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2219-T851 Sheet and plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2219 / T851 / Sheet and plate
SpecificationsAMS-QQ-A-250/30
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.8.0, Table 3.2.8.0(b) (pdf page 168 of the chapter file)
Dimension bands6
Density2851 kg/m³

Design Mechanical and Physical Properties (room temperature)

Converted from the handbook table (ksi, Msi, lb/in³) and rounded to 4 significant figures; dimension bands in inches with mm in parentheses. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.

Dimension band0.250–1.000 in (6.35–25.4 mm)1.001–2.000 in (25.43–50.8 mm)2.001–3.000 in (50.83–76.2 mm)3.001–4.000 in (76.23–101.6 mm)4.001–5.000 in (101.6–127 mm)5.001–6.000 in (127–152.4 mm)
SpecificationAMS-QQ-A-250/30AMS-QQ-A-250/30AMS-QQ-A-250/30AMS-QQ-A-250/30AMS-QQ-A-250/30AMS-QQ-A-250/30
BasisABABABABABAB
Ftu, MPaL420.6427.5420.6427.5……………………
LT427.5434.4427.5434.4427.5434.4413.7420.6406.8413.7393399.9
Fty, MPaL324.1330.9324.1330.9……………………
LT317.2324.1317.2324.1310.3317.2303.4310.3296.5303.4289.6296.5
Fcy, MPaL324.1330.9324.1330.9……………………
LT330.9337.8330.9337.8……………………
Fsu, MPaL248.2248.2248.2248.2……………………
LT248.2248.2248.2248.2……………………
Fbru (e/D = 1.5), MPaL655661.9655661.9……………………
LT655661.9655661.9……………………
Fbru (e/D = 2.0), MPaL834.3848.1834.3848.1……………………
LT834.3848.1834.3848.1……………………
Fbry (e/D = 1.5), MPaL524537.8524537.8……………………
LT524537.8524537.8……………………
Fbry (e/D = 2.0), MPaL648.1648.1634.3648.1……………………
LT648.1648.1634.3648.1……………………
e, %L………………………………
LT887766555544
E, GPa72.3972.3972.3972.39……………………
Ec, GPa74.4674.4674.4674.46……………………
G, GPa27.5827.5827.5827.58……………………
ν0.330.330.330.33……………………
ρ, kg/m³2851285128512851……………………

Effect of Temperature

Percent of the room-temperature value against temperature, digitized from the handbook figures (the shortest exposure of each figure, every 10 °F). Strength curves give the allowable at temperature; "after exposure" curves give the room-temperature property after a soak at that temperature.

Strength allowables at temperature, percent of room temperature

°CF_tu
-184120.6
-129110.4
-73106.9
-18103.8
3898.8
9392
14983.3
20466.5
2646
31631.1
37117.1
4277.6

Factors in percent of the room-temperature allowable.

Other 2219 Tables

Source and Use

U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.