What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On Monday, February 23, 2004 at 8:49 CST N9103Z, a Piper PA-46-310P on an IFR flight plan from panama city, FL (pfn) to tulsa, ok (rvs), broke up in-flight near Arlington, Alabama. Review of the radar data revealed the airplane was at 24,000 feet, heading northwest at 08:46:54. At 08:47:58, the airplane was at 9,600 feet. The last beacon return was at 08:48:44. The airplane was heading southeast at 3,100 feet. The first observed wreckage consisted of the forward fuselage section separated approximately six feet aft of the aircraft instrument panel and minus the right wing section outboard of the landing gear. The left wing was attached minus the left aileron. The engine and propeller were attached. Propeller blade strikes were evidenced approx. 18" from ground level on a tree in front of the wreckage. Paint transfer marks from departed right wing were noted on top of fuselage and extended aft to separation. The second observed wreckage was located a half a mile from the first and consisted of the remaining fuselage section and empennage, minus the horizontal stabilizer and elevator assembly. Paint transfer marks were noted at the separation line of the fuselage and extended diagonally to the aft exit.
As the FAA filed it
(-23) ON MONDAY, FEBRUARY 23, 2004 AT 8:49 CST N9103Z, A PIPER PA-46-310P ON AN IFR FLIGHT PLAN FROM PANAMA CITY, FL (PFN) TO TULSA, OK (RVS), BROKE UP IN-FLIGHT NEAR ARLINGTON, ALABAMA. REVIEW OF THE RADAR DATA REVEALED THE AIRPLANE WAS AT 24,000 FEET, HEADING NORTHWEST AT 08:46:54. AT 08:47:58, THE AIRPLANE WAS AT 9,600 FEET. THE LAST BEACON RETURN WAS AT 08:48:44. THE AIRPLANE WAS HEADING SOUTHEAST AT 3,100 FEET. THE FIRST OBSERVED WRECKAGE CONSISTED OF THE FORWARD FUSELAGE SECTION SEPARATED APPROXIMATELY SIX FEET AFT OF THE AIRCRAFT INSTRUMENT PANEL AND MINUS THE RIGHT WING SECTION OUTBOARD OF THE LANDING GEAR. THE LEFT WING WAS ATTACHED MINUS THE LEFT AILERON. THE ENGINE AND PROPELLER WERE ATTACHED. PROPELLER BLADE STRIKES WERE EVIDENCED APPROX. 18" FROM GROUND LEVEL ON A TREE IN FRONT OF THE WRECKAGE. PAINT TRANSFER MARKS FROM DEPARTED RIGHT WING WERE NOTED ON TOP OF FUSELAGE AND EXTENDED AFT TO SEPARATION. THE SECOND OBSERVED WRECKAGE WAS LOCATED A HALF A MILE FROM THE FIRST AND CONSISTED OF THE REMAINING FUSELAGE SECTION AND EMPENNAGE, MINUS THE HORIZONTAL STABILIZER AND ELEVATOR ASSEMBLY. PAINT TRANSFER MARKS WERE NOTED AT THE SEPARATION LINE OF THE FUSELAGE AND EXTENDED DIAGONALLY TO THE AFT EXIT.
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 N9103Z · 1
Matched to the same aircraft by N-number and date.