ISO 898 PART 1 – 2013 (EXTRACT)
Mechanical properties of fasteners made of carbon steel and alloy steel — Part 1: Bolts, screws and studs with specified property classes — Coarse thread and fine pitch thread
- made of carbon steel or alloy steel,
- having triangular ISO metric screw thread in accordance with ISO 68-1,
- with coarse pitch thread M1,6 to M39, and fine pitch thread M8x1 to M39x3,
- with diameter/pitch combinations in accordance with ISO 261 and ISO 262, and
- having thread tolerances in accordance with ISO 965-1, ISO 965-2 and ISO 965-4. It is not applicable to set screws and similar threaded fasteners not under tensile stress (see ISO 898-5).
It does not specify requirements for such properties as weldability, corrosion resistance resistance to shear stress, torque/clamp force performance (for test method, see ISO 16047), or fatigue resistance
Chemical composition as per ISO 898-1 for typical grades
| CLASS | MATERIAL AND TREATMENT | C | C | P | S | B | TEMPERING TEMP. [C] |
| MIN | MAX | MAX | MAX | MAX | |||
| 8.8 | CARBON STEEL WITH ADDITIVES (E.G. B, MN OR CR) QUENCHED AND TEMPERED | 0.15 (D) | 0.4 | 0.025 | 0.025 | 0.003 | 425 |
| CARBON STEEL QUENCHED AND TEMPERED | 0.25 | 0.55 | 0.035 | 0.025 | |||
| 10.9 | CARBON STEEL WITH ADDITIVES (E.G. B, MN OR CR) QUENCHED AND TEMPERED | 0.15 (D) | 0.35 | 0.025 | 0.025 | 0.003 | 340 |
| CARBON STEEL QUENCHED AND TEMPERED | 0.25 | 0.55 | 0.025 | 0.025 | 0.003 | 425 | |
| CARBON STEEL WITH ADDITIVES (E.G. B, MN OR CR) QUENCHED AND TEMPERED | 0.20 (D) | 0.55 | 0.025 | 0.025 | |||
| ALLOY STEEL QUENCHED AND TEMPERED (G) | 0.2 | 0.55 | 0.025 | 0.025 | |||
| 12.9 | ALLOY STEEL QUENCHED AND TEMPERED (G) | 0.28 | 0.5 | 0.025 | 0.025 | 0.003 | 380 |
(G) ALLOY STEEL SHALL CONTAIN ONE OF THE FOLLOWING ELEMENTS: CHROMIUM 0.30%, NICKEL 0.30%, MOLYBDENUM 0.20%, VANADIUM 0.10%
Mechanical properties of screws and studs according to EN ISO 898-1:2013 Property class 4.6 to 12.9.
| No. | Mechanical properties | property classes | ||||||||||
| 4,6 | 4,8 | 5,6 | 5,8 | 6,8 | 8.8 | 8,8 | 9,8 | 10,9 | 12,9 | |||
| d<16 mmᵃ | d>16 mmᵇ | d<16 mm | ||||||||||
| 1 | Tensile strength, Rm, MPa | nom. ° | 400 | 500 | 600 | 800 | 900 | 1000 | 1200 | |||
| min. | 400 | 420 | 500 | 520 | 600 | 800 | 830 | 900 | 1040 | 1220 | ||
| 2 | Lower proof stress ReL ᵈ, MPa | nom. ᶜ | 240 | – | 300 | – | – | – | – | – | – | – |
| min. | 240 | – | 300 | – | – | – | – | – | – | – | ||
| 3 | Yield strength, Rp0.2, MPa | nom. ᶜ | – | – | – | – | – | 640 | 640 | 720 | 900 | 1080 |
| min. | – | – | – | – | – | 640 | 660 | 720 | 940 | 1100 | ||
| 4 | Yield strength at 0.0048 d for whole screw, Rpf, MPa | nom. ᶜ | – | 320 | – | 400 | 480 | – | – | – | – | – |
| min. | – | 340ᵉ | – | 420ᵉ | 480ᵉ | – | – | – | – | – | ||
| 5 | Proof stress, Spᶠ, MPa | nom. | 225 | 310 | 280 | 380 | 440 | 580 | 600 | 650 | 830 | 970 |
| Stress during proofing load testing ᴼ | 0,94 | 0,91 | 0,93 | 0,90 | 0,92 | 0,91 | 0,91 | 0,90 | 0,88 | 0,88 | ||
| 6 | Elongation after fracture (test specimen), A, % | min. | 22 | – | 20 | – | – | 12 | 12 | 10 | 9 | 8 |
| 7 | Contraction after fracture (test specimen), Z, % | min. | – | 52 | 48 | 48 | 44 | |||||
| 8 | Elongation after fracture, Af (whole screw) | min. | – | 0,24 | – | 0,22 | 0,20 | – | – | – | – | – |
| 9 | Ductility in event of head soundness test | Inget brott | ||||||||||
| 10 | Vickers hardness, HV | min. | 120 | 130 | 155 | 160 | 190 | 250 | 255 | 290 | 320 | 385 |
| F ≥ 98 N | max. | 220ᵍ | 250 | 320 | 335 | 360 | 380 | 435 | ||||
| 11 | Brinell hardness, HBW | min. | 114 | 124 | 147 | 152 | 181 | 238 | 242 | 276 | 304 | 366 |
| F = 30 D² | max. | 209ᵍ | 238 | 304 | 318 | 342 | 361 | 414 | ||||
| 12 | Rockwell hardness, HRB | min. | 67 | 71 | 79 | 82 | 89 | – | ||||
| max. | 95,0ᵍ | 99,5 | – | |||||||||
| Rockwell hardness, HRC | min. | – | 22 | 23 | 28 | 32 | 39 | |||||
| max. | – | 32 | 34 | 37 | 39 | 44 | ||||||
| 13 | Surface hardness, HV 0.3 | max. | – | h | h, i | h, j | ||||||
| 14 | Min. height of non-decarburised zone, | min. | – | ½ H1 | ⅔ H1 | ¾ H1 | ||||||
| E, mm | ||||||||||||
| Max. depth of complete decarburisation, | max. | – | 0,015 | |||||||||
| G, mm | ||||||||||||
| 15 | Reduction in hardness after re-annealing, HV | max. | – | 20 | ||||||||
| 16 | Fracture torque, MB,Nm | min. | – | regarding to ISO 898-7 | ||||||||
| 17 | Impact strength, Kᵥᵏ˴ˡ, J | min. | – | 27 | – | 27 | 27 | 27 | 27 | m | ||
| 18 | Surface defects | ISO 6157-1ⁿ | ISO | |||||||||
| 6157-3 | ||||||||||||
a) The values do not apply to structural bolts.
b) For structural bolts ≥ M12.
c) Nominal values are only specified in order to indicate property class in the designation system.
d) If the lower proof stress ReL cannot be determined, it is permitted to measure the yield strength Rp0.2.
e) For property classes 4.8, 5.8 and 6.8, the values for Rpf min are under investigation.
f) Proof loads are specified in SS-EN ISO 898-1:2013.
g) Hardness determined at the end of the screw must be max. 250 HV, 238 HB or 99.5 HRB.
h) The surface hardness may not be more than 30 Vickers units higher than the measured core hardness determined with HV 0.3.
i) No surface hardness exceeding 390 HV is permitted.
j) No surface hardness exceeding 435 HV is permitted.
Hardness requirement as per ISO 898-1 for typical grades
| HARDNESS SCALE | CLASS 8.8 | CLASS 8.8 | CLASS 10.9 | CLASS 12.9 | |
| M16 AND BELOW | ABOVE M16 | ||||
| VICKERS, HV | MIN. | 250 | 255 | 320 | 385 |
| MAX. | 320 | 335 | 380 | 435 | |
| BRINELL, HB | MIN. | 238 | 242 | 304 | 366 |
| MAX. | 304 | 318 | 361 | 414 | |
| ROCKWELL, HRC | MIN. | 22 | 23 | 32 | 39 |
| MAX. | 32 | 34 | 39 | 44 | |