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Al alloys of 2xxx series (Al 2024 ) with high specific strength, good fracture toughness, and excellent fatigue properties have been found important applications in the aerospace industry. In commercial Al 2024 alloys, Cu and Mg are the main alloying elements with small amount of Si and other minor elements such as Mn, Zn, Ti and Fe [1][2]. Nonetheless, has recently been reported an increment on strength and hardness by Mg addition (< 2 wt. %); however, this is accompanied by a decrease in ductility and impact resistance [3].the final mechanical properties are a direct function of experimental sequence, the target of this work is to evaluate the effect of Mg addition and solution heat treatment time and on microstructure and hardening during aging of the 2024 Al alloy (Al 2024 ).The Al 2024 alloy fabrication with 0.25 wt. % of Mg additions (Al2024-0.25 Mg) was made by conventional casting, the melt was degassed with argon gas (20 psi) for 5 min and AlTiB was added as grain refiner (0.13 % wt.). Modification with Mg was performed with addition of pure Mg (99.99 %). The solution heat treatment (SHT) was at 495°C for 3, 5 and 7 h. The cold-plastic-deformation treatment involved 5 % thickness reductions by cold-rolling and a final aging step (195°C) at several times. The microstructural characterization was done using a SEM Hitachi model SU3500 and a TEM PHILIPS model CM-200; XRD. The mechanical properties were evaluated using hardness test in accordance with the ASTM standards.The microstructures of Al 2024-0.25 Mg alloy after SHT times of 3, 5 and 7 h are illustrated in Fig. 1. It is observed that in all SHT times, the segregation decreases when is compared with as-cast condition. However, Cu-rich phases remain undissolved. It is probable that a saturation of the aluminum matrix has been reached or longer SHT times are required. The Fig. 2 shows the effect of solution time on aging treatment, the HV values in samples with 5h of solution time are higher than 3 and 7h of solution time. The Fig. 3 shows the micrographs of Al 2024 Alloy after SHT at 5h (a-b) and peak hardening (c-d). In the peak age-hardening is observed the presence of precipitates with the needletype morphology. In addition, rod-like precipitates are identified.

Al alloys possess many favorable characteristics which make them useful in a wide variety of application. Particularly, the Al 2024 alloys are extensively used as structural materials in commercial airplanes owing to their good balance of properties including high specific strength, formability and corrosion resistance [1,2]. These properties are mainly important in the aerospace industry. These alloys are currently used in high volume manufacturing in the aerospace e.g. aircraft wing and fuselage structures are made of T3 and T4 Al 2024 alloy sheet [1][2]. By another hand, the mechanical properties of this alloy can be influenced by artificial aging and by plastic deformation, such as equal channel angular pressing, high pressure torsion and cold rolling. However, only few of thermomechanical treatments have been practically applied to Al alloys, like heat treatment T8 of Al 2024 and T9 of Al 2A12 alloys [4], in which the applied deformation is relatively small. The reason is to avoid the introduction of the non-uniform distribution of dislocation cell structures which may act as nucleation sites of heterogeneous precipitation [4]. Although, it should be mentioned that a significant increase of the strength was achieved by relatively large cold deformation after solution treatment in others studies [5] The Al 2024-0.25 Mg alloy fabrication was made by conventional casting, the melt was degassed with argon gas (20 psi) for 5 min period and AlTiB was added as grain refiner (0.13 % wt.). Modification with Mg was performed with addition of pure Mg (99.99 %). The hot-plastic-deformation treatment consisted of 50% of thickness reduction by hot-rolling at 490°C, followed by a solution heat treatment (SHT) at 495°C and different times. The cold-plastic-deformation treatment involved 5 and 15 % thickness reductions by cold-rolling and a final aging step (195°C) at several times. The microstructural characterization was done using a SEM Hitachi model SU3500 and a TEM PHILIPS model CM-200; XRD. The mechanical properties were evaluated using hardness test in accordance with the ASTM standards.The precipitates with rod-like shapes are analyzed by EDS-Maps-TEM and SADP-TEM (Fig.1). The results shown that the precipitates are rich in the elements Al, Cu and Mn allowing infer that they correspond to the T-phase (Al 20 Cu 2 Mn 3 ) with orthorhombic structure. Has been reported that the presence of this phase during the solution heat treatment have a positive role in promoting dislocation accumulation and grain refinement during plastic deformation, which increase the kinetic of the precipitation during aging. The Fig. 2 show the micrographs of the Al 2024-0.25 Mg alloy with 5 (1) and 15 (2) % plastic deformation under solution condition and peak age-hardening at 300 min. In the peak age-hardening is observed the presence of precipitates with the needle-type morphology. The peak age-hardening in Al 2024-0.25 Mg alloy show the presence of S´ precipitates (Al 2 CuMg) with needle-type morphology. In addition, the apparent number de...