THE PIC & AN FAA EXAMINER (F/E) WERE ON A PART 135 CHECK FLT. ABT 900' TO 1000' AGL, THE F/E INITIATED AN AUTOROTATION (A/R) WITH INTENTIONS OF A PWR RECOVERY, ALTHO NO PROCEDURE FOR PERFORMING PWR RECOVERY FM AN A/R WAS PUBLISHED IN THE FLT MANUAL (F/M). HE INITIATED THE A/R BY MOVG THE FUEL FLOW CONTROL/POWER LEVER (FFC) OUT OF THE FULL FWD (PWR LOCKED) PSN. AT ABT 400' AGL & 65 KTS, THE FFC WAS PSND BACK TO THE FULL FWD (DETENT) PSN. AT ABT 65' AGL, THE PIC INITIATED A FLARE WITH COLLECTIVE PITCH CTL, BUT THE ENG LACKED RESPONSE. THE PIC CONTD THE A/R TO TOUCHDOWN ON SOFT TRRN. DRG THE LNDG, THE TAIL ROTOR STRUCK A MOUND OF DIRT, BOTH TAIL ROTOR BLADES SEPD, THEN THE HELICOPTER ROLLED ON ITS RGT SIDE & CAME TO REST. INV REVEALED THE GOVERNOR ANTICIPATOR WOULD NOT HAVE ACTIVATED UNTIL COLLECTIVE PITCH WAS APPLIED & THE ENG COULD TAKE UP TO 9 SEC TO SPOOL UP. F/M ADDRESSED ONLY FULL STOP (A/R) LNDGS. MANUAL FOR AEROSPATIALE INSTRUCTORS RESTRICTED PWR RCVRY TO 200' AGL. NO MECH STOP WAS PROVIDED TO KEEP THE ENG FM GOING BLO 50% DRG PWR RDCN FOR A/R.