For those that suggest cast iron blocks, this is the difference.
7075-T651. T651 temper 7075 has an ultimate tensile strength of 570 MPa (83,000 psi) and yield strength of 500 MPa (73,000 psi). It has a failure elongation of 3–9%. These properties can change depending on the form of material used.
Not weldable
2024 T4
Tensile  Yield
  68k      47k
Weldable
6061 T6 
Tensile    yield
   45k        40k
Very weldable
The most commonly used aluminum casting alloy is 356. These specs are for the best grade, heat treated:
Alloy       HT         Tensile     Yield         BHN
A356    T6          40k       30k        75
 356         T6          33k         24k          70
Very weldable
The Yield Strength of common gray cast iron is about 30k but, it doesn't yield much, it breaks. That's why they don't list the yield. Note, the elongation. 
It does have a vibration dampening property that other materials don't have and why it's also used in machine tools.
Grey cast iron (ASTM A48)    C 3.4, Si 1.8, Mn 0.5 
 Yield        Tensile   Elongation   BHN
  --—        50k        0.5        260    
Uses:
Engine cylinder blocks, flywheels, gearbox cases, machine-tool bases 
Possible to be welded
It varies a little but, aluminum weighs about .100 per CI, and cast iron, .260 per CI.
The welded join on all aluminums goes down to 16 to 20k tensile strength (that's the annealed strength) and the surrounding  areas, that reach 300F or more.
Aluminum, is to gummy to machine, in the annealed state and has to be HTed before machining. As I stated before, mil specs require roughing and re-heat treating of larger sections. The reason for that, is to stress relieve the parts. That also applies to forgings.