What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) During final approach to the Madera muni airport (mae), the aircraft experienced a loss of engine power and landed short of runway 30 approximately 215 feet in the dirt. There were no injuries sustained when the aircraft finally came to rest. The pilot-in-charge (PIC) reported the engine began to sputter and eventually stopped operating while on final approach with an airspeed of 70 knots and an altitude of 600 feet and carburetor heat on. Upon impact, the aircraft's lower nose gear strut was torn-off (no damage to the firewall) and there was minor damage found on the left wing tip due to it contacting the ground. The aircraft'f fuel system was investigated for any possible contamination, which was found to be satisfactory. Also, the carburetor heat (air box) control valve was checked along with the engine's timing prior to operation and both were found to be satisfactory. There were no unusual airworthiness items found that contributed to the stoppage of the engine. A teardown of the engine to comply with the manufacturer's recommendation of inspecting the internal components for sudden engine stoppage prior to returning the engine back to service is pending.
As the FAA filed it
(-23) DURING FINAL APPROACH TO THE MADERA MUNI AIRPORT (MAE), THE AIRCRAFT EXPERIENCED A LOSS OF ENGINE POWER AND LANDED SHORT OF RUNWAY 30 APPROXIMATELY 215 FEET IN THE DIRT. THERE WERE NO INJURIES SUSTAINED WHEN THE AIRCRAFT FINALLY CAME TO REST. THE PILOT-IN-CHARGE (PIC) REPORTED THE ENGINE BEGAN TO SPUTTER AND EVENTUALLY STOPPED OPERATING WHILE ON FINAL APPROACH WITH AN AIRSPEED OF 70 KNOTS AND AN ALTITUDE OF 600 FEET AND CARBURETOR HEAT ON. UPON IMPACT, THE AIRCRAFT'S LOWER NOSE GEAR STRUT WAS TORN-OFF (NO DAMAGE TO THE FIREWALL) AND THERE WAS MINOR DAMAGE FOUND ON THE LEFT WING TIP DUE TO IT CONTACTING THE GROUND. THE AIRCRAFT'F FUEL SYSTEM WAS INVESTIGATED FOR ANY POSSIBLE CONTAMINATION, WHICH WAS FOUND TO BE SATISFACTORY. ALSO, THE CARBURETOR HEAT (AIR BOX) CONTROL VALVE WAS CHECKED ALONG WITH THE ENGINE'S TIMING PRIOR TO OPERATION AND BOTH WERE FOUND TO BE SATISFACTORY. THERE WERE NO UNUSUAL AIRWORTHINESS ITEMS FOUND THAT CONTRIBUTED TO THE STOPPAGE OF THE ENGINE. A TEARDOWN OF THE ENGINE TO COMPLY WITH THE MANUFACTURER'S RECOMMENDATION OF INSPECTING THE INTERNAL COMPONENTS FOR SUDDEN ENGINE STOPPAGE PRIOR TO RETURNING THE ENGINE BACK TO SERVICE IS PENDING.