2014-T6 Hand forging: 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 | 2014 / T6 / Hand forging |
| Specifications | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.1.0, Table 3.2.1.0(f) (pdf page 34 of the chapter file) |
| Dimension bands | 7 |
| Density | 2796 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 | 0–2 in (0–50.8 mm), area 0–256 in2 (0–165200 mm²) | 2.001–3.000 in (50.83–76.2 mm), area 0–256 in2 (0–165200 mm²) | 3.001–4.000 in (76.23–101.6 mm), area 0–256 in2 (0–165200 mm²) | 4.001–5.000 in (101.6–127 mm), area 0–256 in2 (0–165200 mm²) | 5.001–6.000 in (127–152.4 mm), area 0–256 in2 (0–165200 mm²) | 6.001–7.000 in (152.4–177.8 mm), area 0–256 in2 (0–165200 mm²) | 7.001–8.000 in (177.8–203.2 mm), area 0–256 in2 (0–165200 mm²) | |
|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 | AMS 4133, AMS-A-22771, and AMS-QQ-A-367 | |
| Basis | S | S | S | S | S | S | S | |
| Ftu, MPa | L | 448.2 | 441.3 | 434.4 | 427.5 | 420.6 | 413.7 | 406.8 |
| LT | 448.2 | 441.3 | 434.4 | 427.5 | 420.6 | 413.7 | 406.8 | |
| ST | … | 427.5 | 420.6 | 413.7 | 406.8 | 399.9 | 393 | |
| Fty, MPa | L | 386.1 | 386.1 | 379.2 | 372.3 | 365.4 | 358.5 | 351.6 |
| LT | 386.1 | 379.2 | 379.2 | 372.3 | 365.4 | 358.5 | 351.6 | |
| ST | … | 379.2 | 372.3 | 365.4 | 365.4 | 358.5 | 351.6 | |
| Fcy, MPa | L | 386.1 | 386.1 | 379.2 | 372.3 | 365.4 | … | … |
| LT | 386.1 | 379.2 | 379.2 | 372.3 | 365.4 | … | … | |
| ST | … | … | … | … | … | … | … | |
| Fsu, MPa | L | 275.8 | 268.9 | 268.9 | 262 | 262 | … | … |
| LT | 275.8 | 268.9 | 268.9 | 262 | 262 | … | … | |
| ST | … | 268.9 | 268.9 | 262 | 262 | … | … | |
| Fbru (e/D = 1.5), MPa | L | 627.4 | 620.5 | 606.7 | 599.8 | 586.1 | … | … |
| LT | 627.4 | 620.5 | 606.7 | 599.8 | 586.1 | … | … | |
| ST | … | 620.5 | 606.7 | 599.8 | 586.1 | … | … | |
| Fbru (e/D = 2.0), MPa | L | 806.7 | 792.9 | 779.1 | 772.2 | 758.4 | … | … |
| LT | 806.7 | 792.9 | 779.1 | 772.2 | 758.4 | … | … | |
| ST | … | 792.9 | 779.1 | 772.2 | 758.4 | … | … | |
| Fbry (e/D = 1.5), MPa | L | 537.8 | 537.8 | 530.9 | 524 | 510.2 | … | … |
| LT | 537.8 | 537.8 | 530.9 | 524 | 510.2 | … | … | |
| ST | … | 537.8 | 530.9 | 524 | 510.2 | … | … | |
| Fbry (e/D = 2.0), MPa | L | 620.5 | 620.5 | 606.7 | 599.8 | 586.1 | … | … |
| LT | 620.5 | 620.5 | 606.7 | 599.8 | 586.1 | … | … | |
| ST | … | 620.5 | 606.7 | 599.8 | 586.1 | … | … | |
| e, % | L | 8 | 8 | 8 | 7 | 7 | 6 | 6 |
| LT | 3 | 3 | 3 | 2 | 2 | 2 | 2 | |
| ST | … | 2 | 2 | 1 | 1 | 1 | 1 | |
| E, GPa | 72.39 | 72.39 | 72.39 | 72.39 | 72.39 | 72.39 | 72.39 | |
| Ec, GPa | 74.46 | 74.46 | 74.46 | 74.46 | 74.46 | 74.46 | 74.46 | |
| G, GPa | 27.58 | 27.58 | 27.58 | 27.58 | 27.58 | 27.58 | 27.58 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, kg/m³ | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | 2796 | |
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
Moduli at temperature
Elongation and exposure effects
| °C | F_tu | F_ty | F_cy | F_su | F_bru | F_bry |
|---|---|---|---|---|---|---|
| -184 | 112.5 | 113.2 | ||||
| -129 | 106.5 | 108.8 | ||||
| -73 | 103.6 | 105.3 | ||||
| -18 | 101.5 | 102.1 | ||||
| 38 | 98.8 | 99 | 98.6 | 99.2 | 99.1 | 99 |
| 93 | 93.3 | 95.1 | 91.8 | 94.5 | 94.7 | 94.6 |
| 149 | 84.3 | 86.5 | 82.9 | 86.9 | 86.7 | 87.7 |
| 204 | 68.4 | 68.2 | 67.3 | 73.1 | 70.1 | 73.4 |
| 26 | 34.9 | 36.2 | 31.8 | 50.9 | 35.1 | 34.9 |
| 316 | 14.6 | 15.3 | 15.8 | 23.3 | 21.7 | 21.3 |
| 371 | 8.1 | 7.6 | 11.2 | 12.8 | 13.2 | 12.8 |
| 427 | 4.9 |
Factors in percent of the room-temperature allowable.
Other 2014 Tables
- 2014-T6 Clad sheet (Table 3.2.1.0(c))
- 2014-T6 Die forging (Table 3.2.1.0(e))
- 2014-T6 Sheet (Table 3.2.1.0(b))
- 2014-T6 and T651 Bar, rod, and shapes, rolled, drawn, or cold-finished (Table 3.2.1.0(d))
- 2014-T6, T6510, and T6511 Extruded bar, rod, and shapes (Table 3.2.1.0(g))
- 2014-T62 Bar, rod, and shapes, rolled, drawn, or cold-finished (Table 3.2.1.0(d))
- 2014-T62 Clad plate (Table 3.2.1.0(c))
- 2014-T62 Clad sheet (Table 3.2.1.0(c))
- 2014-T62 Extruded bar, rod, and shapes (Table 3.2.1.0(g))
- 2014-T62 Plate (Table 3.2.1.0(b))
- 2014-T62 Sheet (Table 3.2.1.0(b))
- 2014-T651 Clad plate (Table 3.2.1.0(c))
- 2014-T651 Plate (Table 3.2.1.0(b))
- 2014-T652 Die forging (Table 3.2.1.0(e))
- 2014-T652 Hand forging (Table 3.2.1.0(f))
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.