For a start you'd be looking at a wingspan far greater then 55ft. Over 100ft and probably more than 150ft. Therein, considering the fragility of making a structure light enough (even if can find 6 very light cyclopilots), lies just one of the problems that would be encountered.
I've only ever seen single seat types of pedal powered aircraft (although I haven't spent a lot of time looking). Using two or more people would throw up a few problems.
Using rough figures, take the Gossamer Condor, the first successful pedal aircraft. The
wing span was approximately 30m, the
wing chord (length of the wing between the leading edge and the trailing edge) looked around 3m, so roughly the wing area was 90sqm (30x3, and
using a basic assumption that the wing is a rectangle in plan view). The weight was around 30kg, and with a (light) cyclist/pilot in it would be around 90kg. This would give a
wing loading of 1kg/sqm.
Put another pilot in, and say that weight goes up to about 150kg. Now in order to get the same craft in the air with the same performance (ie
wing loading) the wing area would need to be increased (conveniently with these numbers) 150sqm. Using the same chord of 3m, and just varying the span you can see a span of 50m would now be