Stress area: 36.61 mm² · Proof load: 35,512 N · Clamp load (75%): 26,634 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 42.6 | 31.4 | 377.0 | 434.4 |
| Oiled | 0.15 | 32.0 | 23.6 | 283.2 | 326.3 |
| Zinc Plated | 0.18 | 38.4 | 28.3 | 339.9 | 391.6 |
| Waxed | 0.1 | 21.3 | 15.7 | 188.5 | 217.2 |
| MoS₂ | 0.12 | 25.6 | 18.9 | 226.6 | 261.0 |
| Galvanized | 0.25 | 53.3 | 39.3 | 471.7 | 543.5 |
Stress area: 39.17 mm² · Proof load: 37,995 N · Clamp load (75%): 28,496 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 45.6 | 33.6 | 403.6 | 465.0 |
| Oiled | 0.15 | 34.2 | 25.2 | 302.7 | 348.7 |
| Zinc Plated | 0.18 | 41.0 | 30.2 | 362.9 | 418.1 |
| Waxed | 0.1 | 22.8 | 16.8 | 201.8 | 232.5 |
| MoS₂ | 0.12 | 27.4 | 20.2 | 242.5 | 279.4 |
| Galvanized | 0.25 | 57.0 | 42.0 | 504.5 | 581.2 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 36.61 mm² = 26,634 N
Step 2 — Torque (dry): T = 0.20 × 0.0080 m × 26,634 N = 42.6 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