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    ASTM F467/F467M Specifications

    Standard requirements for nonferrous nuts used in general applications.

    Scope

    ASTM F467 (this page follows ASTM F467-13ε2) covers the requirements for commercial wrought nonferrous nuts 0.250 to 1.500 in. (1/4 to 1 1/2 in.) inclusive in diameter, in a number of alloys in common use and intended for general service applications. Values are in inch-pound units; F467M is the metric companion specification. Applicable bolts, cap screws and studs for use with these nuts are covered by ASTM F468. Unless otherwise specified, nut dimensions are to ASME B18.2.2 and threads are Class 2B to ASME B1.1.

    ASTM F467/F467M Chemical Composition

    ASTM F467/F467M Copper and Copper-Base Alloys

    UNS Designation
    Number
    Alloy General
    Name
    Al Cu,
    min
    Fe,
    max
    Mn,
    max
    Ni,
    max
    P Si Zn,
    max A
    Pb,
    max
    Tin As,
    max
    ASTM F467/F467M Grade C11000 110 ETP copper . . . 99.9 . . . . . . . . . . . . . . . . . . . . . . . . . . .
    ASTM F467/F467M Grade C26000 260 brass . . . 68.5-71.5 0.05 . . . . . . . . . . . . balance 0.07 . . . . . .
    ASTM F467/F467M Grade C27000 270 brass . . . 63.0-68.5 0.07 . . . . . . . . . . . . balance 0.10 . . . . . .
    ASTM F467/F467M Grade C46200 462 naval brass . . . 62.0-65.0 0.10 . . . . . . . . . . . . balance 0.20 0.5-1.0 . . .
    ASTM F467/F467M Grade C46400 464 naval brass . . . 59.0-62.0 0.10 . . . . . . . . . . . . balance 0.20 0.5-1.0 . . .
    ASTM F467/F467M Grade C51000 510 phosphor bronze . . . balance A 0.10 . . . . . . 0.03-0.35 . . . 0.30 0.05 4.2-5.8 . . .
    ASTM F467/F467M Grade C61300 613 aluminum bronze 6.0- 7.5 B 2.0-3.0 0.10 0.15 C 0.015 0.10 0.05 0.01 0.20-0.50 . . .
    ASTM F467/F467M Grade C61400 614 aluminum bronze 6.0- 8.0 88.0 D 1.5-3.5 1.0 . . . . . . . . . . . . . . . . . . . . .
    ASTM F467/F467M Grade C63000 630 aluminum bronze 9.0- 11.0 78.0 D 2.0-4.0 1.5 4.0-5.5 . . . 0.25 max . . . . . . 0.20 max . . .
    ASTM F467/F467M Grade C64200 642 aluminum silicon bronze 6.3- 7.6 88.65 D 0.30 0.10 0.25 . . . 1.5-2.2 E 0.50 0.05 0.20 max 0.15
    ASTM F467/F467M Grade C65100 651 silicon bronze . . . 96.0 D 0.8 0.7 . . . . . . 0.8-2.0 1.5 0.05 . . . . . .
    ASTM F467/F467M Grade C65500 655 silicon bronze . . . 94.8 D 0.8 1.5 0.6 . . . 2.8-3.8 1.5 0.05 . . . . . .
    ASTM F467/F467M Grade C66100 661 silicon bronze . . . 94.0 D 0.25 1.5 . . . . . . 2.8-3.5 1.5 0.20-0.8 . . . . . .
    ASTM F467/F467M Grade 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 . . .
    ASTM F467/F467M Grade C71000 710 cupro-nickel . . . 74.0 D 0.60 1.00 19.0-23.0 C . . . . . . 1.00 0.05 . . . . . .
    ASTM F467/F467M Grade C71500 715 cupro-nickel . . . 65.0 D 0.40-0.7 1.00 29.0-33.0 C . . . . . . 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 %.

    ASTM F467/F467M Nickel and Nickel-Base Alloys

    UNS Designation Number Alloy General Name Al C, max Cr Cu A Fe, max Mn, max Ni A P, max Si, max Ti Co, max Mo S, max V W Cb †
    ASTM F467/F467M Grade N10001 335 Ni-Mo . . . 0.05 1.0 max . . . 4.0- 6.0 1.0 balance 0.025 1.00 . . . 2.50 26.0- 30.0 0.030 0.2- 0.4 . . . . . .
    ASTM F467/F467M Grade N10276 276 Ni-Mo-Cr . . . 0.02 14.5- 16.5 . . . 4.0- 7.0 1.00 balance 0.040 0.08 . . . 2.50 15.0- 17.0 0.030 0.35 max 3.0- 4.5 . . .
    ASTM F467/F467M Grade N04400 400 Ni-Cu Class A . . . 0.3 . . . balance 2.5 2.0 63.0- 70.0 . . . 0.5 . . . B . . . 0.024 . . . . . . . . .
    ASTM F467/F467M Grade N04405 405 Ni-Cu Class B . . . 0.3 . . . balance 2.5 2.0 63.0- 70.0 . . . 0.5 . . . B . . . 0.025- 0.060 . . . . . . . . .
    ASTM F467/F467M Grade N05500 500 Ni-Cu-Al 2.30- 3.15 0.25 . . . balance 2.0 1.5 63.0- 70.0 . . . 0.5 0.35- 0.85 B . . . 0.01 . . . . . . . . .
    ASTM F467/F467M Grade N06059 59 Ni- Cr-Mo 0.1- 0.4 0.010 max 22.0- 24.0 0.5 max 1.5 max 0.5 max balance 0.015 max 0.10 max . . . 0.3 max 15.0- 16.5 0.010 max . . . . . . . . .
    ASTM F467/F467M Grade N06625 625C Ni-Cr-Mo-Cb 0.40 max 0.10 20.0- 23.0 . . . 5.0 max 0.50 58.0 min 0.015 0.50 max 0.40 max 1.00 max 8.0- 10.0 0.015 . . . . . . 3.2- 4.2
    ASTM F467/F467M Grade N06686 686 Ni-Cr-Mo-W . . . 0.010 max 19.0- 23.0 . . . 5.0 max 0.75 max balance 0.04 max 0.08 max 0.02- 0.25 . . . 15.0- 17.0 0.02 max . . . 3.0- 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).

    ASTM F467/F467M Aluminum-Base Alloys A

    UNS DesignationNumber Alloy GeneralName Al A Cr Cu Fe, max M,max Si,max Ti,max Zn,max Mn Other Elements, max
    Each Total
    ASTM F467/F467M Grade A92024 2024 Aluminum 2024 balance 0.10max 3.8-4.9 0.50 0.30-0.9 0.50 0.15 B 0.25 1.2-1.8 0.05 0.15
    ASTM F467/F467M Grade A96061 6061 Aluminum 6061 balance 0.04-0.35 0.15-0.40 0.7 0.15 0.40-0.8 0.15 0.25 0.8-1.2 0.05 0.15
    ASTM F467/F467M Grade A96262 6262 Aluminum 6262 balance 0.04-0.14 0.15-0.40 0.7 0.15 0.40-0.8 0.15 0.25 0.8-1.2 C . . .
    • (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 %.

    ASTM F467/F467M Titanium and Titanium-Base Alloys A

    UNS Designation Number Alloy General Name Al C Fe Ti H N O Pd V Cr Mo Zr Sn Si Ru Residuals B
    each, max total, max
    ASTM F467/F467M Grade R50250 1 Titanium Gr 1 . . . 0.10 0.20 balance 0.0125 0.05 0.18 . . . . . . . . . . . . . . . . . . . . . . . . 0.1 0.4
    ASTM F467/F467M Grade R50400 2 Titanium Gr 2 . . . 0.10 0.30 balance 0.0125 0.05 0.25 . . . . . . . . . . . . . . . . . . . . . . . . 0.1 0.4
    ASTM F467/F467M Grade R50700 4 Titanium Gr 4 . . . 0.10 0.50 balance 0.0125 0.07 0.40 . . . . . . . . . . . . . . . . . . . . . . . . 0.1 0.4
    ASTM F467/F467M Grade R56400 5 Titanium Gr 5 5.5- 6.75 0.10 0.40 balance 0.0125 0.05 0.20 . . . 3.5- 4.5 . . . . . . . . . . . . . . . . . . 0.1 0.4
    ASTM F467/F467M Grade R56401 23 Titanium Ti-6Al-4V ELI 5.5- 6.5 0.08 0.25 balance 0.0125 0.05 0.13 . . . 3.5- 4.5 . . . . . . . . . . . . . . . . . . 0.1 0.4
    ASTM F467/F467M Grade R52400 7 Titanium Gr 7 . . . 0.10 0.30 balance 0.0125 0.05 0.25 0.12- 0.25 . . . . . . . . . . . . . . . . . . . . . 0.1 0.4
    ASTM F467/F467M Grade R58640 19 Titanium Ti-38-6-44 3.0- 4.0 0.05 0.30 balance 0.0200 0.03 0.12 0.10 A 7.5- 8.5 5.5- 6.5 3.5- 4.5 3.5- 4.5 . . . . . . 0.10 C 0.15 0.4
    ASTM F467/F467M Grade R55111 32 Titanium Ti-5111 4.5- 5.5 0.08 0.25 balance 0.0125 0.03 0.11 . . . 0.6- 1.4 . . . 0.6- 1.2 0.6- 1.4 0.6- 1.4 0.06- 0.14 . . . 0.1 0.4
    • (A) All reported values are maximums, unless a range is specified.
    • (B) A residual is an element present in a metal or an alloy in small quantities inherent to the manufacturing process but not added intentionally. Residual elements need not be reported unless a report is specifically required by the purchaser.
    • (C) Ruthenium and Palladium, or both, may be added to Grade 19 for enhanced corrosion resistance as negotiated between purchaser and vendor. Chemical analysis is not required unless specifically negotiated.

    ASTM F467/F467M Mechanical Requirements

    ASTM F467/F467M Mechanical Requirements (Inch)

    Alloy Mechanical Property Marking Hardness, min A Proof Stress, Hex Nut min, ksi Proof Stress, Heavy Hex Nut min, ksi B
    ASTM F467 Alloy Cu 110 F 467A 65 HRF 30 32
    ASTM F467 Alloy Cu 260 F467AB 55 HRF 60 65
    ASTM F467 Alloy Cu 270 F 467B 55 HRF 60 65
    ASTM F467 Alloy Cu 462 F 467C 65 HRB 50 54
    ASTM F467 Alloy Cu 464 F 467D 55 HRB 50 54
    ASTM F467 Alloy Cu 510 F 467E 60 HRB 60 65
    ASTM F467 Alloy Cu 613 F 467F 70 HRB 80 86
    ASTM F467 Alloy Cu 614 F 467G 70 HRB 75 81
    ASTM F467 Alloy Cu 630 F 467H 85 HRB 100 108
    ASTM F467 Alloy Cu 642 F 467J 75 HRB 75 81
    ASTM F467 Alloy Cu 651 F 467K 75 HRB 70 76
    ASTM F467 Alloy Cu 655 F 467L 60 HRB 50 54
    ASTM F467 Alloy Cu 661 F467M 75 HRB 70 76
    ASTM F467 Alloy Cu 675 F 467N 60 HRB 55 59
    ASTM F467 Alloy Cu 710 F 467P 50 HRB 45 49
    ASTM F467 Alloy Cu 715 F 467R 60 HRB 55 59
    ASTM F467 Alloy Ni 59 Grade 1 F 467FN 21HRC 120 130
    ASTM F467 Alloy Ni 59 Grade 2 F 467GN 23HRC 135 146
    ASTM F467 Alloy Ni 59 Grade 3 F 467HN 25HRC 160 173
    ASTM F467 Alloy Ni 59 Grade 4 F 467JN 80HRB 100 108
    ASTM F467 Alloy Ni 335 F 467S 20 HRC 115 124
    ASTM F467 Alloy Ni 276 F 467T 20 HRC 110 119
    ASTM F467 Alloy Ni 400 F 467U 75 HRB 80 86
    ASTM F467 Alloy Ni 405 F 467V 60 HRB 70 76
    ASTM F467 Alloy Ni 500 F 467W 24 HRC 130 140
    ASTM F467 Alloy Ni 625 Grade 1 F 467AC 85 HRB-35 HRC 60 65
    ASTM F467 Alloy Ni 625 Grade 2‡ F 467AD 85 HRB-35 HRC 120 130
    ASTM F467 Alloy Ni 686 Grade 1 F 467BN 21 HRC 120 130
    ASTM F467 Alloy Ni 686 Grade 2 F 467CN 23 HRC 135 146
    ASTM F467 Alloy Ni 686 Grade 3 F 467DN 25 HRC 160 173
    ASTM F467 Alloy Ni 686 Grade 4 F 467EN 65 HRB-25HRC 100 108
    ASTM F467 Alloy Al 2024-T4C F 467X 70 HRB 55 59
    ASTM F467 Alloy Al 6061-T6 F 467Y 40 HRB 40 43
    ASTM F467 Alloy Al 6262-T9 F 467Z 60 HRB 52 56
    ASTM F467 Alloy Ti 1 F 467AT 140 HV 40 43
    ASTM F467 Alloy Ti 2 F 467BT 150 HV 55 59
    ASTM F467 Alloy Ti 4 F 467CT 200 HV 85 92
    ASTM F467 Alloy Ti 5 F 467DT 30 HRC 135 146
    ASTM F467 Alloy Ti 7 F 467ET 160 HV 55 59
    ASTM F467 Alloy Ti-19 F 467FT 24 HRC 120 130
    ASTM F467 Alloy Ti 23 F 467GT 25 HRC 125 135
    ASTM F467 Alloy Ti-5111 F 467HT 24 HRC 105 113
    • (A) For aluminum and titanium alloys hardness values are for information only.
    • (B) Proof stress values for heavy hex nuts are based on 1.08 times the value for corresponding regular hex nuts.
    • (C) Aluminum alloy 2024-T4 shall be supplied in naturally aged condition. This material is not recommended for nuts in sizes greater than 1/4 (0.250) in.

    ASTM F467M Mechanical Requirements (Metric)

    Alloy Mechanical Property Marking Hardness, min A Proof Stress, Mpa
    ASTM F467M Cu 110 F467MA 65 HRF 205
    ASTM F467M Cu 260 F467MAB 55 HRF 415
    ASTM F467M Cu 270 F467MB 55 HRF 415
    ASTM F467M Cu 462 F467MC 65 HRB 345
    ASTM F467M Cu 464 F467MD 55 HRB 345
    ASTM F467M Cu 510 F467ME 60 HRB 415
    ASTM F467M Cu 614 F467MG 70 HRB 520
    ASTM F467M Cu 630 F467MH 85 HRB 690
    ASTM F467M Cu 642 F467MJ 75 HRB 520
    ASTM F467M Cu 651 F467MK 75 HRB 485
    ASTM F467M Cu 655 F467ML 60 HRB 345
    ASTM F467M Cu 661 F467MM 75 HRB 485
    ASTM F467M Cu 675 F467MN 60 HRB 380
    ASTM F467M Cu 710 F467MP 50 HRB 310
    ASTM F467M Cu 715 F467MR 60 HRB 380
    ASTM F467M Ni 59 Grade 1 F467FN 21HRC 825
    ASTM F467M Ni 59 Grade 2 F467GN 23HRC 930
    ASTM F467M Ni 59 Grade 3 F467HN 25HRC 1100
    ASTM F467M Ni 59 Grade 4 F467JN 80HRB 690
    ASTM F467M Ni 335 F467MS 20 HRC 790
    ASTM F467M Ni 276 F467MT 20 HRC 760
    ASTM F467M Ni 400 F467MU 75 HRB 550
    ASTM F467M Ni 405 F467MV 60 HRB 485
    ASTM F467M Ni 500 F467MW 24 HRC 900
    ASTM F467M Ni 625 F 467AC 85 HRB-35 HRC 415
    ASTM F467M Ni 686 Grade 1 F 467MBN 21 HRC 825
    ASTM F467M Ni 686 Grade 2 F 467MCN 23 HRC 930
    ASTM F467M Ni 686 Grade 3 F 467MDN 25 HRC 1100
    ASTM F467M Ni 686 Grade 4 F 467MEN 65 HRB-25 HRC 690
    ASTM F467M Al 2024-T4B F467MX 70 HRB 380
    ASTM F467M Al 6061-T6 F467MY 40 HRB 275
    ASTM F467M Al 6262-T9 F467MZ 60 HRB 360
    ASTM F467M Ti 1 F467MAT 140 HV 275
    ASTM F467M Ti 2 F467MBT 150 HV 380
    ASTM F467M Ti 4 F467MCT 200 HV 585
    ASTM F467M Ti 5 F467MDT 30 HRC 930
    ASTM F467M Ti 7 F467MET 160 HV 380
    ASTM F467M Ti 19 F467MFT 24 HRC 825
    ASTM F467M Ti 23 F467MGT 25 HRC 860
    ASTM F467M Ti-5111 F467MHT 24 HRC 725
    • (A) For aluminum and titanium alloys hardness values are for information only.
    • (B) Aluminum alloy 2024-T4 shall be supplied in naturally aged condition. This material is not recommended for nuts in nominal thread diameter larger than M6.

    ASTM F467/F467M Tensile Stress Areas and Threads per Inch

    Nominal Size, in. Coarse Threads-UNC Fine Threads-UNF 8 Thread Series-8UN
    Threads/in. Stress Area A, in 2 Threads/in. Stress Area A, in 2 Threads/in. Stress Area A, in 2
    1/ 4 20 0.0318 28 0.0364 . . . . . .
    5/ 16 18 0.0524 24 0.0580 . . . . . .
    3/ 8 16 0.0775 24 0.0878 . . . . . .
    7/ 16 14 0.1063 20 0.1187 . . . . . .
    1/ 2 13 0.1419 20 0.1599 . . . . . .
    9/ 16 12 0.1820 18 0.2030 . . . . . .
    5/ 8 11 0.2260 18 0.2560 . . . . . .
    3/ 4 10 0.3340 16 0.3730 . . . . . .
    7/ 8 9 0.4620 14 0.5090 . . . . . .
    1 8 0.6060 12 0.6630 . . . . . .
    1 1/ 8 7 0.7630 12 0.8560 8 0.790
    1 1/ 4 7 0.9690 12 1.0730 8 1.000
    1 3/ 8 6 1.1550 12 1.3150 8 1.233
    1 1/ 2 6 1.4050 12 1.5810 8 1.492
    • (A) Tensile stress areas are computed using the following formula:
    • A s = 0.7854 [ D - 0.9743/n ]
      • where:
      • As = tensile stress area, in. 2 ,
      • D = nominal size (basic major diameter), in., and
      • n = number of threads per inch.

    ASTM F467/F467M Tensile Stress Areas and Threads per Metric

    Nominal Nut Diameter and Thread Pitch Stress Area, Amm 2 Nominal Nut Diameter and Thread Pitch Stress Area, Amm 2
    M6 × 1 20.1 M16 × 2 157
    M8 × 1.25 36.6 M20 × 2.5 245
    M10 × 1.5 58.0 M24 × 3 353
    M12 × 1.75 84.3 M30 × 3.5 561
    M14 × 2 115 M36 × 4 817
    • (A) Tensile stress areas are computed using the following formula:
    • As = 0.7854 (D − 0.9382P) 2
      • where:
      • As = tensile stress area, mm. 2 ,
      • D = nominal size (basic major diameter), mm., and
      • n = number of threads per mm.

    ASTM F467 Condition (Heat Treatment)

    Except as provided in 4.2.3, nuts are furnished in the condition below (4.2.2). When required, stress relieving is specified by the purchaser for all copper alloys and nickel alloys 400 and 405 (4.2.3). Unless otherwise specified, nuts may be hot pressed, cold formed or machined at the manufacturer's option (4.2.1).

    Alloy Condition
    Copper (all alloys) As formed or stress relieved at manufacturer's option
    Nickel alloys 400 and 405 As formed or stress relieved at manufacturer's option
    Nickel alloy 500 Solution annealed and aged
    Aluminum alloy 2024-T4 Solution treated and naturally aged
    Aluminum alloy 6061-T6 Solution treated and artificially aged
    Aluminum alloy 6262-T9 Solution treated, artificially aged, and cold worked
    Titanium 625 Annealed

    ASTM F467/F467M Supplementary Requirements

    S1 – Stress Corrosion Requirements, Copper Alloys

    When S1 is specified, copper alloy fasteners must show no evidence of cracking after immersion for 30 min in an aqueous solution of mercurous nitrate, tested per ASTM B154. Mercury is a health hazard: mercury vapor detection and removal equipment and rubber gloves are recommended during the test.

    S2 – Shipment Lot Testing

    When S2 is specified on the order (3.1.6), the manufacturer tests the individual lots for shipment: a chemical analysis of a randomly selected finished nut from each lot (or the starting material analysis, with heat or lot control maintained), and mechanical property tests per this specification and ASTM F1470. A test report with the actual chemical and mechanical results is furnished for each lot (16.2).

    S3 – Dye Penetrant Inspection

    When dye penetrant inspection is specified on the purchase order, nuts are tested per ASTM E165 or another mutually acceptable procedure, and conform to acceptance criteria agreed between purchaser and manufacturer.

    S4 – Heat Control (Alloys 400, 405, and 500 Only)

    Applies to alloys 400, 405 and 500 only. When S4 is specified, the manufacturer controls the product by heat analysis and identifies the finished product in each shipment by the actual heat number. S2 is then invoked automatically, and the heat analysis is reported on the test reports.

    ASTM F467 Testing, Sampling and Marking

    Nuts are tested in full section (12.2.1) and hardness is taken on the top or bottom face (12.2.2) to ASTM E18 or E92: one reading for 1/4 to 7/16 in., the average of four readings 90 degrees apart for 1/2 in. and larger (13.2.2). Where both proof load and hardness are tested, proof load governs acceptance (6.2).

    A lot is up to 100 000 nuts of one type, alloy and temper, diameter and thread series (9.1). Sample size by lot: 50 and under, 2; 51 to 500, 3; 501 to 35 000, 5; 35 001 to 100 000, 8; acceptance number 0, rejection number 1 (10.1).

    Proof load is the Table 2 proof stress times the Table 4 tensile stress area (13.2.1). For example, a 1/2-13 UNC hex nut (stress area 0.1419 sq in) in naval brass 462 (50 ksi) must carry 7,095 lbf.

    Every nut is marked with the manufacturer's symbol and the alloy/mechanical property marking from Table 2, raised or depressed (17.1), for example F 467C for naval brass 462 or F 467U for Ni-Cu alloy 400. Each shipping unit is marked with the ASTM designation, alloy number, property marking, size, manufacturer, number of pieces, country of origin and purchase order number (17.3).

    When specified, the manufacturer furnishes a certificate of compliance (16.1); when S2 shipment lot testing is specified, a test report with the mechanical test results for each lot (16.2). Packaging is to ASTM D3951 unless otherwise specified (17.2.1).

    Frequently Asked Questions

    What is ASTM F467?

    ASTM F467 is the Standard Specification for Nonferrous Nuts for General Use. ASTM F467-13ε2 covers commercial wrought nonferrous nuts 0.250 to 1.500 in. inclusive in diameter (1.1), in inch-pound units; F467M is the metric companion (Note 1). It is under ASTM Committee F16 on Fasteners.

    Which alloys does ASTM F467 cover?

    ASTM F467-13ε2 Table 1 lists 35 wrought alloys: 16 copper-base (C11000, C26000, C27000, C46200, C46400, C51000, C61300, C61400, C63000, C64200, C65100, C65500, C66100, C67500, C71000, C71500), 8 nickel-base (N10001, N10276, N04400, N04405, N05500, N06059, N06625, N06686), 3 aluminum-base (A92024, A96061, A96262) and 8 titanium (R50250, R50400, R50700, R56400, R56401, R52400, R58640, R55111). Table 2 gives hardness, proof stress and marking for each; alloys 59 and 686 have four strength grades and alloy 625 has two.

    What is the difference between ASTM F467 and F468?

    F467 covers nonferrous nuts. ASTM F468 covers the applicable nonferrous bolts, hex cap screws, socket head cap screws and studs for use with them (1.2).

    Which dimensions and threads apply to F467 nuts?

    Unless otherwise specified, nut dimensions are to ASME B18.2.2 (7.1) and threads are Class 2B to ASME B1.1 (7.2). Nuts are supplied without any additive chemical or metallic finish unless otherwise specified (8.2).

    How is F467 nut strength checked?

    By proof load and hardness. Table 2 sets a minimum hardness and a minimum proof stress for hex and heavy hex nuts for each alloy; heavy hex values are 1.08 times the hex value. Proof load (proof stress times the Table 4 stress area) is tested per ASTM F606 and governs acceptance when both tests are made (6.2, 13.2.1).

    What are the F467 supplementary requirements?

    S1 stress corrosion test for copper alloys (mercurous nitrate, ASTM B154), S2 shipment lot testing with a test report, S3 dye penetrant inspection (ASTM E165), and S4 heat control for alloys 400, 405 and 500. They apply only when the purchaser specifies them.