When an aircraft takes off with the mass limited by the TODA:
the " balanced take-off distance" equals 115% of the " all engine take-off distance"
the distance from brake release to V1 will be equal to the distance from V1 to the 35 feet point
the actual take-off mass equals the field length limited take-off mass
the end of the runway will be cleared by 35 feet following an engine failure at V1