Stress area: 58.0 mm² · Proof load: 56,260 N · Clamp load (75%): 42,195 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 84.4 | 62.3 | 747.0 | 860.6 |
| Oiled | 0.15 | 63.3 | 46.7 | 560.3 | 645.5 |
| Zinc Plated | 0.18 | 76.0 | 56.1 | 672.7 | 775.0 |
| Waxed | 0.1 | 42.2 | 31.1 | 373.5 | 430.3 |
| MoS₂ | 0.12 | 50.6 | 37.3 | 447.8 | 516.0 |
| Galvanized | 0.25 | 105.5 | 77.8 | 933.8 | 1075.8 |
Stress area: 61.2 mm² · Proof load: 59,364 N · Clamp load (75%): 44,523 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 89.0 | 65.6 | 787.7 | 907.6 |
| Oiled | 0.15 | 66.8 | 49.3 | 591.2 | 681.2 |
| Zinc Plated | 0.18 | 80.1 | 59.1 | 708.9 | 816.8 |
| Waxed | 0.1 | 44.5 | 32.8 | 393.9 | 453.8 |
| MoS₂ | 0.12 | 53.4 | 39.4 | 472.6 | 544.5 |
| Galvanized | 0.25 | 111.3 | 82.1 | 985.1 | 1134.9 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 58.0 mm² = 42,195 N
Step 2 — Torque (dry): T = 0.20 × 0.0100 m × 42,195 N = 84.4 N·m
Proof stress per ISO 898-1:2013 Table 4. Stress area per ISO 898-1 Annex A. K-factor per VDI 2230.
Socket head cap screws, racing/motorsport, aerospace, maximum strength applications — highest standard grade