MIL-DTL-46192C(MR)
TABLE II.
Mechanical properties of plate.
_______________________________________________________________________________
Yield strength
Elongation
Thickness,
Tensile strength
0.2% offset
in 2 inches
Direction
inches
min,ksi
min, ksi
min, percent
Long
0.500-1.500
68.0
58.0
7
transverse
1.501-2.000
68.0
58.0
7
2.001-3.000
68.0
59.0
6
3.001-4.000
68.0
59.0
5
Longitudinal
0.500-1.500
66.0
59.0
10
1.501-2.000
66.0
59.0
9
2.001-3.000
67.0
60.0
8
3.001-4.000
68.0
61.0
7
_____________________________________________________________________________
3.7.2 Tolerances. Unless otherwise specified in the contract or
order (see
6.2), the plates submitted for acceptance shall not vary from the
specified
dimensions by an amount greater than the tolerances shown in ANSI
H35.2.
Similarly, the thickness tolerance shall be as specified in table
III.
TABLE III. Thickness tolerances.
___________________________________________________________________________
Ordered thickness,
Tolerance,
inch
inches
Minus
Plus____________
0.500-0.875,
incl.
0.030
1/
0.876-1.125,
incl.
0.035
--
1.126-1.375,
incl.
0.040
--
1.376-1.625,
incl.
0.045
--
1.626-1.875,
incl.
0.050
--
1.876-2.250,
incl.
0.055
--
2.251-2.750,
incl.
0.060
--
2.751-3.000,
incl.
0.065
--
3.001-4.000,
incl.
0.070
--_____________
1/ The values for the plus column are derived from the full range tolerances
specified in table 3.1 (for sheet and plate not specified for aerospace
application) of ANSI H35.2. For example, the tolerance for a 2.0 inch thick by
a 73 inches wide plate would be as follows:
Thickness tolerance (from ANSI H35.2)
0.060
+
Full tolerance less minus tolerance
0.120 - 0.055 = 0.065
Derived plus tolerance
0.065
Tabulated minus tolerance
0.055
-5-
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