I believe that's one of the reasons many light twin engined aircraft actually have worse safety records compared to single engined light aircraft. If one engine fails at low speed, the plane will probably crash as the rudder doesn't have enough authority to counteract the torque generated by asymmetric thrust. The solution was to build a physically asymmetrical aircraft, like the
Scaled Composites Boomerang. This allows the engines to be spaced much closer together, with the CoG in between them, so an engine failure has only a small impact on flying qualities.

Airliners don't have this problem, however. Only a bigger rudder is required. I wonder if FBW in some aircraft automatically adjusts for an engine out...?
Also, on the flip side... if an engine disintegrates on the VC-10, for example, then it has the possibility of taking out the other engines.
Last edited by Slotback on Fri Dec 18, 2009 12:48 pm, edited 1 time in total.