ENGINEERING TOOL

M14 Bolt Torque Chart

Target preload and tightening torque ranges (min–typ–max) for M14 bolts across six property classes and five friction states. K-factor method, basis fully disclosed.

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Torque by Property Class and Friction State

Quick answer: class 8.8 · electro zinc ≈ 123 N·m (108–144); other classes and friction states below.

ClassRp0.2 (MPa)Target preload (kN)Dry / Black
K 0.18–0.22 · N·m
Electro Zinc
K 0.15–0.2 · N·m
Hot-Dip Galv.
K 0.18–0.25 · N·m
Oiled
K 0.12–0.15 · N·m
Wax / PTFE / Anti-seize
K 0.08–0.12 · N·m
4.834027.477
69–84
65
57–77
84
69–96
50
46–57
38
31–46
8.864051.5144
130–159
123
108–144
159
130–180
94
87–108
72
58–87
10.994075.7212
191–233
180
159–212
233
191–265
138
127–159
106
85–127
12.9110088.6248
223–273
211
186–248
273
223–310
161
149–186
124
99–149
A2-7045036.2101
91–112
86
76–101
112
91–127
66
61–76
51
41–61
A4-8060048.3135
122–149
115
101–135
149
122–169
88
81–101
68
54–81

Cell shows the typical value; the small line below is the range (min–max).

Fine-Thread Torque Matrix

Fine-thread series (M14 × 1.5 mm) target preload and tightening torque ranges, same basis as the coarse chart; the fine-thread stress area As follows ISO 898-1:2013 Table 6 (this page takes M14 As = 125 mm²).

ClassRp0.2 (MPa)Target preload (kN)Dry / Black
K 0.18–0.22 · N·m
Electro Zinc
K 0.15–0.2 · N·m
Hot-Dip Galv.
K 0.18–0.25 · N·m
Oiled
K 0.12–0.15 · N·m
Wax / PTFE / Anti-seize
K 0.08–0.12 · N·m
4.834029.783
75–92
71
62–83
92
75–104
54
50–62
42
33–50
8.864056157
141–172
133
118–157
172
141–196
102
94–118
78
63–94
10.994082.3230
207–253
196
173–230
253
207–288
150
138–173
115
92–138
12.9110096.3270
243–296
229
202–270
296
243–337
175
162–202
135
108–162
A2-7045039.4110
99–121
94
83–110
121
99–138
72
66–83
55
44–66
A4-8060052.5147
132–162
125
110–147
162
132–184
96
88–110
74
59–88

Cell shows the typical value; the small line below is the range (min–max).

Basis of Calculation & Sources

Torque follows the K-factor (nut factor) method T = K·D·F: D is the nominal diameter and F the target preload = 70% of Rp0.2 × thread stress area (M14 As = 115 mm²). Yield strengths are published values from ISO 898-1 (carbon/alloy steel) and ISO 3506-1 (stainless A2/A4). K follows published empirical ranges per friction condition (Machinery's Handbook; the wax/PTFE/anti-seize band K≈0.10 follows Machine Design test data). The grease/MoS₂ band (K≈0.11) nearly overlaps anti-seize and is available in the calculator instead of a separate column.

Stainless note: A2/A4 austenitic thread pairs gall easily under frictional heating. Always apply anti-seize and follow the Wax/PTFE/Anti-seize column (K≈0.10).

Boundary: this chart is a simplified K-factor estimate, not a full VDI 2230 analysis (which accounts for joint resilience, embedment and assembly method). Friction is the dominant variable — no single torque value exists without its friction state. Always follow the design specification or manufacturer torque table.

FAQ

What is the tightening torque for an M14 class 8.8 bolt?

It depends on the friction state (typical values at 70% of Rp0.2 target preload): oiled ≈ 94 N·m, electro zinc ≈ 123 N·m, hot-dip galvanized ≈ 159 N·m, dry/black ≈ 144 N·m, anti-seize ≈ 72 N·m. See the matrix above for ranges — no single torque value exists without its friction state.

What is the target preload for an M14 bolt?

At 70% of Rp0.2: class 4.8 ≈ 27.4 kN, 8.8 ≈ 51.5 kN, 10.9 ≈ 75.7 kN; stainless A2-70 ≈ 36.2 kN and A4-80 ≈ 48.3 kN.

Can I use carbon-steel torque values for stainless M14 (A2-70/A4-80)?

No. The classes have different yield strengths (A2-70 = 450 MPa, A4-80 = 600 MPa), so target preloads differ; and stainless thread pairs gall easily — always apply anti-seize and follow the Wax/PTFE/Anti-seize column (K≈0.10).

What basis are these torque values calculated on?

The K-factor method T = K·D·F with target preload = 70% of Rp0.2 × stress area (yield strengths per ISO 898-1 / ISO 3506-1 published values) and K per published empirical friction ranges. Estimated values, not assembly instructions; run a full VDI 2230 analysis for critical joints.

Related References

Disclaimer: This chart is an engineering estimation for selection and budgeting only. It does not constitute assembly instructions or acceptance criteria.

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