What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On June 18, 2009, at approximately 2145 CDT, the flight crew of N182GT encountered severe blowing dust due to a storm front passing through the area. The national weather service was reporting a haboob in the area in the at 2130 CDT. The aircraft impacted a farm approximately 13 miles east of floydada and 2 miles north of Dougherty, Texas. The VFR flight originated in houston and was enroute to plainview, Texas. Two crewmembers were onboard. Plainview UNICOM (pvw) was contacted by the flight crew at approximately 2120 to ask about weather conditions, and again at 2135 to ask about runway availability. Plainview UNICOM attempted to contact the aircraft at 2150 and received no repsonse. The aircraft impacted soft terrain in a near vertical direction on a heading of 110 degrees. The impact was nonsurvivable. The propeller, engine, and instrument panel were located underneath the impact crater approximately 6 feet below surface. Aircraft debris was scatter over 100 yards in an easterly directon. All four corners of the aircraft were accounted for, as was control continuity. The propeller and engine displayed signs indicating engine power on impact.
As the FAA filed it
(-23) ON JUNE 18, 2009, AT APPROXIMATELY 2145 CDT, THE FLIGHT CREW OF N182GT ENCOUNTERED SEVERE BLOWING DUST DUE TO A STORM FRONT PASSING THROUGH THE AREA. THE NATIONAL WEATHER SERVICE WAS REPORTING A HABOOB IN THE AREA IN THE AT 2130 CDT. THE AIRCRAFT IMPACTED A FARM APPROXIMATELY 13 MILES EAST OF FLOYDADA AND 2 MILES NORTH OF DOUGHERTY, TEXAS. THE VFR FLIGHT ORIGINATED IN HOUSTON AND WAS ENROUTE TO PLAINVIEW, TEXAS. TWO CREWMEMBERS WERE ONBOARD. PLAINVIEW UNICOM (PVW) WAS CONTACTED BY THE FLIGHT CREW AT APPROXIMATELY 2120 TO ASK ABOUT WEATHER CONDITIONS, AND AGAIN AT 2135 TO ASK ABOUT RUNWAY AVAILABILITY. PLAINVIEW UNICOM ATTEMPTED TO CONTACT THE AIRCRAFT AT 2150 AND RECEIVED NO REPSONSE. THE AIRCRAFT IMPACTED SOFT TERRAIN IN A NEAR VERTICAL DIRECTION ON A HEADING OF 110 DEGREES. THE IMPACT WAS NONSURVIVABLE. THE PROPELLER, ENGINE, AND INSTRUMENT PANEL WERE LOCATED UNDERNEATH THE IMPACT CRATER APPROXIMATELY 6 FEET BELOW SURFACE. AIRCRAFT DEBRIS WAS SCATTER OVER 100 YARDS IN AN EASTERLY DIRECTON. ALL FOUR CORNERS OF THE AIRCRAFT WERE ACCOUNTED FOR, AS WAS CONTROL CONTINUITY. THE PROPELLER AND ENGINE DISPLAYED SIGNS INDICATING ENGINE POWER ON IMPACT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.