5086-H112 Sheet and plate: MIL-HDBK-5J Design Allowables
show US units (ksi, Msi, lb/in³) open the MIL-HDBK-5J tool compare against temperature find alternatives
| Material class | Aluminum |
| Alloy / temper / form | 5086 / H112 / Sheet and plate |
| Specifications | AMS-QQ-A-250/7 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.5.3.0, Table 3.5.3.0(b) (pdf page 238 of the chapter file) |
| Dimension bands | 4 |
| Density | 2657 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 band | 0.188–0.499 in (4.775–12.67 mm) | 0.500–1.000 in (12.7–25.4 mm) | 1.001–2.000 in (25.43–50.8 mm) | 2.001–3.000 in (50.83–76.2 mm) | |
|---|---|---|---|---|---|
| Specification | AMS-QQ-A-250/7 | AMS-QQ-A-250/7 | AMS-QQ-A-250/7 | AMS-QQ-A-250/7 | |
| Basis | S | S | S | S | |
| Ftu, MPa | L | 248.2 | 241.3 | 241.3 | 234.4 |
| LT | 248.2 | 241.3 | 241.3 | 234.4 | |
| Fty, MPa | L | 124.1 | 110.3 | 96.53 | 96.53 |
| LT | 117.2 | 110.3 | 96.53 | 96.53 | |
| Fcy, MPa | L | 117.2 | 103.4 | 96.53 | 96.53 |
| LT | 124.1 | 110.3 | 96.53 | 96.53 | |
| Fsu, MPa | L | 151.7 | 144.8 | 144.8 | 137.9 |
| LT | 151.7 | 144.8 | 144.8 | 137.9 | |
| Fbru (e/D = 1.5), MPa | L | 372.3 | 358.5 | 358.5 | 351.6 |
| LT | 372.3 | 358.5 | 358.5 | 351.6 | |
| Fbru (e/D = 2.0), MPa | L | 496.4 | 482.6 | 482.6 | 468.8 |
| LT | 496.4 | 482.6 | 482.6 | 468.8 | |
| Fbry (e/D = 1.5), MPa | L | 172.4 | 165.5 | 165.5 | 165.5 |
| LT | 172.4 | 165.5 | 165.5 | 165.5 | |
| Fbry (e/D = 2.0), MPa | L | 213.7 | 193.1 | 193.1 | 193.1 |
| LT | 213.7 | 193.1 | 193.1 | 193.1 | |
| e, % | L | 8 | 10 | 14 | 14 |
| LT | … | … | … | … | |
| E, GPa | 70.33 | 70.33 | 70.33 | 70.33 | |
| Ec, GPa | 71.71 | 71.71 | 71.71 | 71.71 | |
| G, GPa | 26.54 | 26.54 | 26.54 | 26.54 | |
| ρ, kg/m³ | 2657 | 2657 | 2657 | 2657 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 5086 Tables
- 5086-H111 Extrusion (Table 3.5.3.0(b))
- 5086-H112 Extrusion (Table 3.5.3.0(b))
- 5086-H32 Sheet and plate (Table 3.5.3.0(b))
- 5086-H34 Sheet and plate (Table 3.5.3.0(b))
- 5086-H36 Sheet and plate (Table 3.5.3.0(b))
- 5086-H38 Sheet and plate (Table 3.5.3.0(b))
- 5086-O Extrusion (Table 3.5.3.0(b))
- 5086-O Sheet and plate (Table 3.5.3.0(b))
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.