This specification covers forged low alloy and stainless steel piping components for use in pressure systems. Included are flanges, fittings, valves, and similar parts to specified dimensions or to dimensional standards.
TABLE 1 Heat Treating Requirements
|
Grade
|
Heat Treat Type
|
Austenitizing/Solutioning
|
Cooling
|
Quenching Cool
|
Tempering Temperature,
|
|
Temperature, Minimum
|
Media
|
Minimum or
|
|
|
|
or Range, °F [°C]A
|
|
Below °F [°C]
|
Range, °F [°C]
|
|
|
|
Low Alloy Steels
|
|
|
F 5, F 5a
|
anneal
|
1750
|
[955]
|
furnace cool
|
B
|
B
|
|
normalize and temper
|
1750
|
[955]
|
air cool
|
B
|
1250 [675]
|
F 9
|
anneal
|
1750
|
[955]
|
furnace cool
|
B
|
B
|
|
normalize and temper
|
1750
|
[955]
|
air cool
|
B
|
1250 [675]
|
F 91
|
normalize and temper
|
1900-1975 [1040-1080]
|
air cool
|
B
|
1350–1470 [730–800]
|
F 11, Class 1, 2, 3
|
anneal
|
1650
|
[900]
|
furnace cool
|
B
|
B
|
|
normalize and temper
|
1650
|
[900]
|
air cool
|
B
|
1150 [620]
|
F 12, Class 1, 2
|
anneal
|
1650
|
[900]
|
furnace cool
|
B
|
B
|
|
normalize and temper
|
1650
|
[900]
|
air cool
|
B
|
1150 [620]
|
F 22, Class 1, 3
|
anneal
|
1650
|
[900]
|
furnace cool
|
B
|
B
|
|
normalize and temper
|
1650
|
[900]
|
air cool
|
B
|
1250 [675]
|
F 22V
|
normalize and temper or
|
1650
|
[900]
|
air cool or liquid
|
B
|
1250 [675]
|
|
quench and temper
|
|
|
|
|
|
TABLE 2 Chemical RequirementsA
|
Identifi-
|
UNS
|
Grade
|
|
|
|
|
Composition, %
|
|
|
|
|
cation
|
Desig-
|
|
Carbon
|
Manga-
|
Phos-
|
Sulfur
|
Silicon
|
Nickel
|
Chromium
|
Molybde-
|
Colum-
|
Titan-
|
Other
|
Symbol
|
nation
|
|
|
nese
|
phorus
|
|
|
|
|
num
|
bium
|
ium
|
Elements
|
|
|
|
|
|
Low Alloy Steels
|
|
|
|
|
|
|
|
F 5C
|
K41545
|
4 to 6 % chromium
|
0.15
|
0.30–0.60 0.030
|
0.03
|
0.5
|
0.5
|
4.0–6.0
|
0.44–0.65
|
...
|
...
|
...
|
F 5aC
|
K42544
|
4 to 6 % chromium
|
0.25
|
0.6
|
0.04
|
0.03
|
0.5
|
0.5
|
4.0–6.0
|
0.44–0.65
|
...
|
...
|
...
|
F 9
|
K90941
|
9 % chromium
|
0.15
|
0.30–0.60 0.030
|
0.03
|
0.50–1.00
|
...
|
8.0–10.0
|
0.90–1.10
|
...
|
...
|
...
|
F 91
|
K90901
|
9 % chromium, 1 %
|
0.08–0.12
|
0.30–0.60 0.020
|
0.01
|
0.20–0.50
|
0.4
|
8.0–9.5
|
0.85–1.05
|
0.06–0.10 ...
|
N 0.03–0.07
|
|
molybdenum, 0.2 %
|
|
|
Al 0.02D
|
|
|
vanadium plus
|
|
|
|
|
|
|
|
|
|
|
V 0.18–0.25
|
|
columbium and
|
|
|
Ti 0.01D
|
Zr 0.01D
|
|
nitrogen
|
|
|
F 11
|
K11597
|
1.25 % chromium,
|
0.05–0.15
|
0.30–0.60 0.030
|
0.03
|
0.50–1.00
|
...
|
1.00–1.50
|
0.44–0.65
|
...
|
...
|
...
|
Class 1
|
|
0.5 % molybdenum
|
|
|
|
|
|
|
|
|
|
|
|
F 11
|
K11572
|
1.25 % chromium,
|
0.10–0.20
|
0.30–0.80 0.040
|
0.04
|
0.50–1.00
|
...
|
1.00–1.50
|
0.44–0.65
|
...
|
...
|
...
|
Class 2
|
|
0.5 % molybdenum
|
|
|
|
|
|
|
|
|
|
|
|
F 11
|
K11572
|
1.25 % chromium,
|
0.10–0.20
|
0.30–0.80 0.040
|
0.04
|
0.50–1.00
|
...
|
1.00–1.50
|
0.44–0.65
|
...
|
...
|
...
|
Class 3
|
|
0.5 % molybdenum
|
|
|
|
|
|
|
|
|
|
|
|
F 12
|
K11562
|
1 % chromium,
|
0.05–0.15
|
0.30–0.60 0.045
|
0.045
|
0.50 max
|
...
|
0.80–1.25
|
0.44–0.65
|
...
|
...
|
...
|
Class 1
|
|
0.5 % molybdenum
|
|
|
|
|
|
|
|
|
|
|
|
F 12
|
K11564
|
1 % chromium,
|
0.10–0.20
|
0.30–0.80 0.040
|
0.04
|
0.10–0.60
|
...
|
0.80–1.25
|
0.44–0.65
|
...
|
...
|
...
|
Class 2
|
|
0.5 % molybdenum
|
|
|
|
|
|
|
|
|
|
|
|
F 22
|
K21590 chromium-molybdenum
|
0.05–0.15
|
0.30–0.60 0.040
|
0.04
|
0.5
|
...
|
2.00–2.50
|
0.87–1.13
|
...
|
...
|
...
|
Class 1
|
|
|
|
|
|
|
|
|
|
|
|
|
...
|
F 22
|
K21590 chromium-molybdenum
|
0.05–0.15
|
0.30–0.60 0.040
|
0.04
|
0.5
|
...
|
2.00–2.50
|
0.87–1.13
|
...
|
...
|
...
|
Class 3
|
|
|
|
|
|
|
|
|
|
|
|
|
|
F 22V
|
K31835 2.25 % chromium, 1 %
|
0.11–0.15
|
0.30–0.60 0.015
|
0.01
|
0.1
|
0.25
|
2.00–2.50
|
0.90–1.10
|
0.07
|
0.03
|
Cu 0.20
|
|
|
molybdenum, 0.25 %
|
|
|
|
|
|
|
|
|
|
|
V 0.25–0.35
|
|
|
vanadium
|
|
|
|
|
|
|
|
|
|
|
B 0.002
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Ca 0.015E
|
TABLE 3 Tensile and Hardness Requirements A
|
Grade Symbol
|
Tensile Strength,
min, ksi [MPa]
|
Yield Strength, min,
ksi [MPa]B
|
Elongation in 2 in.
[50 mm] or 4D,
min, %
|
Reduction of
Area, min, %
|
Brinell Hardness
Number, HBW
|
Low Alloy Steels
|
F 5
|
70
|
[485]
|
40 [275]
|
20
|
35
|
143–217
|
F 5a
|
90
|
[620]
|
65 [450]
|
22
|
50
|
187–248
|
F 9
|
85
|
[585]
|
55 [380]
|
20
|
40
|
179–217
|
F 91
|
90
|
[620]
|
60 [415]
|
20
|
40
|
190–248
|
F 11 Class 1
|
60
|
[415]
|
30 [205]
|
20
|
45
|
121–174
|
F 11 Class 2
|
70
|
[485]
|
40 [275]
|
20
|
30
|
143–207
|
F 11 Class 3
|
75
|
[515]
|
45 [310]
|
20
|
30
|
156–207
|
F 12 Class 1
|
60
|
[415]
|
32 [220]
|
20
|
45
|
121–174
|
F 12 Class 2
|
70
|
[485]
|
40 [275]
|
20
|
30
|
143–207
|
F 22 Class 1
|
60
|
[415]
|
30 [205]
|
20
|
35
|
170 max
|
F 22 Class 3
|
75
|
[515]
|
45 [310]
|
20
|
30
|
156–207
|
F 22V
|
85–110 [585–780]
|
60 [415]
|
18
|
45
|
174–237
|
A Where ellipses appear in this table, there is no requirement and the test for the value need neither be performed nor a value reported.
B Determined by the 0.2 % offset method. For ferritic steels only, the 0.5 % extension-under-load method may also be used.
C For sections over 5 in. [130 mm] in thickness, the minimum tensile strength shall be 70 ksi [485 MPa].
D For sections over 5 in. [130 mm] in thickness, the minimum tensile strength shall be 65 ksi [450 MPa].
E Longitudinal. The transverse elongation shall be 25 % in 2 in. or 50 mm, min.
F Longitudinal. The transverse reduction of area shall be 45 % min.
G 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]