"......the only place you will find documentation of any take off weight for an experimental aircraft is in the aircraft log book where the completion of the phase one testing is documented with the gross weight when the V speeds were determined."
That may be true for a more recent aircraft..., but my Operating Limitations do not require such information to be included in the logs. Only the statement "I certify that this aircraft is controllable through its normal range of speeds and throughout all maneuvers to be executed; and the aircrafthas no hazardous operating characteristics or design features."
(To all) Feel free to attempt to find any reference to any weight (limitation or anything else) in the paperwork for N84KF in the attached pdf documents. Also, any requirement in the documents or any FAR to enter in the logs such information at any time.