PAX ABOARD HIGH PERFORMANCE HOME BUILT ACFT TOOK COMMAND AFTER PLT LOST CTL AND STALLED ON LNDG AT DLS.

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ACFT OWNER WAS FLYING HIS LANCAIR 360 FOR THE FLT PORTION OF HIS BFR. HE WAS NOT CURRENT; AND HAD NOT FLOWN FOR APPROX 30 DAYS. HE HAD APPROX 30 HRS IN HIS ACFT; AND HAD BEEN SIGNED OFF AFTER APPROX 10 HRS OF DUAL WITH A PLT ACCEPTABLE TO LANCAIR AND OWNER'S INSURANCE COMPANY. RETURNING TO THE ARPT; AFTER 1 HR OF AIRWORK; OWNER PROCEEDED TO LAND THE ACFT. THE APCH WAS STABLE; AND SPDS WERE AS BRIEFED. OWNER FLARED HIGH; PITCHED UP; DEVELOPED A HIGH RATE OF SINK; AND HIT RWY HARD; TAIL FIRST. THE NOSE CAME DOWN HARD; AND THE ACFT BOUNCED INTO THE AIR; L WING LOW. AS THE OWNER DID NOTHING TO CORRECT; I TOOK CTL AND INITIATED A GAR; UNCERTAIN THAT I COULD SUCCESSFULLY LAND ON THE RWY. AS I CLBED OUT; OWNER RETRACTED THE GEAR. I WAS TOO LATE TO STOP HIS ACTION; AS I WANTED TO LEAVE THE GEAR DOWN; SUSPECTING GEAR DAMAGE. GEAR CAME DOWN (3 GREEN) ON DOWNWIND; AND ACFT WAS LANDED UNEVENTFULLY. WE DECIDED TO TAXI-IN; AND WERE MET BY LCL PLTS; WHO INDICATED WE SHOULD SHUT DOWN. ON GETTING OUT; WE DISCOVERED THE RUDDER HAD BEEN POPPED OFF THE UPPER 2 HINGE PINS; AND WAS HANGING IN THE LOWER PIN. ON WALKING FORWARD TO INSPECT THE GEAR; WE FOUND BOTH PROP BLADES CURLED BACK. THE NOSEWHEEL FORK WAS BENT; AND THE NOSEWHEEL WAS CUT. NO OTHER DAMAGE WAS FOUND TO THE ACFT STRUCTURE OR LNDG GEAR. MY LACK OF EXPERIENCE IN THE ACFT LED TO MY SLOW REACTION TO A LNDG ATTITUDE THAT I KNEW ( OR SAW) TO BE INCORRECT; BUT DID NOT UNDERSTAND WOULD BE CRITICAL SO QUICKLY. I UNDERSTOOD INTELLECTUALLY WHAT NEEDED TO BE DONE; IN TERMS OF 'FLYING' THE ACFT ONTO THE RWY; BUT WAS IN NO WAY PREPARED TO USE CTL (LIFT) SO QUICKLY. I WAS ALSO COMPLACENT ABOUT FLYING WITH AN EXPERIENCED (BUT NOT IN THIS ACFT) PLT ON A BFR. WHEN HE OVER-FLARED; I WAS NOT READY TO HELP SOLVE THE PROB. OUR COMBINED LACK OF EXPERIENCE LEFT US UNPREPARED TO DEAL WITH ANYTHING OUT OF THE CORRECT FLT REGIME.