This specification
covers a variety of carbon, alloy, and
martensitic stainless steel nuts in the size range 1
⁄ 4 through 4 in.
and metric M6 through M100 nominal. It also covers austenitic
stainless steel nuts in the size range 1
⁄ 4 in. and M6 nominal and
above. These nuts are intended for high-pressure or high temperature service, or both. Grade
substitutions without the
purchaser’s permission are not allowed.
Bars from which the nuts are made shall be hot-wrought.
The material may be further processed by centerless grinding
or by cold drawing. Austenitic stainless steel may be solution
annealed or annealed and strain-hardened. When annealed and
strain hardened austenitic stainless steel is ordered in accordance with Supplementary Requirement S1,
the purchaser
should take special care to ensure that 8.2.2, Supplementary
Requirement S1, and Appendix X1 are thoroughly understood.
Grades | Material | UNS Number |
---|---|---|
2H | Carbon Steel | - |
2HM | Carbon Steel | - |
3 | Ferritic Stainless Steel Type 501 | S50100 |
4 | Carbon, Molybdenum Steel |
- |
6 | Ferritic Stainless Steel Type 410 | S41000 |
7 | Chromium Molybdenum Steel Type 4140, 4142, 4145, 4140H, 4142H, 4145H | - |
7M | Chromium Molybdenum Steel Type 4140, 4142, 4145, 4140H, 4142H, 4145H | - |
8 | Austenitic Stainless Steel Type 304 | S30400 |
8M | Austenitic Stainless Steel Type 316 | S31600 |
8T | Austenitic Stainless Steel Type 321 | S32100 |
16 | Chromium Molybdenum Vanadium Alloy Steel | - |
(For all grades, please visit ASTM A194 Grades)
Stainless steels for all types of Grade 6 and 8 nuts shall
be made by one of the following processes:
Electric-furnace (with separate degassing and refining
optional),
Vacuum induction furnace, or
Either of the above followed by electroslag remelting,
or consumable-arc remelting.
The steel producer shall exercise adequate control to
eliminate excessive unhomogeneity, nonmetallics, pipe,
porosity, and other defects.
Grades 1 and 2 nuts shall be hot or cold forged, or shall
be machined from hot-forged, hot-rolled, or cold-drawn bars.
All Grade 1 and 2 nuts shall be stress-relieved at a
temperature of at least 1000 °F [538 °C] after forming or
machining from bar with the following exceptions:
Nuts made by hot forging.
Nuts machined from hot-forged or hot-rolled bar.
Nuts machined from hot-forged/hot-rolled and coldfinished (max 10 % reduction in area) bar.
Nuts machined from cold-drawn and annealed (min
1000 °F [538 °C]) bar.
Grade 1 and 2 nuts made by hot forging or by
machining from hot-forged or hot-rolled bars need not be stress
relieved.
Grades 2H, 2HM, 3, 6, 6F, 7, 7M, and 16 nuts shall be
hot- or cold-forged or shall be machined from hot-forged,
hot-rolled, or cold-drawn bars and shall be heat treated to meet
the required mechanical properties. These grades shall be
uniformly reheated to the proper austenitizing temperature (a
group thus reheated being known as a quenching charge) and
quenched under substantially uniform conditions for each
quenching charge and tempered as shown below. Grades 2H,
2HM, 3, 7, and 7M shall be liquid quenched. Grades 6 and 6F
shall be quenched in liquid or inert gas. Grade 16 shall be
heated to a temperature range from 1700 to 1750 °F (925 to
955 °C) and oil quenched.
Grade | Minimum Tempering Temperature, °F |
---|---|
2H | 850 [455] |
2HM | 1150 [620] |
3 | 1050 [565] |
6 and 6F | 1100 [595] |
7 | 1100 [595] |
7M | 1150 [620] |
16 | 1200 [650] |
Nuts machined from bar heat treated in accordance with this
specification need not be reheat-treated. For Grade 2HM and
7M nuts, a final stress relief shall be done at or above the
minimum tempering temperature after all forming, machining,
and tapping operations. This final stress relief may be the
tempering operation.
Grade 6 and 6F nuts shall be tempered for a minimum
of 1 h at the temperature.
Grades 8, 8C, 8CLN, 8M, 8T, 8F, 8P, 8N, 8MN, 8R, 8S,
8LN, 8MLN, 8MLCuN, 8ML4CuN, and 9C nuts shall be hot
or cold forged, or shall be machined from hot-forged, hotrolled or cold-drawn bars.
Grades 8A, 8CA, 8CLNA, 8MA, 8TA, 8FA, 8PA, 8NA,
8MNA, 8R A, 8SA, 8LNA, 8MLNA, 8MLC uNA,
8ML4CuNA, and 9CA nuts shall be hot- or cold-forged or shall
be machined from hot-forged, hot-rolled, or cold-drawn bars
and the nuts shall subsequently be carbide-solution treated by
heating them for a sufficient time at a temperature to dissolve
chromium carbides followed by cooling at a rate sufficient to
prevent reprecipitation of the carbides.
Grade | Description and UNS Designation | Carbon | Manganese | Phospherus | SulfurE | Silicon | Chromium | Nickel | Molybdenum | Titanium | NiobiumH | Nitrogen | Copper | Selenium | Vanadium | Aluminum |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
1 | carbon | 0.15 min | 1.00 | 0.040 | 0.050 | 0.40 | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- |
2, 2HM, ad 2H | carbon | 0.40 min | 1.00 | 0.040 | 0.050 | 0.40 | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- |
3 | (501) S50100 | 0.10 min | 1.00 | 0.040 | 0.030 | 1.00 | 4.0-6.0 | --- | 00-0.65 | --- | --- | --- | --- | --- | --- | --- |
6 | (410) S41000 | 0.08-0.15 | 1.00 | 0.040 | 0.030 | 1.00 | 11.5-13.5 | --- | --- | --- | --- | --- | --- | --- | --- | --- |
6F | (416) S41600 | 0.15 | 1.25 | 0.060 | 0.15 min | 1.00 | 12.0-14.0 | --- | --- | --- | --- | --- | --- | --- | --- | --- |
6F | (416Se) S41623 | 0.15 | 1.25 | 0.060 | 0.060 | 1.00 | 12.0-14.0 | --- | --- | --- | --- | --- | --- | 0.15 min | --- | --- |
7 G , 7M G | Chromium-Molybdenum | 0.38-0.48 | 0.75-1.0 | 0.035 | 0.04 | 0.15-0.35 | 0.80-1.10 | --- | 0-0.25 | --- | --- | --- | --- | --- | --- | --- |
8, 8A | (304) S30400 | 0.08 | 2.00 | 0.045 | 0.030 | 1.00 | 18.0-20.0 | 8.0-11.0 | --- | --- | --- | --- | --- | --- | --- | --- |
8C, 8CA | (347) S34700 | 0.08 | 2.00 | 0.045 | 0.030 | 1.00 | 17.0-19.0 | 9.0-12.0 | --- | --- | 10 x carbon content min 1.10 | --- | --- | --- | --- | --- |
8CLN, 8CLNA | (347LN) S34751 | 0.005-0.020 | 2.00 | 0.045 | 0.030 | 1.00 | 17.0-19.0 | 9.0-13.0 | --- | --- | 0.20-0.50, 15 x carbon content , min | 0.06-0.10 | --- | --- | --- | --- |
8M, 8MA | (316) S31600 | 0.08 | 2.00 | 0.045 | 0.030 | 1.00 | 16.0-18.0 | 10.0-14.0 | 20-3.00 | --- | --- | --- | --- | --- | --- | --- |
8T, 8TA | (321) S32100 | 0.08 | 2.00 | 0.045 | 0.030 | 1.00 | 17.0-19.0 | 9.0-12.0 | --- | 5 x (C+N) min-0.70 max | --- | 0.10 | --- | --- | --- | --- |
8F, 8FA | (303) S30300 | 0.15 | 2.00 | 0.20 | 0.15 min | 1.00 | 17.0-19.0 | 8.0-10.0 | --- | --- | --- | --- | --- | --- | --- | --- |
8F, 8FA | (303Se) S30323 | 0.15 | 2.00 | 0.20 | 0.06 | 1.00 | 17.0-19.0 | 8.0-10.0 | --- | --- | --- | --- | --- | 0.15 min | --- | --- |
8P, 8PA | (305) S30500 | 0.12 | 2.00 | 0.045 | 0.030 | 1.00 | 17.0-19.0 | 11.0-13.0 | --- | --- | --- | --- | --- | --- | --- | --- |
8N, 8NA | (304N) S30451 | 0.08 | 2.00 | 0.045 | 0.030 | 1.00 | 18.0-20.0 | 8.0-11.0 | --- | --- | --- | 0.10-0.16 | --- | --- | --- | --- |
8LN, 8LNA | (304LN) S30453 | 0.030 | 2.00 | 0.045 | 0.030 | 1.00 | 18.0-20.0 | 8.0-11.0 | --- | --- | --- | 0.10-0.16 | --- | --- | --- | --- |
8MN, 8MA | (316N) S31651 | 0.08 | 2.00 | 0.045 | 0.030 | 1.00 | 16.0-18.0 | 10.0-13.0 | 20-3.00 | --- | --- | 0.10-0.16 | --- | --- | --- | --- |
8MLN, 8MLNA | (316LN) S31653 | 0.030 | 2.00 | 0.045 | 0.030 | 1.00 | 16.0-18.0 | 10.0-13.0 | 20-3.00 | --- | --- | 0.10-0.16 | --- | --- | --- | --- |
8R, 8RA F | (XM19) S20910 | 0.06 | 4.0-6.0 | 0.045 | 0.030 | 1.00 | 20.5-23.5 | 11.5-13.5 | 10-3.00 | --- | 0.10-0.30 | 0.20-0.40 | --- | --- | 0.10-0.30 | --- |
8S, 8SA | (Nitronic 60) S21800 | 0.10 | 7.0-9.0 | 0.060 | 0.030 | 3.5-4.5 | 16.0-18.0 | 8.0-9.0 | --- | --- | --- | 0.08-0.18 | --- | --- | --- | --- |
8MLCuN, 8MLCuNA | (254) S31254 | 0.020 | 1.00 | 0.030 | 0.010 | 0.80 | 19.5-20.5 | 17.5-18.5 | 60-6.5 | --- | --- | 0.18-0.22 | 0.50-1.00 | --- | --- | --- |
B8ML4CuN | (317) S31730 | 0.030 | 2.00 | 0.040 | 0.010 | 1.00 | 17.0-19.0 | 15.0-16.5 | 30-4.0 | --- | --- | 0.045 | 4.0-5.0 | --- | --- | --- |
9C, 9CA | (AL-6XN) N08367 | 0.030 | 2.00 | 0.040 | 0.030 | 1.00 | 20.0-22.0 | 23.5-25.5 | 6.0-7.0 | --- | --- | 0.18-0.25 | 0.75 | --- | --- | --- |
16 | Chromium Molybdenum Vanadium | 0.36-0.47 | 0.45-0.70 | 0.035 | 0.040 | 0.15-0.35 | 0.80-1.15 | --- | 0-0.65 | --- | --- | --- | --- | --- | 0.25-0.35 | 0.15 B |
Note:
A The internal addition of Bi,Se,Te, and Pb is not permitted except for Grades 6F,8F, and
8FA, in which Se is specified and required.
B Total aluminum, soluble and insoluble.
C Maximum unless minimum or range is indicated.
D Where ep ses(...) appear in this table there is no requirement ad the element need not be
determined or reported.
E Because f the degree to which sulfur segregates,product analysis for sulfur over 0.060% max
is not technologically appropriate.
F As described in Specification A276/A276M.
G Typical se l compositions used for this grade include 4140,4142,4145,4140H,4142H, and
4145H.
H Niobium (Nb) and Columbium (Cb) are alternate names for element 41 in the Periodic Table of
the Elements.
I Product Analysis-Individual determinations sometimes vary from the specified limits as
shown in the tables.The several determinations of any individual element in a heat may not vary both
above and below the specified range.Product variation limits are over for maximums,over or under for
ranges, and under for minimums,unless otherwise indicated.
Hardness Test:
Requirements:
All nuts shall meet the hardness requirements specified in Table 2.
Sample nuts of Grades 1, 2, 2H, 2HM, 3, 7, 7M, and
16 which have been given the treatment described in 8.1.5 shall
meet the minimum hardness specified in Table 2.
Number of Tests— (Grades 1, 2, 2H, 3, 7, and 16 and
all types of Grade 6):
Tests on the number of sample nuts in accordance
with the following table shall be performed by the manufacturer following all production heat
treatments:
Lot Size | Samples |
---|---|
Up to 800 | 1 |
801 to 8000 | 2 |
8001 to 22 000 | 3 |
Over 22 000 | 5 |
In addition, a hardness test shall be performed by the
manufacturer in accordance with 8.1.5 on one sample nut
selected from each nominal diameter and series from each
grade and heat number following completion of all production
heat treatments.
Number of Tests, Grades 2HM and 7M:
Each nut shall be tested in accordance with either
Specification A962/A962M or with Test Methods F606/F606M
to ensure product conformance. The use of 100 % electromagnetic testing for hardness as an alternative
to 100 % indentation
hardness testing is permissible when qualified by sampling
using indentation hardness testing. Each lot tested for hardness
electromagnetically shall be 100 % examined in accordance
with Practice E566. Following electromagnetic testing for
hardness, a random sample of a minimum of 100 pieces in each
purchase lot (as defined in 3.1.3) shall be tested by indentation
hardness methods. All samples must meet hardness requirements to permit acceptance of the lot. If any
one sample is
outside of the specified maximum or minimum hardness, the
lot shall be rejected and either reprocessed and resampled, or
tested 100 % by indentation hardness methods.
In addition, 8.1.2.2 shall be met.
Number of Tests, All Types of Grade 8— Tests on the
number of sample nuts in accordance with 8.1.2.1 shall be
performed by the manufacturer.
Test 2— In addition to the testing required by 8.1.2.1
the manufacturer shall also perform hardness tests on sample
nuts after the following test heat treatment.After completion of
all production heat treatments heat the specimen nuts to the
temperatures indicated below for 24 h, then slow cool. Test at
room temperature.
Grade A | Temperature, °F [°C] |
---|---|
1 | 850 [455] |
2, 2H, 2HM | 1000 [540] |
3, 7, 7M | 1100 [590] |
16 | 1200 [650] |
A Nuts intended to be coated with zinc or cadmium (marked in accordance with the requirements of Supplementary Requirement S8) are not subjected to the requirements of 8.1.5 (See Appendix X2).
Special Requirement, Grades 2HM and 7M—
Preparation of Grades 2HM and 7M nuts for hardness test and
the hardness test itself shall be performed with consideration to (1) protect legibility of markings;
(2) minimize exterior dimensional changes; and (3) maintain thread fit.
Proof Load Test:
Requirements— The nuts listed in Tables 3 and 4 shall
be capable of withstanding the proof loads specified therein.
Proof load testing of nuts manufactured to dimensions and
configurations other than those covered in Table 3 or Table 4 is
only required when S9 is specified in the order or inquiry
otherwise the nuts shall be cross-sectional hardness tested per
Annex A3 of Test Methods and Definitions A370. Nuts that
would require a proof load in excess of 160 000 lbf or 705 kN
shall, unless Supplementary Requirements S1 or S4 are invoked in the purchase order or contract, be
proof load tested
per Section 8, or cross sectional hardness tested per Annex A3
of Test Methods and Definitions A370.
Number of Tests:
The manufacturer shall test the number of nuts
specified in 8.1.2.1 following all production heat treatments.
Proof Load tests prevail over hardness tests in the event a
conflict exists relative to minimum strength.
Test Method— The test shall be run using a threaded
mandrel or a test bolt in accordance with Specification A962/ A962M.
Cone Proof Load Test:
Requirements— This test shall be performed only
when visible surface discontinuities become a matter of issue
between the manufacturer and the purchaser. Nuts in the size
range 1 ⁄ 4 to 1
1 ⁄ 2 in. inclusive and M6 to M36 inclusive shall be
proof load tested. Nuts not in this size range and all types of
Grade 8 nuts are not subject to this test. Also, nuts manufactured to dimensions and configurations
other than those covered by Specification A962/A962M, ASME B 1.1, ASME B
1.13M, ASME B 18.2.2, ASME B 18.2.4.6M, and ISO 4033
are not subject to the cone proof load test. The cone proof load
applied shall be determined in accordance with the Cone Proof
Load requirements in Specification A962/A962M (tables or
formulae or both) based upon the proof stresses shown in Table
5 and Table 6 of Specification A194/A194M.
Number of Tests— The manufacturer shall sample and
test the number of nuts specified in 8.1.2.1. The lot shall be considered acceptable if the sample
nut(s) withstand(s) application of the cone proof load without failure.
Grade and Type | Completed Nuts | Sample Nut after Treatment | |||
---|---|---|---|---|---|
Brinell Hardness | Rockwell Hardness | Brinell Hardness, min | Rockwell Hardness B Scale,min | ||
C Scale | B Scale | ||||
1 | 121 min | --- | 70 min | 121 | 70 |
2 | 159 to 352 | --- | 84 min | 159 | 84 |
2H to 11 ⁄ 2 in. or M36, incl | 248 to 327 | 24 to 35 | --- | 179 | 89 |
2H over 11 ⁄ 2 in. or M36 | 212 to 327 | 35 max | 95 min | 147 | 79 |
2HM and 7M | 159 to 235 | --- | 84 to 99 | 159 | 84 |
3, 7, and 16 | 248 to 327 | 24 to 35 | --- | 201 | 94 |
6 and 6F | 228 to 271 | 20 to 28 | --- | --- | --- |
8, 8C, 8CLN, 8M, 8T, 8F, 8P, 8N, 8MN, 8LN, 8MLN, 8MLCuN, 8ML4CuN, and 9C | 126 to 300 | 32 max | 60 min | --- | --- |
8A, 8CA, 8CLNA, 8MA, 8TA, 8FA, 8PA, 8NA, 8MNA, 8LNA, 8MLNA, 8MLCuNA, 8ML4CuNA, and 9CA | 126 to 1929 | --- | 60 to 90 | --- | --- |
8R, 8RA, 8S, and 8SA | 183 to 271 | 25 max | 88 min | --- | --- |
A Where ellipses (...) appear in this table there is no requirement.
Nominal Size, in. | Threads per Inch | Stress Area in. 2 | ||
---|---|---|---|---|
All Types of Grade 8, Grades 9C and 9CA | ||||
Heavy Hex H | Hex I | |||
1⁄4 | 20 | 0.0316 | 2540 | 2380 |
5⁄16 | 18 | 0.0524 | 4190 | 3930 |
3⁄8 | 16 | 0.0774 | 6200 | 5810 |
7⁄16 | 14 | 0.1063 | 8500 | 7970 |
1⁄2 | 13 | 0.1419 | 11350 | 10640 |
9⁄16 | 12 | 0.182 | 14560 | 13650 |
5⁄8 | 11 | 0.226 | 18080 | 16950 |
3⁄4 | 10 | 0.334 | 26720 | 25050 |
7⁄8 | 9 | 0.462 | 36960 | 34650 |
1 | 8 | 0.606 | 48480 | 45450 |
1 1⁄8 | 8 | 0.790 | 63200 | 59250 |
1 1⁄4 | 8 | 1.000 | 80000 | 75000 |
1 3⁄8 | 8 | 1.233 | 98640 | 92450 |
1 1⁄2 | 8 | 1.492 | 119360 | 111900 |
Note:
A See limit for proof load test. The proof load for jam nuts shall be 46 % of the tabulated
load.
B Based on proof stress of 130 000 psi.
C Based on proof stress of 120 000 psi.
D Based on proof stress of 150 000 psi.
E Based on proof stress of 135 000 psi.
F Based on proof stress of 175 000 psi.
G Based on proof stress of 150 000 psi.
H Based on proof stress of 80 000 psi.
I Based on proof stress of 75 000 psi.
Proof Stress – MPa, Minimum | |||
---|---|---|---|
Type | Grade 1 | Grades 2, 2HM, 6, 6F & 7M | Grades 2H 3, 7, & 16 |
Hex | 825 | 930 | 1035 |
Heavy Hex | 895 | 1035 | 1205 |
Nuts shall be hexagonal in shape, and in accordance
with the dimensions for the hex or heavy hex series, as
required, by ASME B 18.2.2, ASME B 18.2.4.6M, and ISO
4033. Unless otherwise specified, the American National
Standard Heavy Hex Series shall be used and nuts shall be
either double chamfered or have a machined or forged washer
face, at the option of the manufacturer, and, conform to the
angularity requirements of ASME B 18.2.2, ASME B
18.2.4.6M, and ISO 4033.
Unless otherwise specified, threads shall be in accordance with ASME B 1.1 or ASME B 1.13M, and
shall be
gauged in accordance with ASME B 1.2 and ASME B 1.13M
as described.
Nuts up to and including 1 in. nominal size shall be
UNC Series Class 2B fit. Metric nuts up to and including M24
nominal size shall be coarse thread series tolerance 6H.
Nuts over 1 in. nominal size shall be either UNC
Series Class 2B fit or 8 UN Series Class 2B fit. Unless
otherwise specified, the 8 UN series shall be furnished. Metric
nuts over M24 nominal size shall be coarse thread series
tolerance 6H.
Note:
Modification of thread dimensions may result in loss of load
carrying ability
In addition to the requirements of Specification A962/ A962M, nuts shall be legibly marked on one face with marking representing the grade, type, and applicable manufacturing process shown in Table 7. Marking of wrench flats or bearing surfaces is not permitted unless agreed upon between manufacturer and purchaser.
Grade and Type | Nuts Hot-Forged or Cold-Punched | Nuts Machined from Bar Stock | Nuts Manu-factured in Accordance with 6.6 |
---|---|---|---|
1 | 1 | 1B | --- |
2 | 2 | 2B | --- |
2H B | 2H | 2HB | --- |
2HM B,C | 2HM | 2HMB | --- |
3 | 3 | 3B | --- |
6 | 6 | 6B | --- |
6F | 6F | 6FB | --- |
7 | 7 | 7B | --- |
7L D | 7L | 7BL | --- |
7M B,C | 7M | 7MB | --- |
7ML B,D | 7ML | 7MLB | --- |
8 | 8 | 8B | 8A |
8C | 8C | 8CB | 8CA |
8CLN | 8CLN | 8CLNB | 8CLNA |
8M | 8M | 8MB | 8MA |
8T | 8T | 8TB | 8TA |
8F | 8F | 8FB | 8FA |
8P | 8P | 8PB | 8PA |
8N | 8N | 8NB | 8NA |
8MN | 8MN | 8MNB | 8MNA |
8R | 8R | 8RB | 8RA |
8S | 8S | 8SB | 8SA |
8LN | 8LN | 8LNB | 8LNA |
8MLN | 8MLN | 8MLNB | 8MLNA |
8MLCuN | 8MLCuN | 8MLCuNB | 8MLCuNA |
8ML4CuN | 8ML4CuN | 8ML4CuNB | 8ML4CuNA |
9C | 9C | 9CB | 9CA |
16 | 16 | 16B | --- |
Note:
A Where ellipses (...) appear in this table there is no requirement.
B The letters H and M indicate heat-treated nuts (see Section 6)
C An underline as a marking requirement for grades 2HM and 7M has been
removed but is permitted.
D See Supplementary Requirement S3.
One or more of the following supplementary requirements shall be applied only when specified by the purchaser in the inquiry, contract, or order. Details of these supplementary requirements shall be agreed upon in writing by the manufacturer and purchaser. Supplementary requirements shall in no way negate any requirement of the specification itself.
S1.1 Strain hardened Grades 8, 8C, 8T, 8M, 8F, 8P, 8N, or 8MN nuts may be specified. When Supplementary Requirement S1 is invoked in the order, nuts shall be machined from cold drawn bars or shall be cold forged to shape. No subsequent heat treatment shall be performed on the nuts. Nuts made in accordance with this requirement shall be proof load tested in accordance with 8.2.2.1 and shall withstand the proof load specified in Table S1.1 and Table S1.2. Testing nuts requiring proof loads over 160 000 lbf or 705 kN is only required when Supplementary Requirement S4 is invoked. The hardness limits of Table 2 do not apply to strain hardened nuts. Nuts made in accordance with this requirement shall be marked with the Grade symbol underlined.
S2.1 The purchaser’s representative may select two nuts per keg (200-lb unit [90-kg]) for sizes 5 ⁄ 8 in. and M16 and smaller, one nut per keg for sizes over 5 ⁄ 8 in. and M16 up to and including 11 ⁄ 2 in. and M36, and one nut per every two kegs for sizes larger than 11 ⁄ 2 in. and M36, which shall be subjected to the tests specified in Section 8.
S3.1 When low-temperature requirements are specified for Grade 7 nuts, the Charpy test procedures and requirements as defined in Specification A320/A320M for Grade L7 shall apply. When low-temperature requirements are specified for Grade 7M nuts, the Charpy test procedures and requirements as defined in Specification A320/A320M for Grade L7M shall apply. Charpy specimens may be taken from a sample nut, nut blank, or may be taken from separate test samples of the same heat processed through heat treatment with the nuts for which the test is to apply. Impact testing is not required when the bar stock or nut is smaller than 5 ⁄ 8 in. [16 mm] in diameter. S3.2 An “L” shall be added to the marking, as shown in Table 7, for nuts so tested.
Proof loads are not design loads.
Proof Load, kN A | |||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|
Nominal Size, mm | Thread Pitch | Stress Area, mm 2 | All Types of Grade 8 (strain hardened) | All Types of Grade 8 (strain hardened) | |||||||
Heavy Hex C | Hex B | ||||||||||
M6 | 1.0 | 20.1 | 17.3 | 15.3 | |||||||
M8 | 1.25 | 36.6 | 31.3 | 27.8 | |||||||
M10 | 1.50 | 58.0 | 49.9 | 44.1 | |||||||
M12 | 1.75 | 84.3 | 72.5 | 64.1 | |||||||
M14 | 2.0 | 115.0 | 98.9 | 87.4 | |||||||
M16 | 2.0 | 157.0 | 135.0 | 119.3 | |||||||
M20 | 2.5 | 245.0 | 210.9 | 186.2 | |||||||
M22 | 2.5 | 303.0 | 240.9 | 209.0 | |||||||
M24 | 3.0 | 353.0 | 280.6 | 243.5 | |||||||
M27 | 3.0 | 459.0 | 332.7 | 300.6 | |||||||
M30 | 3.5 | 561.0 | 406.7 | 367.5 | |||||||
M36 | 4.0 | 817.0 | 563.7 | 506.5 |
Note:
A The proof load for jam nuts shall be 46 % of the tabulated
value.
B Based on proof stress of 760 MPa up to M20 mm; 690 MPa M22 to M24 mm; 655 MPa M27 to M30;
and 620 MPa for M36.
C Based on proof stress of 860 MPa up to M20 mm; 795 MPa M22 to M24 mm; 725 MPa M27 to M30
mm; and 690 MPa for M36.
S4.1 Proof load testing of nuts requiring proof loads of over 160 000 lbf or 705 kN is required. Testing shall be performed in accordance with 8.2 to the loads required in Table S4.1 and Table S4.2. The maximum load will be based entirely on the equipment available.
S5.1 When control of nuts by actual heat analysis is required and this supplementary requirement is specified, the manufacturer shall identify the completed nuts in each shipment by the actual heat number. When this supplementary requirement is specified, a certificate including the results of the actual production tests of each test lot together with the heat chemical analysis shall be furnished by the manufacturer.
S6.1 For design metal temperatures above 1000 °F [540 °C], the material shall have a grain size of No. 7 or coarser as determined in accordance with Test Methods E112. The grain size so determined shall be reported on the Certificate of Test.
Nominal Size, mm | Thread Pitch | Stress Area, mm 2 | Proof Load, kN B | ||
---|---|---|---|---|---|
Grade 1 Heavy Hex | Grades 2, 2HM, 6, 6F, 7M Heavy Hex |
Grades 2H, 3, 7, 16 Heavy Hex |
|||
M42 | 4.5 | 1120 | 1002.4 | 1159.2 | 1349.6 |
M48 | 5 | 1470 | 1315.7 | 1521.4 | 1771.4 |
M56 | 5.5 | 2030 | 1816.9 | 2101.0 | 2446.2 |
M64 | 6 | 2680 | 2398.6 | 2773.8 | 3229.4 |
M72 | 6 | 3460 | 3096.7 | 3581.1 | 4169.3 |
Note:
A ASME B 18.2.4.6M in the size range over M36 provides dimensions only for heavy hex
nuts.
B Proof loads for nuts of larger dimensions or other thread series may be calculated by
multiplying the thread stress area times the proof stress in the notes to Table 4
or Table S1.2. The proof load for jam nuts shall be 46 % of the tabulated load.
It is the purchaser’s responsibility to specify in the
purchase order all information required by the coating facility.
Examples of such information may include but are not limited
to the following:
Reference to the appropriate coating specification
and type, thickness, location, modification to dimensions, and
hydrogen embrittlement relief.
NOTE S7.1—Modification of thread dimensions may result in loss of
load carrying ability.
Reference to Specifications A153/A153M, B633,
B695, B696, B766, F1941/F1941M, F2329/F2329M, or Test
Method F1940, or other standards.
Nuts coated with zinc shall have ZN marked after the grade symbol. Nuts coated with cadmium shall have
CD
marked after the grade symbol.
As an example the marking for zinc-coated 2H bolting components will now be 2HZN rather than 2H.
S9.1 Proof load tests of nuts made to dimensions, thread pitch, and configurations other than those covered in Table 3 or Table 4 shall be made using loads agreed upon between the manufacturer and the purchaser.
S10.1 Each nut shall be tested for hardness by indentation method and shall meet the requirements specified in Table 2.
Strain hardening is the increase in strength and hardness that results from plastic deformation below the recrystallization temperature (cold work). This effect is produced in austenitic stainless steels by reducing oversized bars to the desired final size by cold drawing or other process. The degree of strain hardening achievable in any alloy is limited by its strain hardening characteristics. In addition, the amount of strain hardening that can be produced is further limited by the variables of the process, such as the total amount of crosssection reduction, die angle and bar size. In large diameter bars, for example, plastic deformation will occur principally in the outer regions of the bar, so that the increased strength and hardness due to strain hardening is achieved predominantly near the surface of the bar. That is, the smaller the bar, the greater the penetration of strain hardening. Thus, the mechanical properties of a given strain hardened bolting compdependent not just on the alloy, but also on the size of bar from which it is machined.
Use of coated bolting components at temperatures above approximately one-half the melting point (Fahrenheit or Celsius) of the coating is not recommended unless consideration is given to the potential for liquid and solid metal embrittlement, or both. The melting point of elemental zinc is approximately 780 °F [415 °C]. Therefore, application of zinc coated bolting components should be limited to temperatures less than 390 °F [210 °C]. The melting point of cadmium is approximately 600 °F [320 °C]. Therefore, application of cadmium coated bolting components should be limited to temperatures less than 300 °F [160 °C].
bolting; chemical analysis; coated; marking on bolting components; nuts; plated