waxed | 0.1 | 334.0 | 452.8 | 4008.0 | 4617.3 |
| MoS₂ | 0.12 | 400.8 | 543.4 | 4809.6 | 5541.2 |
| Galvanized | 0.25 | 835.1 | 1132.2 | 10021.2 | 11545.3 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 120,000 psi × 0.462 in² = 41,580 lbs
Step 2 — Torque (dry): T = 0.20 × 0.875 in × 41,580 lbs ÷ 12 = 606.4 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.