What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Eyewitness report and evidence at the scene shows that the PA-28-140 impacted a 75 foot tall tree on the centerline of the runway just 2,640 feet from the end of runway 30 at Livingston TX during a night approach during what eyewitnesses described as extremely gusty winds. Investigation at the scene shows good continuity to all flight control cables. Propeller and engine were removed from the wreckage and stored at a local hangar. Both wings were more than 50 percent full of gasoline which appeared clean and uncontaminated, gascolator/fuel strainer/carburetor all contained fuel. Inspection of the engine showed clean spark plugs, both magnetos were sparking, and borescope inspection of cylinders was good. Thumb compression good on all four cylinders. Carburetor air box heat valve was in the open (no heat) position and no evidence of impact witness marks to show otherwise. Carburetor floats appeared to be the proper type and the accelerator pump squirted fuel on the first activation when tested. One eyewitness described seeing the white (landing) light and two small "red and blue" lights inflight, seconds before the crash. Eyewitnesses said they saw the flashing anticollision & ldg lights.
As the FAA filed it
(-23) EYEWITNESS REPORT AND EVIDENCE AT THE SCENE SHOWS THAT THE PA-28-140 IMPACTED A 75 FOOT TALL TREE ON THE CENTERLINE OF THE RUNWAY JUST 2,640 FEET FROM THE END OF RUNWAY 30 AT LIVINGSTON TX DURING A NIGHT APPROACH DURING WHAT EYEWITNESSES DESCRIBED AS EXTREMELY GUSTY WINDS. INVESTIGATION AT THE SCENE SHOWS GOOD CONTINUITY TO ALL FLIGHT CONTROL CABLES. PROPELLER AND ENGINE WERE REMOVED FROM THE WRECKAGE AND STORED AT A LOCAL HANGAR. BOTH WINGS WERE MORE THAN 50 PERCENT FULL OF GASOLINE WHICH APPEARED CLEAN AND UNCONTAMINATED, GASCOLATOR/FUEL STRAINER/CARBURETOR ALL CONTAINED FUEL. INSPECTION OF THE ENGINE SHOWED CLEAN SPARK PLUGS, BOTH MAGNETOS WERE SPARKING, AND BORESCOPE INSPECTION OF CYLINDERS WAS GOOD. THUMB COMPRESSION GOOD ON ALL FOUR CYLINDERS. CARBURETOR AIR BOX HEAT VALVE WAS IN THE OPEN (NO HEAT) POSITION AND NO EVIDENCE OF IMPACT WITNESS MARKS TO SHOW OTHERWISE. CARBURETOR FLOATS APPEARED TO BE THE PROPER TYPE AND THE ACCELERATOR PUMP SQUIRTED FUEL ON THE FIRST ACTIVATION WHEN TESTED. ONE EYEWITNESS DESCRIBED SEEING THE WHITE (LANDING) LIGHT AND TWO SMALL "RED AND BLUE" LIGHTS INFLIGHT, SECONDS BEFORE THE CRASH. EYEWITNESSES SAID THEY SAW THE FLASHING ANTICOLLISION & LDG LIGHTS.
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 N98287 · 1
Matched to the same aircraft by N-number and date.