5086-H112 Sheet and plate: MIL-HDBK-5J Design Allowables
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| 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 | 0.096 lb/in3 |
Design Mechanical and Physical Properties (room temperature)
As printed in the handbook table. 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 | 0.500–1.000 in | 1.001–2.000 in | 2.001–3.000 in | |
|---|---|---|---|---|---|
| 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, ksi | L | 36 | 35 | 35 | 34 |
| LT | 36 | 35 | 35 | 34 | |
| Fty, ksi | L | 18 | 16 | 14 | 14 |
| LT | 17 | 16 | 14 | 14 | |
| Fcy, ksi | L | 17 | 15 | 14 | 14 |
| LT | 18 | 16 | 14 | 14 | |
| Fsu, ksi | L | 22 | 21 | 21 | 20 |
| LT | 22 | 21 | 21 | 20 | |
| Fbru (e/D = 1.5), ksi | L | 54 | 52 | 52 | 51 |
| LT | 54 | 52 | 52 | 51 | |
| Fbru (e/D = 2.0), ksi | L | 72 | 70 | 70 | 68 |
| LT | 72 | 70 | 70 | 68 | |
| Fbry (e/D = 1.5), ksi | L | 25 | 24 | 24 | 24 |
| LT | 25 | 24 | 24 | 24 | |
| Fbry (e/D = 2.0), ksi | L | 31 | 28 | 28 | 28 |
| LT | 31 | 28 | 28 | 28 | |
| e, % | L | 8 | 10 | 14 | 14 |
| LT | … | … | … | … | |
| E, Msi | 10.2 | 10.2 | 10.2 | 10.2 | |
| Ec, Msi | 10.4 | 10.4 | 10.4 | 10.4 | |
| G, Msi | 3.85 | 3.85 | 3.85 | 3.85 | |
| ρ, lb/in3 | 0.096 | 0.096 | 0.096 | 0.096 | |
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.