What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
On July 1, 2015, about 1320 central daylight time, a Piper PA-24-250, N6168P, experienced a loss of engine power after takeoff from runway 18 at at rockin m airport (T14), quinlan, Texas and impacted a field. The airplane was destroyed by impact forces and post-crash fire. Both private-rated pilots were fatally injured. The airplane was registered to and operated by the pilot under 14 code of federal regulations part 91 as a personal flight that was not operating on a flight plan. Visual meteorological prevailed at the time of the accident. The flight was originating at the time of the accident.
The airplane wreckage was about 0.32 nautical miles southeast of the runway center and oriented on a west-southwest airplane tail to nose heading. The airplane was upright and exhibited crushing along the wing leading edges and airplane nose. The landing gear jack screw extension equated to a fully extended landing gear, and the cockpit flap control handle was in the flaps fully extended position.
As the FAA filed it
ON JULY 1, 2015, ABOUT 1320 CENTRAL DAYLIGHT TIME, A PIPER PA-24-250, N6168P, EXPERIENCED A LOSS OF ENGINE POWER AFTER TAKEOFF FROM RUNWAY 18 AT AT ROCKIN M AIRPORT (T14), QUINLAN, TEXAS AND IMPACTED A FIELD. THE AIRPLANE WAS DESTROYED BY IMPACT FORCES AND POST-CRASH FIRE. BOTH PRIVATE-RATED PILOTS WERE FATALLY INJURED. THE AIRPLANE WAS REGISTERED TO AND OPERATED BY THE PILOT UNDER 14 CODE OF FEDERAL REGULATIONS PART 91 AS A PERSONAL FLIGHT THAT WAS NOT OPERATING ON A FLIGHT PLAN. VISUAL METEOROLOGICAL PREVAILED AT THE TIME OF THE ACCIDENT. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT.
THE AIRPLANE WRECKAGE WAS ABOUT 0.32 NAUTICAL MILES SOUTHEAST OF THE RUNWAY CENTER AND ORIENTED ON A WEST-SOUTHWEST AIRPLANE TAIL TO NOSE HEADING. THE AIRPLANE WAS UPRIGHT AND EXHIBITED CRUSHING ALONG THE WING LEADING EDGES AND AIRPLANE NOSE. THE LANDING GEAR JACK SCREW EXTENSION EQUATED TO A FULLY EXTENDED LANDING GEAR, AND THE COCKPIT FLAP CONTROL HANDLE WAS IN THE FLAPS FULLY EXTENDED POSITION.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N6168P · 2
Matched to the same aircraft by N-number and date.