Just for the record, 6061 T6 wrought aluminum bars have the following mechanical properties . 6061 T6 is an aircraft quality aluminum alloy, far stronger than many aluminum alloys.
Tensile strength = 45 ksi** (This is the point where stress will break the part)
Yield strength = 40 ksi (This is the point where the bent part will stay bent)
Modulus of Elasticity in tension = 10 X 10^6 psi (This is the materials resistance to bending used to calculate deflections of structures).
Aluminum is subject to failure from high and low cycle fatigue.
Low Carbon Cold Rolled Steel (AISI 1018)*** wrought bars have the following mechanical properties:
Tensile Strength = 64 ksi
Yield Strength = 54 ksi
Modulus of Elasticity in tension = 29 X 10^6 psi
From this one can see that the steel is 42 percent stronger, and 290 percent less likely to deflect a given distance under load.
Steel also has very good resistance to fatigue failures.
The bottom line IMO is the only material to use to support loads in an environment where vibration is common is to use steel for the project.
** "ksi" stands for 1000 times the value in pounds per square inch . 29 ksi = 29,000 pounds per square inch (crossectional area of beam). 64 ksi = 64,000 pounds per square inch (crossectional area of beam).
*** 1018 is one of the weakest of the common steels. A chrome-molly steel will have strengths ranging from 98 to 234 ksi Tensile strength depending on its heat treatment.