Stress area: 8.78 mm² · Proof load: 8,517 N · Clamp load (75%): 6,387 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 5.1 | 3.8 | 45.1 | 52.0 |
| Oiled | 0.15 | 3.8 | 2.8 | 33.6 | 38.7 |
| Zinc Plated | 0.18 | 4.6 | 3.4 | 40.7 | 46.9 |
| Waxed | 0.1 | 2.6 | 1.9 | 23.0 | 26.5 |
| MoS₂ | 0.12 | 3.1 | 2.3 | 27.4 | 31.6 |
| Galvanized | 0.25 | 6.4 | 4.7 | 56.6 | 65.3 |
Stress area: 9.79 mm² · Proof load: 9,496 N · Clamp load (75%): 7,122 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 5.7 | 4.2 | 50.4 | 58.1 |
| Oiled | 0.15 | 4.3 | 3.2 | 38.1 | 43.8 |
| Zinc Plated | 0.18 | 5.1 | 3.8 | 45.1 | 52.0 |
| Waxed | 0.1 | 2.8 | 2.1 | 24.8 | 28.6 |
| MoS₂ | 0.12 | 3.4 | 2.5 | 30.1 | 34.7 |
| Galvanized | 0.25 | 7.1 | 5.2 | 62.8 | 72.4 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 8.78 mm² = 6,387 N
Step 2 — Torque (dry): T = 0.20 × 0.0040 m × 6,387 N = 5.1 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