2026-T3511 Extrusions: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2026 / T3511 / Extrusions |
| Specifications | AMS 4338 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.5.0, Table 3.2.5.0(b) (pdf page 153 of the chapter file) |
| Dimension bands | 5 |
| Density | 0.1 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 | 0.000–0.249 in | 0.250–0.499 in | 0.500–1.499 in | 1.500–2.249 in | 2.250–3.250 in | |||||
|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4338 | AMS 4338 | AMS 4338 | AMS 4338 | AMS 4338 | |||||
| Basis | A | B | A | B | A | B | A | B | S | |
| Ftu, ksi | L | 66 | 69 | 70 | 72 | 72 | 75 | 73 | 76 | 73 |
| LT | 58 | 61 | 62 | 64 | 66 | 67 | 64 | 67 | 61 | |
| Fty, ksi | L | 48 | 51 | 52 | 53 | 53 | 56 | 54 | 57 | 54 |
| LT | 41 | 44 | 45 | 46 | 46 | 48 | 44 | 49 | 42 | |
| Fcy, ksi | L | 43 | 45 | 46 | 47 | 47 | 47 | 49 | 52 | 50 |
| LT | 42 | 45 | 46 | 46 | 46 | 49 | 45 | 47 | 43 | |
| Fsu, ksi | L | 37 | 39 | 37 | 38 | 32 | 33 | 32 | 33 | 32 |
| LT | 37 | 39 | 37 | 38 | 32 | 33 | 32 | 33 | 32 | |
| Fbru (e/D = 1.5), ksi | L | 90 | 94 | 92 | 95 | 87 | 90 | 85 | 89 | 85 |
| LT | 90 | 94 | 92 | 95 | 87 | 90 | 85 | 89 | 85 | |
| Fbru (e/D = 2.0), ksi | L | 112 | 117 | 113 | 117 | 109 | 114 | 108 | 112 | 105 |
| LT | 112 | 117 | 113 | 117 | 109 | 114 | 108 | 112 | 105 | |
| Fbry (e/D = 1.5), ksi | L | 62 | 66 | 66 | 67 | 61 | 64 | 61 | 64 | 61 |
| LT | 62 | 66 | 66 | 67 | 61 | 64 | 61 | 64 | 61 | |
| Fbry (e/D = 2.0), ksi | L | 76 | 81 | 81 | 83 | 76 | 81 | 76 | 80 | 76 |
| LT | 76 | 81 | 81 | 83 | 76 | 81 | 76 | 80 | 76 | |
| e, % | L | 11 | 11 | 12 | 12 | 11 | 11 | 11 | 11 | 10 |
| LT | … | … | … | … | 8 | 8 | 8 | 8 | 8 | |
| E, Msi | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | |
| Ec, Msi | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | |
| G, Msi | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | 4 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
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.