ASTM F467-13(2018)

This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the
Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Designation:F467 −13 (Reapproved 2018)
Standard Specification for
Nonferrous Nuts for General Use
ThisstandardisissuedunderthefixeddesignationF467;thenumberimmediatelyfollowingthedesignationindicatestheyearoforiginal
adoption or, in the case of revision, the year of last revision.Anumber in parentheses indicates the year of last reapproval.Asuperscript
epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope* E18 Test Methods for Rockwell Hardness of Metallic Ma-
terials
1.1 This specification covers the requirements for commer-
E29 Practice for Using Significant Digits in Test Data to
cial wrought nonferrous nuts 0.250 to 1.500 in. inclusive in
Determine Conformance with Specifications
diameterinanumberofalloysincommonuseandintendedfor
E34 Test Methods for Chemical Analysis of Aluminum and
general service applications.
Aluminum-Base Alloys (Withdrawn 2017)
1.2 Applicablebolts,capscrews,andstudsforusewithnuts
E38 Methods for Chemical Analysis of Nickel-Chromium
covered by this specification are covered by Specification
and Nickel-Chromium-Iron Alloys (Withdrawn 1989)
F468.
E53 Test Method for Determination of Copper in Unalloyed
Copper by Gravimetry
1.3 The values stated in inch-pound units are to be regarded
as standard. No other units of measurement are included in this E54 Test Methods for ChemicalAnalysis of Special Brasses
and Bronzes (Withdrawn 2002)
standard.
E55 Practice for Sampling Wrought Nonferrous Metals and
NOTE 1—This specification is the inch-pound companion to Specifica-
Alloys for Determination of Chemical Composition
tionF467M;therefore,noSIequivalentsarepresentedinthespecification.
E62 Test Methods for Chemical Analysis of Copper and
1.4 This international standard was developed in accor-
CopperAlloys(PhotometricMethods)(Withdrawn2010)
dance with internationally recognized principles on standard-
E75 Test Methods for Chemical Analysis of Copper-Nickel
ization established in the Decision on Principles for the
and Copper-Nickel-Zinc Alloys (Withdrawn 2010)
Development of International Standards, Guides and Recom-
E76 Test Methods for Chemical Analysis of Nickel-Copper
mendations issued by the World Trade Organization Technical
Alloys (Withdrawn 2003)
Barriers to Trade (TBT) Committee.
E92 Test Methods for Vickers Hardness and Knoop Hard-
ness of Metallic Materials
2. Referenced Documents
E101 TestMethodforSpectrographicAnalysisofAluminum
2.1 ASTM Standards:
and Aluminum Alloys by the Point-to-Plane Technique
B154 Test Method for Mercurous Nitrate Test for Copper
(Withdrawn 1996)
Alloys
E120 Test Methods for Chemical Analysis of Titanium and
B574 Specification for Low-Carbon Nickel-Chromium-
Titanium Alloys (Withdrawn 2003)
Molybdenum, Low-Carbon Nickel-Molybdenum-
E165 Practice for Liquid Penetrant Examination for General
Chromium, Low-Carbon Nickel-Molybdenum-
Industry
Chromium-Tantalum, Low-Carbon Nickel-Chromium-
E227 Test Method for Optical Emission Spectrometric
Molybdenum-Copper, and Low-Carbon Nickel-
Analysis of Aluminum and Aluminum Alloys by the
Chromium-Molybdenum-Tungsten Alloy Rod
Point-to-Plane Technique (Withdrawn 2002)
D3951 Practice for Commercial Packaging
E354 Test Methods for Chemical Analysis of High-
Temperature,Electrical,Magnetic,andOtherSimilarIron,
Nickel, and Cobalt Alloys
This specification is under the jurisdiction of ASTM Committee F16 on
E478 Test Methods for ChemicalAnalysis of CopperAlloys
Fasteners and is the direct responsibility of Subcommittee F16.04 on Nonferrous
E1409 Test Method for Determination of Oxygen and Nitro-
Fasteners.
gen in Titanium and TitaniumAlloys by Inert Gas Fusion
Current edition approved Sept. 1, 2018. Published September 2018. Originally
ε2
F468 Specification for Nonferrous Bolts, Hex Cap Screws,
approved in 1976. Last previous edition approved in 2013 as F467 – 13 . DOI:
10.1520/F0467-13R18.
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Standards volume information, refer to the standard’s Document Summary page on The last approved version of this historical standard is referenced on
the ASTM website. www.astm.org.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
F467−13 (2018)
Socket Head Cap Screws, and Studs for General Use
Alloy Condition
F606/F606M Test Methods for Determining the Mechanical
Copper (all alloys) As formed or stress relieved at manufacturer’s
Properties of Externally and Internally Threaded
option
Fasteners, Washers, Direct Tension Indicators, and Rivets Nickel alloys 400 and 405 As formed or stress relieved at manufacturer’s
option
F1470 Practice for Fastener Sampling for Specified Me-
Nickel alloy 500 Solution annealed and aged
chanical Properties and Performance Inspection
Aluminum alloys:
4 2024-T4 Solution treated and naturally aged
2.2 ASME Standards:
6061-T6 Solution treated and artificially aged
B 1.1 Unified Inch Screw Threads (UN and UNR Thread
6262-T9 Solution treated, artificially aged, and cold
worked
Form)
Titanium As formed
B 18.2.2 Square and Hex Nuts
625 Annealed
4.2.3 Stress Relieving—Whenrequired,stressrelievingshall
3. Ordering Information
be specified by the purchaser for all copper alloys and nickel
3.1 Orders for nuts under this specification shall include the
alloys 400 and 405.
following information:
3.1.1 Quantity (number of pieces of each item and size); 5. Chemical Composition
3.1.2 Name of item;
5.1 Chemical Composition—The nuts shall conform to the
3.1.3 Size (diameter and threads per inch);
chemical composition specified in Table 1 for the specified
3.1.4 Alloy number (Table 1);
alloy.
3.1.5 Stress relieving, if required (4.2.3);
5.2 Manufacturer’s Analysis:
3.1.6 “Shipment lot” testing, as required (Section 9);
5.2.1 Except as provided in 5.2.2, when test reports are
3.1.7 Source inspection, if required (Section 14);
required on the inquiry or purchase order (3.1.8), the manu-
3.1.8 Certificate of compliance or test report, if required
facturer shall make individual analyses of randomly selected
(Section 16); finished nuts from the product to be shipped and report the
results to the purchaser. Alternatively, if heat and lot identities
3.1.9 Additional requirements, if any, to be specified on
have been maintained, the analysis of the raw material from
the purchase order (4.2.1, 7.2, 8.2, 12.1, and 13.1),
which the nuts have been manufactured may be reported
3.1.10 Supplementary requirements, if any; and
instead of product analysis.
3.1.11 ASTM designation (including year or published
5.2.2 For aluminum nuts, instead of 5.2.1, the manufacturer
date).
may furnish a certificate of conformance certifying compliance
NOTE 2—A typical ordering description is as follows: 10 000 pieces,
with the chemical composition specified in Table 1.
Hex Nut, 0.250" -20, Alloy 270, Furnish Certificate of Compliance,
Supplementary Requirement S 1, ASTM Specification F 467-XX
5.3 Product Analysis:
5.3.1 Product analyses may be made by the purchaser from
4. Materials and Manufacture
finished products representing each lot. The chemical compo-
sition thus determined shall conform to the requirements in
4.1 Materials:
Table 1.
4.1.1 The nuts shall be manufactured from material having
5.3.2 In the event of disagreement, a referee chemical
a chemical composition conforming to the requirements in
analysis of samples from each lot shall be made in accordance
Table 2 and capable of developing the required mechanical
with 12.1 and 13.1.
properties for the specified alloy in the finished fastener. See
Specification B574 for nickel alloys.
6. Mechanical Properties
4.1.2 The starting condition of the raw material shall be at
the discretion of the fastener manufacturer but shall be such
6.1 Thenutsshallbetestedinaccordancewiththemechani-
that the finished products conform to all the specified require-
cal testing requirements for the applicable type and shall meet
ments.
the mechanical requirements in Table 2 for the specified alloy.
4.2 Manufacture:
6.2 Wherebothproofloadandhardnesstestsareperformed,
4.2.1 Forming—Unless otherwise specified, the nuts shall
the proof load test results shall take precedence for acceptance
be hot pressed, cold formed, or machined from suitable purposes.
material at the option of the manufacturer.
7. Dimensions
4.2.2 Condition—Except as provided in 4.2.3, the nuts shall
be furnished in the condition specified below:
7.1 Nuts—Unless otherwise specified, the dimensions of
nuts shall be in accordance with the requirements of ASME
B18.2.2.
Available from American Society of Mechanical Engineers (ASME), ASME
7.2 Threads—Unless otherwise specified, the nuts shall
International Headquarters, Two Park Ave., New York, NY 10016-5990, http://
www.asme.org. have Class 2B threads in accordance with ASME B1.1.
F467−13 (2018)
TABLE 1 Chemical Requirements
Composition, %
Copper and Copper-Base Alloys
UNS
Mang
Designation
Copper, Iron, Nickel, Phos- Zinc, Lead, Arsenic,
Alloy General Name Aluminum anese, Silicon Tin
A
Number
min max max phorus max max max
max
C11000 110 ETP copper 99.9
C26000 260 brass 68.5–71.5 0.05 balance 0.07
C27000 270 brass 63.0–68.5 0.07 balance 0.10
C46200 462 naval brass 62.0–65.0 0.10 balance 0.20 0.5–1.0
C46400 464 naval brass 59.0–62.0 0.10 balance 0.20 0.5–1.0
A
C51000 510 phosphor bronze balance 0.10 0.03–0.35 0.30 0.05 4.2–5.8
B C
C61300 613 aluminum bronze 6.0– 2.0–3.0 0.10 0.15 0.015 0.10 0.05 0.01 0.20–0.50
7.5
D
C61400 614 aluminum bronze 6.0– 88.0 1.5–3.5 1.0
8.0
D
C63000 630 aluminum bronze 9.0– 78.0 2.0–4.0 1.5 4.0–5.5 0.25 max 0.20 max
11.0
D E
C64200 642 aluminum silicon bronze 6.3– 88.65 0.30 0.10 0.25 1.5–2.2 0.50 0.05 0.20 max 0.15
7.6
D
C65100 651 silicon bronze 96.0 0.8 0.7 0.8–2.0 1.5 0.05
D
C65500 655 silicon bronze 94.8 0.8 1.5 0.6 2.8–3.8 1.5 0.05
D
C66100 661 silicon bronze 94.0 0.25 1.5 2.8–3.5 1.5 0.20–0.8
C67500 675 manganese bronze 0.25 max 57.0–60.0 0.8–2.0 0.05–0.5 balance 0.20 0.5–1.5
D C
C71000 710 cupro-nickel 74.0 0.60 1.00 19.0–23.0 1.00 0.05
D C
C71500 715 cupro-nickel 65.0 0.40–0.7 1.00 29.0–33.0 1.00 0.05
A
Elements shown as balance shall be arithmetically computed by deducting the sum of the other named elements from 100.
B
Copper plus specified elements = 99.8 min; copper plus silver = 88.5–91.5.
C
Cobalt is to be counted as nickel.
D
Minimum content of copper plus all other elements with specified limits shall be 99.5 %.
E
An alloy containing as high as 2.6 % silicon is acceptable provided the sum of all the elements other than copper, silicon, and iron does not exceed 0.30 %.

F467−13 (2018)
TABLE1 Continued
Nickel and Nickel-Base Alloys
UNS
Manga Phos
Designa- Alumi- Carbon, Chro- Iron, Silicon, Cobalt, Molyb- Sulfur, Vana- Tung- Nio-
A A
Alloy General Name Copper nese, Nickel phous, Titanium
†
tion num max mium max max max denum max dium sten bium
max max
Number
N10001 335 Ni-Mo 0.05 1.0 4.0– 1.0 balance 0.025 1.00 2.50 26.0– 0.030 0.2–
max 6.0 30.0 0.4
N10276 276 Ni-Mo-Cr 0.02 14.5– 4.0– 1.00 balance 0.040 0.08 2.50 15.0– 0.030 0.35 3.0–
16.5 7.0 17.0 max 4.5
B
N04400 400 Ni-Cu 0.3 balance 2.5 2.0 63.0– 0.5 0.024
Class A 70.0
B
N04405 405 Ni-Cu 0.3 balance 2.5 2.0 63.0– 0.5 0.025–
Class B 70.0 0.060
B
N05500 500 Ni-Cu-Al 2.30– 0.25 balance 2.0 1.5 63.0– 0.5 0.35– 0.01
3.15 70.0 0.85
N06059 59 Ni– 0.1– 0.010 22.0– 0.5 1.5 0.5 balance 0.015 0.10 0.3 15.0– 0.010
Cr-Mo 0.4 max 24.0 max max max max max max 16.5 max
C
N06625 625 Ni-Cr-Mo-Cb 0.40 0.10 20.0– 5.0 0.50 58.0 0.015 0.50 0.40 1.00 8.0– 0.015 3.2–
max 23.0 max min max max max 10.0 4.2
N06686 686 Ni-Cr-Mo-W 0.010 19.0– 5.0 0.75 balance 0.04 0.08 0.02– 15.0– 0.02 3.0–
max 23.0 max max max max 0.25 17.0 max 4.4
A
Elements shown as balance shall be arithmetically computed by deducting the sum of the other named elements from 100.
B
Cobalt is to be counted as nickel.
C
Alloy 625 material shall be refined using the electroslag remelting process (ESR), or the vacuum arc remelting process (VAR).

F467−13 (2018)
TABLE1 Continued
Composition, %
A
Aluminum-Base Alloys
UNS
Other Elements,
Desig-
Al- General Alumi- Chro- Iron, Manganese, Silicon, Titanium, Zinc, Magne- max
nation Copper
A
loy Name num mium max max max max max sium
Num-
Each Total
ber
B
A92024 2024 Aluminum balance 0.10 3.8– 0.50 0.30– 0.50 0.15 0.25 1.2– 0.05 0.15
2024 max 4.9 0.9 1.8
A96061 6061 Aluminum balance 0.04– 0.15– 0.7 0.15 0.40– 0.15 0.25 0.8– 0.05 0.15
6061 0.35 0.40 0.8 1.2
C
A96262 6262 Aluminum balance 0.04– 0.15– 0.7 0.15 0.40– 0.15 0.25 0.8–
6262 0.14 0.40 0.8 1.2
A
Analysis shall regularly be made only for the elements specified in this table. If, however, the presence of other elements is suspected or indicated in amounts greater than the specified limits, further analysis shall be
made to determine that these elements are not present in excess of the specified limits.
B
Titanium + zirconium 0.20 %, max.
C
Lead 0.4–0.7 %; bismuth 0.4–0.7 %.

F467−13 (2018)
TABLE1 Continued
A
Titanium and Titanium-Base Alloys
B
UNS
Residuals
Car- Nitro- Oxy- Molyb- Zirco- Sili Ruthe-
Des- General Alumi- Iron, Tita- Hydro- Palla- Vana- Chro- Tin,
Alloy bon, gen, gen, denum, nium, con, nium,
each, total,
ignation Name num, Al Fe nium, Ti gen, H dium, Pd dium, V mium, Cr Sn
C N O Mo Zr Si Ru
max max
Number
R50250 1 Titanium Gr 1 0.10 0.20 balance 0.0125 0.05 0.18 0.1 0.4
R50400 2 Titani
...