Stress area: 115.44 mm² · Proof load: 111,977 N · Clamp load (75%): 83,983 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 235.2 | 173.5 | 2081.7 | 2398.4 |
| Oiled | 0.15 | 176.4 | 130.1 | 1561.3 | 1798.8 |
| Zinc Plated | 0.18 | 211.6 | 156.1 | 1872.8 | 2157.7 |
| Waxed | 0.1 | 117.6 | 86.7 | 1040.8 | 1199.2 |
| MoS₂ | 0.12 | 141.1 | 104.1 | 1248.8 | 1438.8 |
| Galvanized | 0.25 | 293.9 | 216.8 | 2601.2 | 2997.0 |
Stress area: 124.55 mm² · Proof load: 120,814 N · Clamp load (75%): 90,610 N
| Surface Condition | K Factor | N·m | ft·lbs | in·lbs | kgf·cm |
|---|---|---|---|---|---|
| Plain/Dry | 0.2 | 253.7 | 187.1 | 2245.4 | 2587.0 |
| Oiled | 0.15 | 190.3 | 140.4 | 1684.3 | 1940.5 |
| Zinc Plated | 0.18 | 228.3 | 168.4 | 2020.6 | 2328.0 |
| Waxed | 0.1 | 126.9 | 93.6 | 1123.2 | 1294.0 |
| MoS₂ | 0.12 | 152.2 | 112.3 | 1347.1 | 1552.0 |
| Galvanized | 0.25 | 317.1 | 233.9 | 2806.6 | 3233.5 |
Formula: T = K × D × F
Step 1 — Clamp load: F = 0.75 × 970 MPa × 115.44 mm² = 83,983 N
Step 2 — Torque (dry): T = 0.20 × 0.0140 m × 83,983 N = 235.2 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