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ISO4014-4017 Class 4.8 and 6.8 and 8.8 and 10.9 and 12.9 Hexagon Head Bolts
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Product: Views:292ISO4014-4017 Class 4.8 and 6.8 and 8.8 and 10.9 and 12.9 Hexagon Head Bolts 
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Valid until: Long-term effective
Last updated: 2021-09-11 03:56
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ISO 898-1 Specification

This part of ISO 898 specifies mechanical and physical properties of bolts, screws and studs made of carbon steel and alloy steel when tested at an ambient temperature range of 10 °C to 35 °C. Fasteners — the term used when bolts, screws and studs are considered all together — that conform to the requirements of this part of ISO 898 are evaluated at that ambient temperature range. They might not retain the specified mechanical and physical properties at elevated temperatures (see Annex B) and/or lower temperatures.

 

ISO 898-1 Chemical Composition

Property class

Material and heat treatment

Chemical composition limits
(cast analysis, %) a

Tempering temperature
·c nin.

c

p
max.

s
max.

a max.

min.

max.

4.6 c, d

Carbon steel or carbon steelwith additives

-

055

0.050

0,060

Not specified

-

4.8 d

5.6 c

013

055

0.050

0,060

5.8 d

-

055

0.050

0,060

6.8 d

015

055

0.050

0,060

8.8 f

Carbon steel with additives (e.g. Boron or Mn or Cr) quenched and tempered

015.

040

0.025

0,025

0,003

425

or
Carbon steel quenched and tempered

025

055

0.025

0,025

or
Anoy steelquenched and tempered 9

020

055

0.025

0,025

9.8 f

Carbon steel with additives (e.g. Boron or Mn or Cr) quenched and tempered

015.

040

0,025

0,025

0,003

425

or
Carbon steel quenched and tempered

025

055

0.025

0,025

or
Alloy steelquenched and tempered 9

020

055

0.025

0,025

10.9 f

Carbon steel with additives (e.g. Boron or Mn or Cr) quenched and tempered

0,20 .

055

0,025

0,025

0,003

425

or
Carbon steel quenched and tempered

025

055

0.025

0,025

or
Alloy steel quenched and tempered 9

020

055

0,025

0,025

12..9 f.h.i

Alloy steel quenched and tempered 9

030

050

0.025

0,025

0,003

425

12..9 f.h.i

Carbon steel with additives (e.g. Boron or Mn or Cr or Molybdenum)quenched and tempered

028

050

0.025

0,025

0,003

380

Note:
a. In case of dispute, the product analysis applies.
b. Boron content can reach 0,005 %, provided that non-effective boron is controlled by addition of titanium and/or aluminium.
c. For cold forged fasteners of property classes 4.6 and 5.6, heat treatment of the wire used for cold forging or of the cold forged fastener itself may be necessary to achieve required ductility.
d. Free cutting steel is allowed for these property classes with the following maximum sulphur, phosphorus and lead contents: sulphur 0,34 %; phosphorus 0,11 %; lead 0,35 %.
e. In case of plain carbon boron steel with a carbon content below 0,25 % (cast analysis), the minimum manganese content shall be 0,6 % for property class 8.8 and 0,7 % for 9.8 and 10.9.
f. For the materials of these property classes, there shall be a sufficient hardenability to ensure a structure consisting of approximately 90 % martensite in the core of the threaded sections for the fasteners in the “as-hardened” condition before tempering.
g. This alloy steel shall contain at least one of the following elements in the minimum quantity given: chromium 0,30 %, nickel 0,30 %, molybdenum 0,20 %, vanadium 0,10 %. Where elements are specified in combinations of two, three or four and have alloy contents less than those given above, the limit value to be applied for steel class determination is 70 % of the sum of the individual limit values shown above for the two, three or four elements concerned.
h. A metallographically detectable white phosphorus enriched layer is not permitted for property class 12.9/12.9. It shall be detected by a suitable test method.
i. Caution is advised when the use of property class 12.9/12.9 is considered. The capability of the fastener manufacturer, the service conditions and the wrenching methods should be considered. Environments may cause stress corrosion cracking of fasteners as processed as well as those coated.

 

ISO 898-1 Mechanical Requirements

No.

Mechanical or physical property

Property class

4.6

4.8

5.6

5.8

6.8

8.8

9.8
d  ≤ 16 mm

10.9

12.9/ 12.9

d

16
mm

d >
16
mm

1

Tensile strength, Rm, MPa

nom.c

400

500

600

900

900

HXll

1200

min.

 

420

500

520

600

800

830

900

100

1220

2

Lower yield strength, ReL d, MPa

nom.c

240

-

300

-

-

-

-

-

-

-

min.

240

-

300

-

-

-

-

-

-

-

3

Stress at 0,2 % non· proportional elongation,
Rp0.2' MPa

nom.c

-

-

-

-

-

640

640

720

900

1080

min.

-

-

-

-

-

640

660

720

940

1100

4

Stress at 0,0048 d non-proportional elongation for full-size fasteners, Rpf, MPa

nom.c

-

320

-

400

480

-

-

-

-

-

min.

-

340e

-

420e

48e

-

-

-

-

-

5

Stress under proof load, Sp,f,MPa

nom.c

225

310

280

380

440

580

600

650

830

970

Proof strength ratio Sp,nom/ReL min or Sp,nom/Rp0,2 min or Sp,nom/Rpf min

min.

094

091

0.93

090

0.92

0.91

0.91

0.90

0.88

0.88

6

Percentage elongation after fracture for machined test pieces, A, %

min.

22

-

20

-

-

12

12

10

9

8

7

Percentage reduction of area after fracture for machined test pieces, Z, %

min.

-

52

48

48

44

8

Elongation after fracture for full-size fasteners, Af (see also Annex C)

min.

-

0.24

-

0.22

0.20

-

-

-

-

-

9

Head soundness

No fracture

10

Vickers hardness, HV F W 98 N

min.

120

130

155

160

190

250

255

290

320

385

max.

220 g

250

320

335

360

380

435

11

Brinell hardness, HBW F = 30 D2

min.

114

124

147

152

181

238

242

276

304

366

max.

209 g

238

304

318

342

361

414


12

Rockwell hardness, HRB

min.

67

71

79

82

89

-

max.

95,0 g

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

Height of non-decarburized thread zone, E, mm

min.

-

1/2 H1

2 /3 H1

3 /4H1

Depth of complete decarburization in the thread, G, mm

max.

-

0,015

15

Reduction of hardness after retempering, HV

max.

-

20

16

Breaking torque, MB, Nm

min.

-

in accordance with ISO 898-7

17

Impact strength, KV k, l, J

min.

-

27

-

27

27

27

27

m

18

Surface integrity in accordance with

ISO 6157-1 n

ISO 6157-3


Note:
a. Values do not apply for structural bolting.
b. For structural bolting d W M12.
c. Nominal values are specified only for the purpose of the designation system for property classes. See Clause 5.
d. In cases where the lower yield strength ReL cannot be determined, it is permissible to measure the stress at 0,2 % non-proportional elongation Rp0,2.
e. For the property classes 4.8, 5.8 and 6.8 the values for Rpf min are under investigation. The present values are given for calculation of the proof stress ratio only. They are not test values.
f. Proof loads are specified in Tables 5 and 7.
g. Hardness determined at the end of a fastener shall be 250 HV, 238 HB or 99,5 HRB maximum.
h. Surface hardness shall not be more than 30 Vickers points above the measured core hardness of the fastener when determination of both surface hardness and core hardness are carried out with HV 0,3.
i. Any increase in hardness at the surface which indicates that the surface hardness exceeds 390 HV is not acceptable.
j. Any increase in hardness at the surface which indicates that the surface hardness exceeds 435 HV is not acceptable.
k. Values are determined at a test temperature of −20 °C, see 9.14.
l.Applies to d W 16 mm.
m. Value for KV is under investigation.
n. Instead of ISO 6157-1, ISO 6157-3 may apply by agreement between the manufacturer and the purchaser.

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