What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Iic privacy data omitted arrived at the accident scene and noted N14GQ had impacted the ground inverted. The nose, left wing outboard of the engine, and complete empennage were not at the accident scene. The visible portion of the left propeller showed no damage. The right propeller was not immediately located. The left wing had separated outboard of the engine. The control cables were intact to the bell crank, which had pulled out of the structure. The complete empennage was missing and the control cables were broom strawed. The right wing had separated outboard of the engine but was still attached to the fuselage by the control cables. A Piper aircraft representative was present and verified continuity of the flight controls. Examination of the fuel system showed fuel was present in the filter cups for both the left and right sides. Examination of the fuel control valves showed both the left and right valves were functionally correctly and in the correct position. The right propeller was located in a sagebrush bush with the visible portion showing no damage. Both the left and right propeller blades that were buried showed rotational damage.
As the FAA filed it
IIC ^PRIVACY DATA OMITTED^ ARRIVED AT THE ACCIDENT SCENE AND NOTED N14GQ HAD IMPACTED THE GROUND INVERTED. THE NOSE, LEFT WING OUTBOARD OF THE ENGINE, AND COMPLETE EMPENNAGE WERE NOT AT THE ACCIDENT SCENE. THE VISIBLE PORTION OF THE LEFT PROPELLER SHOWED NO DAMAGE. THE RIGHT PROPELLER WAS NOT IMMEDIATELY LOCATED. THE LEFT WING HAD SEPARATED OUTBOARD OF THE ENGINE. THE CONTROL CABLES WERE INTACT TO THE BELL CRANK, WHICH HAD PULLED OUT OF THE STRUCTURE. THE COMPLETE EMPENNAGE WAS MISSING AND THE CONTROL CABLES WERE BROOM STRAWED. THE RIGHT WING HAD SEPARATED OUTBOARD OF THE ENGINE BUT WAS STILL ATTACHED TO THE FUSELAGE BY THE CONTROL CABLES. A PIPER AIRCRAFT REPRESENTATIVE WAS PRESENT AND VERIFIED CONTINUITY OF THE FLIGHT CONTROLS. EXAMINATION OF THE FUEL SYSTEM SHOWED FUEL WAS PRESENT IN THE FILTER CUPS FOR BOTH THE LEFT AND RIGHT SIDES. EXAMINATION OF THE FUEL CONTROL VALVES SHOWED BOTH THE LEFT AND RIGHT VALVES WERE FUNCTIONALLY CORRECTLY AND IN THE CORRECT POSITION. THE RIGHT PROPELLER WAS LOCATED IN A SAGEBRUSH BUSH WITH THE VISIBLE PORTION SHOWING NO DAMAGE. BOTH THE LEFT AND RIGHT PROPELLER BLADES THAT WERE BURIED SHOWED ROTATIONAL DAMAGE.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.