2014-T6, T6510, and T6511 Extruded bar, rod, and shapes: MIL-HDBK-5J Design Allowables
show SI units (MPa, GPa, kg/m³) open the MIL-HDBK-5J tool compare against temperature find alternatives
| Material class | Aluminum |
| Alloy / temper / form | 2014 / T6, T6510, and T6511 / Extruded bar, rod, and shapes |
| Specifications | AMS 4153 and AMS-QQ-A-200/2 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.1.0, Table 3.2.1.0(g) (pdf page 35 of the chapter file) |
| Dimension bands | 8 |
| Density | 0.101 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 | 0.000–0.749 in | 0.000–0.750 in, area 25–32 in2 | 0.125–0.499 in, area 0–25 in2 | 0.500–0.749 in, area 0–25 in2 | 0.750–1.499 in, area 0–25 in2 | 1.500–1.750 in, area 0–25 in2 | 1.751–2.999 in, area 0–25 in2 | 3.000–4.499 in, area 0–25 in2 | |||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4153 and AMS-QQ-A-200/2 | AMS 4153 and AMS-QQ-A-200/2 | AMS 4153 and AMS-QQ-A-200/2 | AMS 4153 and AMS-QQ-A-200/2 | AMS 4153 and AMS-QQ-A-200/2 | AMS 4153 and AMS-QQ-A-200/2 | AMS 4153 and AMS-QQ-A-200/2 | AMS 4153 and AMS-QQ-A-200/2 | |||||
| Basis | S | S | A | B | A | B | A | B | A | B | S | S | |
| Ftu, ksi | L | 60 | 68 | 60 | 62 | 64 | 68 | 68 | 70 | 68 | 71 | 68 | 68 |
| LT | … | 56 | 60 | … | 64 | … | 63 | … | 61 | … | 61 | 58 | |
| Fty, ksi | L | 53 | 58 | 53 | 57 | 58 | 62 | 60 | 63 | 60 | 63 | 60 | 60 |
| LT | … | 47 | 53 | … | 55 | … | 54 | … | 52 | … | 52 | 49 | |
| Fcy, ksi | L | … | … | 52 | 56 | 57 | 61 | 59 | 62 | 59 | 62 | … | … |
| LT | … | … | … | … | … | … | … | … | … | … | … | … | |
| Fsu, ksi | L | … | … | 35 | 36 | 37 | 39 | 39 | 41 | 39 | 41 | … | … |
| LT | … | … | 35 | … | 37 | … | 39 | … | 39 | … | … | … | |
| Fbru (e/D = 1.5), ksi | L | … | … | 90 | 93 | 96 | 102 | 102 | 105 | 102 | 106 | … | … |
| LT | … | … | 90 | … | 96 | … | 102 | … | 102 | … | … | … | |
| Fbru (e/D = 2.0), ksi | L | … | … | 116 | 120 | 124 | 132 | 132 | 136 | 132 | 138 | … | … |
| LT | … | … | 116 | … | 124 | … | 132 | … | 132 | … | … | … | |
| Fbry (e/D = 1.5), ksi | L | … | … | 73 | 78 | 80 | 85 | 82 | 86 | 82 | 86 | … | … |
| LT | … | … | 73 | … | 80 | … | 82 | … | 82 | … | … | … | |
| Fbry (e/D = 2.0), ksi | L | … | … | 85 | 91 | 93 | 99 | 96 | 101 | 96 | 101 | … | … |
| LT | … | … | 85 | … | 93 | … | 96 | … | 96 | … | … | … | |
| e, % | L | 6 | 7 | 7 | 7 | 7 | 7 | 7 | 7 | 7 | … | 7 | 7 |
| LT | … | 1 | 5 | … | 5 | … | 5 | … | 2 | … | 2 | 1 | |
| E, Msi | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | |
| Ec, Msi | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | |
| G, Msi | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | 0.101 | |
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
| °F | F_tu | F_ty | F_cy | F_su | F_bru | F_bry |
|---|---|---|---|---|---|---|
| -300 | 112.5 | 113.2 | ||||
| -200 | 106.5 | 108.8 | ||||
| -100 | 103.6 | 105.3 | ||||
| 0 | 101.5 | 102.1 | ||||
| 100 | 98.8 | 99 | 98.6 | 99.2 | 99.1 | 99 |
| 200 | 93.3 | 95.1 | 91.8 | 94.5 | 94.7 | 94.6 |
| 300 | 84.3 | 86.5 | 82.9 | 86.9 | 86.7 | 87.7 |
| 400 | 68.4 | 68.2 | 67.3 | 73.1 | 70.1 | 73.4 |
| 500 | 34.9 | 36.2 | 31.8 | 50.9 | 35.1 | 34.9 |
| 600 | 14.6 | 15.3 | 15.8 | 23.3 | 21.7 | 21.3 |
| 700 | 8.1 | 7.6 | 11.2 | 12.8 | 13.2 | 12.8 |
| 800 | 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 Hand forging (Table 3.2.1.0(f))
- 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-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.