Stress area: 156.67 mm² · Proof load: 151,970 N · Clamp load (75%): 113,977 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 364.7 | 269.0 | 3227.9 | 3718.9 |
| Oiled | 0.15 | 273.5 | 201.7 | 2420.7 | 2788.9 |
| Zinc Plated | 0.18 | 328.3 | 242.1 | 2905.7 | 3347.7 |
| Waxed | 0.1 | 182.4 | 134.5 | 1614.4 | 1860.0 |
| MoS₂ | 0.12 | 218.8 | 161.4 | 1936.5 | 2231.1 |
| Galvanized | 0.25 | 455.9 | 336.3 | 4035.1 | 4648.9 |
Stress area: 167.25 mm² · Proof load: 162,232 N · Clamp load (75%): 121,674 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 389.4 | 287.2 | 3446.5 | 3970.8 |
| Oiled | 0.15 | 292.0 | 215.4 | 2584.4 | 2977.6 |
| Zinc Plated | 0.18 | 350.4 | 258.4 | 3101.3 | 3573.1 |
| Waxed | 0.1 | 194.7 | 143.6 | 1723.2 | 1985.4 |
| MoS₂ | 0.12 | 233.6 | 172.3 | 2067.5 | 2382.1 |
| Galvanized | 0.25 | 486.7 | 359.0 | 4307.7 | 4963.0 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 156.67 mm² = 113,977 N
Step 2 — Torque (dry): T = 0.20 × 0.0160 m × 113,977 N = 364.7 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