Sa 479
Sa 479
Sa 479
SA-479 /SA-479M
867
--`,,```,,,,````-`-`,,`,,`,`,,`---
3.1.11 Surface preparation of shapes (see Manufac- requirements. Consideration should be given to the corrosive media
ture section of Specification A 484/A 484M), before using a stabilization anneal at less than 1800°F [980°C], as such
a treatment may not be fully effective for all media.
3.1.12 The intended use of the material, if the pur-
chaser considers this useful information. NOTE 4 — Grain size requirements for the H grades are described in
Section 7.
NOTE 2 — A typical ordering description is as follows: 5000 lb [2000
kg]; 1.000 in. [25 mm] round bar by 10 to 12 ft [3 to 4 m]; Type 304 4.1.3 Strain Hardened Austenitic Type 316 — When
or UNS S30400; to Specification A 479 [A 479M]; annealed; centerless Type 316 is desired with increased mechanical properties,
--`,,```,,,,````-`-`,,`,,`,`,,`---
ground; plus any optional supplementary requirements; such as, for the strain hardened condition may be specified and is
example, special marking instructions. produced by solution annealing, as described in 4.1.1,
followed by strain hardening sufficient to meet the
required mechanical properties. Solution annealed and
4. Heat Treatment strain hardened material shall be capable of meeting the
4.1 Austenitic Grades: intergranular corrosion test of Supplementary Require-
4.1.1 Except for the strain-hardened grade (see ment S2.
4.1.3), and the hot-rolled grade (see 4.1.4), all austenitic 4.1.3.1 Two strain hardened conditions have
grades of stainless steel shall be furnished in the solution been established for different applications: Level 1 and
annealed condition, with subsequent light cold drawing Level 2 (see the Mechanical Property Requirements
and straightening permitted (see Supplementary Require- table).
ment S5 if annealing must be the final operation). Solution
annealing for all grades, except the H grades (see 4.1.2), 4.1.4 High tensile Type XM-19 shall be in the hot-
N08367 (see 4.1.8), S31254 (see 4.1.5), S32050 (see rolled or strain-hardened condition and shall be capable
4.1.5), S33228 (see 4.1.7), S34565 (see 4.1.6), and of meeting the mechanical property requirements of the
S35315 (see 4.1.9), shall consist of (1) heating the mate- Mechanical Property Requirements table and passing the
rial to a temperature of 1900°F [1040°C] minimum so that intergranular corrosion test prescribed in S2. The strain
grain boundary carbides enter into solution, and cooling hardened condition is achieved by solution annealing fol-
rapidly to prevent grain boundary carbide precipitation; or lowed by cold working sufficient to develop the required
alternatively (2) (except for the columbium and titanium mechanical properties.
stabilized grades 309Cb, 310Cb, 316Cb, 316Ti, 321, 347, 4.1.5 Solution annealing of S31254 and S32050
and 348) immediately following hot working while the shall consist of heating the material to a temperature
temperature is above 1750°F [955°C] so that grain bound- of 2100°F [1150°C] minimum, for an appropriate time
ary carbides are in solution, cooling rapidly to prevent followed by water quenching or rapidly cooling by other
grain boundary carbide precipitation. When Supplemen- means.
tary Requirement S2 is invoked, all austenitic grades
except S30815 shall pass the intergranular corrosion test 4.1.6 Solution annealing of S34565 shall consist
requirements described in S2. of heating the material in the range of temperature from
2050°F [1120°C] to 2140°F [1170°C] for an appropriate
4.1.2 For H grades, the minimum solution anneal-
time, followed by water quenching or rapidly cooling by
ing temperatures shall be as follows:
other means.
4.1.2.1 When hot finished, 1900°F [1040°C] for
Types 304H, 309H, 310H, and 316H; 1925°F [1050°C] 4.1.7 Solution annealing of S33228 shall consist
for Types 321H, 347H, and 348H. of heating the material in the temperature range 2050 to
2160°F [1120 to 1180°C] for an appropriate time fol-
4.1.2.2 When cold worked prior to solution lowed by water quenching or rapid cooling by other
annealing, 1900°F [1040°C] for Types 304H, 309H, means.
310H, and 316H; 2000°F [1095°C] for Types 321H,
347H, and 348H. 4.1.8 Solution annealing of N08367 shall consist of
heating the material to a temperature of 2025°F [1105°C]
NOTE 3 — Solution annealing temperatures above 1950°F [1065°C]
minimum for an appropriate time followed by water
may impair the resistance to intergranular corrosion after subsequent
exposure to sensitizing conditions in the stabilized grades, Types 321, quenching or rapidly cooling by other means.
321 H, 347, 347 H, 348 and 348 H. When intergranular corrosion is 4.1.9 Solution annealing of S35315 shall consist of
of concern, the purchaser should specify the corrosion test of S2 (to
be conducted on sensitized specimens). The manufacturer may, if neces-
heating the material to a temperature of 2100°F [1150°C]
sary, use a lower temperature resolution anneal or a stabilization anneal minimum for an appropriate time followed by water
after a high temperature solution anneal in order to meet corrosion test quenching or rapidly cooling by other means.
868
869
7.2 The H grades shall conform to an average grain the purchase order shall be furnished at the time of ship-
size as follows: ment. The certification shall be positively relatable to the
7.2.1 ASTM No. 6 or coarser for Types 304H, lot of material represented.
309H, 310H, and 316H,
7.2.2 ASTM No. 7 or coarser for Types 321H, 11. Product Marking
347H, and 348H.
11.1 In addition to the marking requirements of Speci-
7.3 For S32615, the grain size as determined in accor- fication A 484/A 484M, materials which have been heat
dance with Test Methods E 112, comparison method, treated in accordance with 4.1, 4.2, 4.3, 4.4 or have been
Plate 11, shall be No. 3 or finer. strain hardened in accordance with 4.1.3 shall be identi-
fied by placement of the following symbols after the
7.4 Supplementary Requirement S1 shall be invoked
grade designation:
when non–H grade austenitic stainless steels are ordered
for ASME Code applications for service above 1000°F 11.1.1 Austenitic Grades:
(540°C). 11.1.1.1 All grades in the annealed condi-
tion — A,
11.1.1.2 Strain hardened Type 316, Level 1 —
8. Mechanical Properties Requirements
S1,
8.1 The material shall conform to the mechanical
property requirements specified in Table 2 for the grade 11.1.1.3 Strain hardened Type 316, Level 2 —
ordered. At least one room-temperature test shall be per- S2,
formed by the manufacturer on a sample from at least 11.1.1.4 Hot-rolled Type XM-19 — H,
one bar or shape from each lot of material. 11.1.1.5 Strain hardened Type XM-19 — S,
8.2 The yield strength shall be determined by the 11.1.1.6 Material meeting Supplementary
offset (0.2%) method as prescribed in Test Methods and Requirement S1 — ELT (unnecessary for H grades).
Definitions A 370.
11.1.1.7 In addition to all other marking require-
8.3 Martensitic material supplied in the annealed con- ments of this specification, when S1 is invoked, all grades
dition shall be capable of meeting the hardened and tem- in the direct quenched condition (heat treated in accor-
pered mechanical properties when heat treated in dance with 4.1.1(2)) shall be marked — D.
accordance with the requirements of 4.4. 11.1.2 Austenitic-Ferritic Grades — All grades in
8.4 Hardness measurements, when required, shall be the annealed condition — A.
made at a location midway between the surface and the 11.1.3 Ferritic Grades — All grades in the annealed
center of the cross section. condition — A.
8.5 Martensitic grades shall be capable of meeting 11.1.4 Martensitic Grades:
the hardness requirements after heat treating as specified 11.1.4.1 All grades in the annealed condi-
in Table 3. tion — A.
11.1.4.2 Types 403 and 410 — COND 1, COND
9. Corrosion Testing 2, or COND 3 as appropriate for the tempering tempera-
ture employed.
9.1 Austenitic stainless steels solution annealed by
the alternative method (see (2) in 4.1.1) shall be tested 11.1.4.3 Type 414, S41500, and Type XM-30
and pass the intergranular corrosion test requirements tempered materials — T.
described in S2.
12. Keywords
10. Certification 12.1 austenitic stainless steel; austenitic-ferritic
10.1 The material manufacturer’s certificate of com- duplex stainless steel; ferritic stainless steel; martensitic
pliance certifying that the material was manufactured and stainless steel; pressure containing parts; pressure vessel
tested in accordance with this specification, together with service; stainless steel bars; stainless steel shapes; temper-
a report of the results required by this specification and ature service applications — high
870
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TABLE 1
CHEMICAL REQUIREMENTS
Composition, %B
UNS Molyb- Other
DesignationA Type Carbon Manganese Phosphorus Sulfur Silicon Chromium Nickel Nitrogen denum ElementsC
Austenitic Grades
N08367 ... 0.030 2.00 0.040 0.030 1.00 20.00– 23.50– 0.18–0.25 6.00–7.00 Cu 0.75 max
22.00 25.50
S20161 ... 0.15 4.0–6.0 0.045 0.030 3.0–4.0 15.0– 18.0 4.0–6.0 0.08–0.20 ... ...
S20910 XM-19 0.06 4.0–6.0 0.045 0.030 1.00 20.5–23.5 11.5–13.5 0.20–0.40 1.50–3.00 Cb 0.10–0.30;
V 0.10–0.30
S21600 XM-17 0.08 7.5–9.0 0.045 0.030 1.00 17.5–20.5 5.0–7.0 0.25–0.50 2.00–3.00 ...
S21603 XM-18 0.03 7.5–9.0 0.045 0.030 1.00 17.5–20.5 5.0–7.0 0.25–0.50 2.00–3.00 ...
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 ... ...
S21904 XM-11 0.04 8.0–10.0 0.045 0.030 1.00 19.0–21.5 5.5–7.5 0.15–0.40 ... ...
S24000 XM-29 0.08 11.5–14.5 0.060 0.030 1.00 17.0–19.0 2.3–3.7 0.20–0.40 ... ...
S34565 ... 0.030 5.0–7.0 0.030 0.010 1.00 23.0–25.0 16.0–18.0 0.40–0.60 4.0–5.0 Cb 0.10 max
S30200 302 0.15 2.00 0.045 0.030 1.00 17.0–19.0 8.0–10.0 0.10 ... ...
S30400 304 0.08C 2.00 0.045 0.030 1.00 18.0–20.0 8.0–10.5 0.10 ... ...
S30403 304L 0.030 2.00 0.045 0.030 1.00 18.0–20.0 8.0–12.0 0.10 ... ...
S30409 304H 0.04–0.10 2.00 0.045 0.030 1.00 18.0–20.0 8.0–10.5 ... ... ...
S30451 304N 0.08 2.00 0.045 0.030 1.00 18.0–20.0 8.0–12.0 0.10–0.16 ... ...
S30453 304LN 0.030 2.00 0.045 0.030 1.00 18.0–20.0 8.0–12.0 0.10–0.16 ... ...
S30600 ... 0.018 2.00 0.020 0.020 3.7–4.3 17.0–18.5 14.0–15.5 ... 0.20 Cu 0.50 max
S30815 ... 0.05–0.10 0.80 0.040 0.030 1.40–2.00 20.0–22.0 10.0–12.0 0.14–0.20 ... Ce 0.03–0.08
S30908 309S 0.08 2.00 0.045 0.030 1.00 22.0–24.0 12.0–15.0 ... ... ...
S30909 309H 0.04–0.10 2.00 0.045 0.030 1.00 22.0–24.0 12.0–15.0 ... ... ...
S30940 309Cb 0.08 2.00 0.045 0.030 1.00 22.0–24.0 12.0–16.0 0.10 ... Cb 10ⴛC−1.10
S30880 ER308D 0.08 1.00–2.50 0.030 0.030 0.25–0.60 19.5–22.0 9.0–11.0 ... ... ...
S31008 310S 0.08 2.00 0.045 0.030 1.00 24.0–26.0 19.0–22.0 ... ... ...
S31009 310H 0.04–0.10 2.00 0.045 0.030 1.00 24.0–26.0 19.0–22.0 ... ... ...
S31040 310Cb 0.08 2.00 0.045 0.030 1.50 24.0–26.0 19.0–22.0 0.10 ... Cb 10ⴛC−1.10
S31254 ... 0.020 1.00 0.030 0.010 0.80 19.5–20.5 17.5–18.5 0.18–0.22 6.0–6.5 Cu 0.50–1.00
S31600 316 0.08C 2.00 0.045 0.030 1.00 16.0–18.0 10.0–14.0 0.10 2.00–3.00 ...
S31603 316L 0.030 2.00 0.045 0.030 1.00 16.0–18.0 10.0–14.0 0.10 2.00–3.00 ...
S31609 316H 0.04–0.10 2.00 0.040 0.030 1.00 16.0–18.0 10.0–14.0 ... 2.00–3.00 ...
S31635 316Ti 0.08 2.00 0.045 0.030 1.00 16.0–18.0 10.0–14.0 0.10 2.00–3.00 Ti5ⴛ(C+N)−0.70
S31640 316Cb 0.08 2.00 0.045 0.030 1.00 16.0–18.0 10.0–14.0 0.10 2.00–3.00 Cb 10ⴛC−1.10
S31651 316N 0.08 2.00 0.045 0.030 1.00 16.0–18.0 10.0–14.0 0.10–0.16 2.00–3.00 ...
S31653 316LN 0.030 2.00 0.045 0.030 1.00 16.0–18.0 10.0–14.0 0.10–0.16 2.00–3.00 ...
S31700 317 0.08 2.00 0.045 0.030 1.00 18.0–20.0 11.0–15.0 0.10 3.0–4.0 ...
S31725 ... 0.030 2.00 0.045 0.030 1.00 18.0–20.0 13.50– 0.10 4.0–5.0 Cu 0.75 max
17.50
S31726 ... 0.030 2.00 0.045 0.030 1.00 17.0–20.0 13.50– 0.10–0.20 4.0–5.0 Cu 0.75 max
17.50
S32050 ... 0.030 1.50 0.035 0.020 1.00 22.0–24.0 20.0–22.0 0.24–0.34 6.0–6.8 Cu 0.4 max
S32100 321 0.08E 2.00 0.045 0.030 1.00 17.0–19.0 9.0–12.0 ... ... Ti 5ⴛ(C+N)−0.70F
S32109 321H 0.04–0.10 2.00 0.040 0.030 1.00 17.0–19.0 9.0–12.0 ... ... Ti
4ⴛ(C+N)−0.70F
S32615 ... 0.07 2.00 0.045 0.030 4.8–6.0 16.5–19.5 19.0–22.0 ... 0.30–1.50 Cu 1.50–2.50
S33228 ... 0.04–0.08 1.00 0.020 0.015 0.30 26.0–28.0 31.0–33.0 ... ... Cb 0.60–1.00
Ce 0.05–0.10
Al 0.025 max
S34700 347 0.08E 2.00 0.045 0.030 1.00 17.0–19.0 9.0–13.0 ... ... Cb 10ⴛC min
S34709 347H 0.04–0.10 2.00 0.045 0.030 1.00 17.0–19.0 9.0–13.0 ... ... Cb 8ⴛC−1.00
S34800 348 0.08E 2.00 0.045 0.030 1.00 17.0–19.0 9.0–13.0 ... ... (Cb+Ta) 10ⴛC
min;
Ta 0.10 max;
Co 0.20 max
S34809 348H 0.04–0.10 2.00 0.040 0.030 1.00 17.0–19.0 9.0–13.0 ... ... (Cb+Ta)
8ⴛC−1.00;
Co 0.20 max;
Ta 0.10 max
S35315 ... 0.04–0.08 2.00 0.040 0.030 1.20–2.00 24.0–26.0 34.0–36.0 0.12–0.18 ... Ce 0.03–0.08
871
TABLE 1
CHEMICAL REQUIREMENTS (CONT’D)
Composition, %B
UNS
Desig- Molyb-
nationA Type Carbon Manganese Phosphorus Sulfur Silicon Chromium Nickel Nitrogen denum Other ElementsC
Austenitic-Ferritic Grades
S31803 ... 0.030 2.00 0.030 0.020 1.00 21.0–23.0 4.5–6.5 0.08–0.20 2.5–3.5 ...
S32205 ... 0.030 2.00 0.030 0.020 1.00 22.0–23.0 4.5–6.5 0.14–0.20 3.0–3.5 ...
S32550 ... 0.04 1.50 0.040 0.030 1.00 24.0–27.0 4.5–6.5 0.10–0.25 2.9–3.9 Cu 1.50–2.50
S32750 ... 0.030 1.20 0.035 0.020 0.80 24.0–26.0 6.0–8.0 0.24–0.32 3.0–5.0 Cu 0.5 max
S32760G ... 0.030 1.00 0.030 0.010 1.00 24.0–26.0 6.0–8.0 0.20–0.30 3.0–4.0 Cu 0.50–1.00;
W 0.50–1.00
S32906 min ... 0.80 ... ... ... 28.0 5.8 0.30 1.50 ...
max 0.030 1.50 0.030 0.030 0.50 30.0 7.5 0.40 2.60 Cu 0.80
S32950 ... 0.03 2.00 0.035 0.010 0.60 26.0–29.0 3.5–5.2 0.15–0.35 1.00–2.50 ...
S39277 ... 0.025 0.80 0.025 0.002 0.80 24.0–26.0 6.5–8.0 0.23–0.33 3.0–4.0 Cu 1.2–2.0;
W 0.8–1.2
Ferritic Grades
S40500 405 0.08 1.00 0.040 0.030 1.00 11.5–14.5 0.60 max ... ... Al 0.10–0.30
S43000 430 0.12 1.00 0.040 0.030 1.00 16.0–18.0 ... ... ... ...
S43035 439 0.07 1.00 0.040 0.030 1.00 17.0–19.0 0.50 max 0.04 ... Ti 0.20 + 4ⴛ
(C+N) min
S44400 444 0.025 1.00 0.040 0.030 1.00 17.5–19.5 1.00 max 0.035 1.75–2.50 (Ti+Cb) 0.20+4ⴛ
(C+N)−0.80
H
S44627 XM-27 0.010 0.40 0.02 0.02 0.40 25.0–27.5 0.50 max 0.015 maxH 0.75–1.50 Cu 0.20 max; Cb
0.05–0.20
S44700 ... 0.010 0.30 0.025 0.020 0.20 28.0–30.0 0.15 max 0.020 3.5–4.2 (C+N) 0.025 max;
Cu 0.15 max
S44800 ... 0.010 0.30 0.025 0.020 0.20 28.0–30.0 2.00–2.50 0.020 3.5–4.2 (C+N) 0.025 max;
Cu 0.15 max
Martensitic Grades
S40300 403 0.15 1.00 0.040 0.030 0.50 11.5–13.0 ... ... ... ...
S41000 410 0.15 1.00 0.040 0.030 1.00 11.5–13.5 ... ... ... ...
S41040 XM-30 0.18 1.00 0.040 0.030 1.00 11.5–13.5 ... ... ... Cb 0.05–0.30
S41400 414 0.15 1.00 0.040 0.030 1.00 11.5–13.5 1.25–2.50 ... ... ...
S41425 ... 0.05 0.50–1.00 0.020 0.005 0.50 12.0–15.0 4.0–7.0 0.06–0.12 1.50–2.00 Cu 0.30 max
I
S41500 0.05 0.50–1.00 0.030 0.030 0.60 11.5–14.0 3.5–5.5 ... 0.50–1.00 ...
S43100 431 0.20 1.00 0.040 0.030 1.00 15.0–17.0 1.25–2.50 ... ... ...
A
New designations established in accordance with Practice E 527 and SAE J1086 published jointly by ASTM and SAE. See ASTM DS-
56C, available from ASTM Headquarters.
B
Maximum unless otherwise indicated.
C
Except as required for specific alloy type, molybdenum, titanium, nickel, cobalt, tantalum, nitrogen, and copper need not be reported but
shall not be present in other than residual amounts; the intent being to prohibit substitution of one alloy type for another due to absence
of control of the above named elements in certain alloys.
D
American Welding Society designation.
E
See Supplementary Requirement S1.
F
Nitrogen content is to be reported for this grade.
G
%Cr + 3.3 ⴛ %Mo + 16 ⴛ %N ≥ 40.
H
Product analysis tolerance over the maximum limit for carbon and nitrogen to be 0.002%.
I
Wrought version of CA6NM.
872
TABLE 2
MECHANICAL PROPERTY REQUIREMENTS
Tensile Yield Elongation
Strength, Strength,A in 2 in. Reduction Brinell
min, min, ksi [50 mm] or of Area, Hardness,
UNS Designation Type Condition ksi [MPa] [MPa] 4D, min, % min, %B max
Austenitic Grades
N08367 ... annealed 95 [655] 45 [310] 30 ... 241
S20161 ... annealed 125 [860] 50 [345] 40 40 311
S20910 XM-19 annealed 100 [690] 55 [380] 35 55 293
Up to 2 in. (50.8 mm), hot-rolled 135 [930] 105 [725] 20 50 ...
incl
Over 2 to 3 in. (50.8 to hot-rolled 115 [795] 75 [515] 25 50 ...
76.2 mm), incl
Over 3 to 8 in. (76.2 to hot-rolled 100 [690] 60 [415] 30 50 ...
203.2 mm), incl
Up to 11⁄2 in. (38.1 mm), strain- 145 [1000] 125 [860] 12 40 ...
incl hardened
Over 11⁄2 to 21⁄4 in. (38.1 strain- 120 [825] 105 [725] 15 45 ...
to 57.2 mm), incl hardened
S21600, S21603 XM-17, XM-18 annealed 90 [620] 50 [345] 40 50 212
S21800 ... annealed 95 [655] 50 [345] 35 55 241
S21904 XM-11 annealed 90 [620] 50 [345] 45 60 ...
S24000 XM-29 annealed 100 [690] 55 [380] 30 50 ...
S30200, S30400, 302, 304, 304H, 304LN, annealed 75 [515]D 30 [205] 30 40 ...
S30409, S30453, ER308,C 309S, 309H,
S30880, S30908, 309Cb, 310S, 310H,
S30909, S30940, 310Cb, 316, 316H, 316Ti,
S31008, S31009, 316Cb, 316LN, 317, 321,
S31040, S31600, 321H, 347, 347H, 348,
S31609, S31635, 348H
S31640, S31653,
S31700, S32100,
S32109, S34700,
S34709, S34800,
S34809
316 strain- 85 [585] 65 [450]E 30 60 ...
hardened
level 1
2 in. and under strain- 95 [655] 75 [515] 25 40 ...
hardened
level 2
Over 2 to 21⁄2 in. (50.8 to strain- 90 [620] 65 [450] 30 40 ...
63.5 mm), incl hardened
level 2
Over 21⁄2 to 3 in. (63.5 to strain- 80 [550] 55 [380] 30 40 ...
76.2 mm), incl hardened
level 2
S30403, S31603 304L, 316L annealed 70 [485] 25 [170] 30 40 ...
S30451, S31651 304N, 316N annealed 80 [550] 35 [240] 30 40 ...
S30600 ... annealed 78 [540] 35 [240] 40 ... ...
S30815 ... annealed 87 [600] 45 [310] 40 50 ...
S31254 ... annealed 95 [655] 44 [305] 35 50 ...
S31725 ... annealed 75 [515] 30 [205] 40 ... ...
S31726 ... annealed 80 [550] 35 [240] 40 ... ...
S32050 ... annealed 98 [675] 48 [330] 40 ... ...
S32615 ... annealed 80 [550] 32 [220] 25 40 ...
S33228 ... annealed 73 [500] 27 [185] 30 ... ...
S34565 ... annealed 115 [795] 60 [415] 35 40 230
S35315 ... annealed 94 [650] 39 [270] 40 ... ...
873
--`,,```,,,,````-`-`,,`,,`,`,,`---
TABLE 2
MECHANICAL PROPERTY REQUIREMENTS (CONT’D)
Tensile Yield Elongation
Strength, Strength,A in 2 in. Reduction Brinell
min, min, ksi [50 mm] or of Area, Hardness,
UNS Designation Type Condition ksi [MPa] [MPa] 4D, min, % min, %B max
Austenitic-Ferritic Grades
S31803 ... annealed 90 [620] 65 [450] 25 ... 290
S32205 ... annealed 90 [620] 65 [450] 25 ... 290
S32550 ... annealed 110 [760] 80 [550] 15 ... 297
S32750 2 in. and under annealed 116 [800]F 80 [550]F 15 ... 310
over 2 in. annealed 110 [760] 75 [515] 15 ... 310
S32760 ... annealed 109 [750] 80 [550] 25 ... 300
S32906 ... annealed 109 [750] 80 [550] 25 ... 310
S32950 ... annealed 100 [690] 70 [485] 15 ... 297
S39277 ... annealed 118 [820] 85 [585] 25 50 293
Ferritic Grades
S40500 405 annealed 60 [415] 25 [170] 20 45 207
S43000, S43035 430, 439 annealed 70 [485] 40 [275] 20G 45G 192
S44627 XM-27 annealed 65 [450] 40 [275] ... 45G 217
S44401 ... annealed 60 [415] 45 [310] 20H 45H 217
S44700 ... annealed 70 [485] 55 [380] 20 40 ...
S44800 ... annealed 70 [485] 55 [380] 20 40 ...
Martensitic Grades
S40300, S41000 403, 410 annealed 70 [485] 40 [275] 20D 45D 223
1 70 [485] 40 [275] 20D 45D 223
2 110 [760] 85 [585] 15 45 269
3 130 [895] 100 [690] 12 35 331
S41400 414 tempered 115 [795] 90 [620] 15 45 321
S41425 ... tempered 120 [825] 95 [655] 15 45 321
S41500 ... normalized 115 [795] 90 [620] 15 45 293
and
tempered
S43100 431I annealed ... ... ... ... 277
tempered 115 [795] 90 [620] 15 45 321
S41040 XM-30 annealed 70 [485] 40 [275] 13G 45G 235
quenched and 125 [860] 100 [690] 13 45 302
tempered
A
See Section 7.
B
Reduction of area does not apply on flat bars 3⁄16 in. [4.80 mm] and under in thickness as this determination is not generally made in this
product size.
C
American Welding Society designation.
D
Tensile strength 70 ksi [485 MPa] min permitted for extruded shapes.
E
For bars greater than 2 in. [51 mm], a cross section, 60 ksi [415 MPa] min, shall be permitted.
F
For sections over 2 in. [50 mm] in thickness, the minimum tensile strength shall be 106 ksi [730 MPa]; the minimum yield strength shall
be 75 ksi [515 MPa].
G
Elongation in 2 in. or 50 mm of 12% min and reduction of area of 35% min permitted for cold-finished bars.
H
Elongation in 2 in. of 12% min and reduction of area of 35% min permitted for cold-drawn or cold-rolled bars.
I
Annealed bars shall be capable of meeting the tempered condition requirements when heat treated in accordance with 4.4.3.
874
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TABLE 3
RESPONSE TO HEAT TREATMENT
Heat Treatment
TemperatureB Hardness
TypeA °F (°C), min Quenchant HRC, min
875
SUPPLEMENTARY REQUIREMENTS
The following may be made requirements when the purchaser specifies them to be appli-
cable.
876
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APPENDIX
(Nonmandatory Information)
X1. RATIONALE REGARDING DEFINITION X1.2 For Boiler Code applications involving tempera-
OF SOLUTION ANNEALING IN 4.1.1 tures where optimum resistance to creep is desired, the
larger grain size of material solution annealed by reheat-
X1.1 It is generally recognized that austenitic stainless
ing is generally desired. For that reason a minimum grain
steels are solution annealed by heating to a temperature
size has been required of the H grades (created for opti-
that dissolves (takes into solution) chromium carbides
mum elevated temperature properties) and a mandatory
and quenching rapidly so that the chromium carbides will
grain size test and report has been added for the non-H
not participate in the grain boundaries which could cause
grades so that the information is available for those desir-
susceptibility to intergranular corrosion in a critically
ing to reclassify a non-H grade to H grade.
corrosive environment. Thus, solution annealing also can
be accomplished for non-stabilized grades by taking X1.3 To satisfy the concerns of inadvertent assign-
advantage of hot rolling temperatures (which always ment of fine grained material to elevated temperature
exceed solution annealing temperature requirements), applications, special marking has been added for material
maintaining hot rolling finishing temperatures well above which meets the requirements of Supplementary Require-
minimum solution annealing requirements, and immedi- ment S1.
ately quenching integral with hot rolling. Stabilized X1.4 A mandatory test for susceptibility to intergranu-
grades (with columbium or titanium added) cannot be lar corrosion has been added for material solution
handled this way since they would become destabilized annealed by the alternative method [see (2) in 4.1.1] so
due to columbium or titanium carbide solution, without that a history of data can be accumulated, as has been done
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877