Stress area: 14.18 mm² · Proof load: 13,755 N · Clamp load (75%): 10,316 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 10.3 | 7.6 | 91.2 | 105.0 |
| Oiled | 0.15 | 7.7 | 5.7 | 68.2 | 78.5 |
| Zinc Plated | 0.18 | 9.3 | 6.9 | 82.3 | 94.8 |
| Waxed | 0.1 | 5.2 | 3.8 | 46.0 | 53.0 |
| MoS₂ | 0.12 | 6.2 | 4.6 | 54.9 | 63.2 |
| Galvanized | 0.25 | 12.9 | 9.5 | 114.2 | 131.5 |
Stress area: 16.13 mm² · Proof load: 15,646 N · Clamp load (75%): 11,735 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 11.7 | 8.6 | 103.6 | 119.3 |
| Oiled | 0.15 | 8.8 | 6.5 | 77.9 | 89.7 |
| Zinc Plated | 0.18 | 10.6 | 7.8 | 93.8 | 108.1 |
| Waxed | 0.1 | 5.9 | 4.4 | 52.2 | 60.2 |
| MoS₂ | 0.12 | 7.0 | 5.2 | 62.0 | 71.4 |
| Galvanized | 0.25 | 14.7 | 10.8 | 130.1 | 149.9 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 14.18 mm² = 10,316 N
Step 2 — Torque (dry): T = 0.20 × 0.0050 m × 10,316 N = 10.3 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