What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
N924WZ, an RV-4, was on approach to runway 7 at Miles Field (3KY9), when the PIC noticed a deer on the runway. He made a low approach to scare away the deer, but when he added full throttle to climb back into the pattern, the engine did not produce full power. The aircraft was still able to climb, and was approaching the departure end of runway 7, so the PIC decided to climb into the pattern to make another approach to runway 7. He kept the traffic pattern "high and tight." Turning base, he realized he was too high and throttled back. The aircraft began to sink faster than the PIC intended, so he again added power, but the aircraft continued to descend. The aircraft impacted the ground close to the tree line south of the approach end of runway 7. Aircraft was substantially damaged. There was no post event fire. Pilot sustained injuries.
Unable to find a mechanical reason for the loss of engine power. Temperature/dewpoint at the time of the accident were reported as 30C and 15C (86F and 59F), which carb ice potential chart indicates could be conducive to "serious icing at glide power."
As the FAA filed it
N924WZ, AN RV-4, WAS ON APPROACH TO RUNWAY 7 AT MILES FIELD (3KY9), WHEN THE PIC NOTICED A DEER ON THE RUNWAY. HE MADE A LOW APPROACH TO SCARE AWAY THE DEER, BUT WHEN HE ADDED FULL THROTTLE TO CLIMB BACK INTO THE PATTERN, THE ENGINE DID NOT PRODUCE FULL POWER. THE AIRCRAFT WAS STILL ABLE TO CLIMB, AND WAS APPROACHING THE DEPARTURE END OF RUNWAY 7, SO THE PIC DECIDED TO CLIMB INTO THE PATTERN TO MAKE ANOTHER APPROACH TO RUNWAY 7. HE KEPT THE TRAFFIC PATTERN "HIGH AND TIGHT." TURNING BASE, HE REALIZED HE WAS TOO HIGH AND THROTTLED BACK. THE AIRCRAFT BEGAN TO SINK FASTER THAN THE PIC INTENDED, SO HE AGAIN ADDED POWER, BUT THE AIRCRAFT CONTINUED TO DESCEND. THE AIRCRAFT IMPACTED THE GROUND CLOSE TO THE TREE LINE SOUTH OF THE APPROACH END OF RUNWAY 7. AIRCRAFT WAS SUBSTANTIALLY DAMAGED. THERE WAS NO POST EVENT FIRE. PILOT SUSTAINED INJURIES.
UNABLE TO FIND A MECHANICAL REASON FOR THE LOSS OF ENGINE POWER. TEMPERATURE/DEWPOINT AT THE TIME OF THE ACCIDENT WERE REPORTED AS 30C AND 15C (86F AND 59F), WHICH CARB ICE POTENTIAL CHART INDICATES COULD BE CONDUCIVE TO "SERIOUS ICING AT GLIDE POWER."
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.