I flew with guy yesterday who was thinking about buying a DA-20 or similer comosite constructed aircraft. As we were talking about adavantages and disadvantages of buying a newer composite vs. an older single (Archer, 172 etc.) he asked me about airframe life of a composite aircaraft. I am unsure about specifics in this area, if there is a max life for a composite aircraft or what long term tests have shown. Does a composite airframe have a limited life, or have substantial differences in durablity than a aluminum aircraft? Thanks for your respones.