# Accident 19990320015089A: Beech A2319, Jacksonville, FL, March 20, 1999 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: March 20, 1999, 20:00 local time - Place: Jacksonville, FL - Airport: Jacksonville International - Damage: Substantial damage - Phase of flight: Level Off Touchdown - Operating rules: General operating rules (Part 91) - Location: 30.4940° N, 81.6878° W: Placed by OpenAirDocs at JACKSONVILLE INTL (JAX), within about a mile (OpenAirDocs) - Nearby events: https://openairdocs.org/map.md?lat=30.4940&lon=-81.6878&mi=10 - Aircraft: N3621Q, a cancelled registration (https://openairdocs.org/deregistered/N3621Q-2014-10-02) (OpenAirDocs) - Registry model: Beech A23-19 (registry code 1151212, https://openairdocs.org/model/beech-a23-19) (OpenAirDocs) - Registry engine: Lycoming 0-320 series (registry code 41508, https://openairdocs.org/engine/lycoming-0-320-series) (OpenAirDocs) - Reported make and model: BEECH A2319 - Reported engine: LYC O320E2C - People aboard: 1 - Fatal injuries: 0 - Pilot certificates: Student - Pilot flight hours: 95 total, 90 in this make and model, 40 in the last 90 days - NTSB investigation: [NTSB ATL99LA057](https://openairdocs.org/ntsb/ATL99LA057) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/19990320015089A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (.19)ON MARCH 20, 1999, AT 1955 EASTERN STANDARD TIME, A BEECH 23, N3621Q, GROUND LOOPED, ACCORDING TO THE PILOT, DURING A FULL STOP LANDING AT THE JACKSONVILLE INTERNATIONAL AIRPORT IN JACKSONVILLE, FLORIDA. THE INSTRUCTIONAL FLIGHT WAS OPERATED BY THE STUDENT PILOT UNDER THE PROVISIONS OF TITLE 14 CFR PART 91 WITH NO FLIGHT PLAN FILED. VISUAL WEATHER CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT. THE STUDENT PILOT WAS NOT INJURED. THE AIRPLANE SUSTAINED SUBSTANTIAL AIRFRAME DAMAGE. THE FLIGHT DEPARTED CUMMING, GEORGIA, AT 1630. ACCORDING TO THE STUDENT PILOT, THE SOLO COUNTRY FLIGHT WAS PLANNED WITH A REFUELING STOP IN JACKSONVILLE. THE STUDENT PILOT REPORTED THAT THE DEPARTURE RUNWAY SURFACE AT CUMMING WAS ROUGH AND UNEVEN. AFTER A ROUGH TAKEOFF ROLL FROM CUMMING, THE ENROUTE FLIGHT TO JACKSONVILLE WAS RELATIVELY UNEVENTFUL. UPON ARRIVING IN THE JACKSONVILLE AREA, THE STUDENT PILOT WAS CLEARED FOR AN APPROACH AND LANDING TO RUNWAY 07. THE PILOT STATED THAT DURING THE FIRST TOUCHDOWN HE HEARD A CRACKING OR POPPING SOUND. AT THIS POINT HE ELECTED TO GO-AROUND FOR ANOTHER APPROACH AND LANDING. ON THE SECOND LANDING, THE AIRPLANE TOUCHED DOWN 35 FEET BEYOND THE NUMBE RS ON RUNWAY 07. DURING THE LANDING ROLL, THE STUDENT PILOT RECALLED THAT THE AIRPLANE BECAME UNCONTROLLABLE AND ROTATED 180 DEGREES IN THE CENTER OF THE RUNWAY. AN EXAMINATION OF THE AIRPLANE SEVERAL DAYS LATER DISCLOSED THAT THE AIRPLANE HAD SUSTAINED SUBSTANTIAL AIRFRAME DAMAGE. (FROM .4) THE SOLO CROSS-COUNTRY FLIGHT WAS PLANNED WITH A REFUELING STOP IN JACKSONVILLE. THE STUDENT PILOT REPORTED THAT THE DEPARTURE RUNWAY SURFACE AT THE DEPARTURE AIRPORT WAS ROUGH AND UNEVEN. UPON ARRIVING IN THE JACKSONVILLE AREA, THE STUDENT PILOT WAS CLEARED FOR AN APPROACH TO AND A LANDING ON RUNWAY 07. THE STUDENT PILOT STATED THAT DURING THE FIRST LANDING HE HEARD A CRACKING OR POPPING SOUND. THE STUDENT PILOT DESCRIBED THE TOUCHDOWN AS NORMAL. AT THIS POINT HE ELECTED TO GO-AROUND FOR ANOTHER APPROACH AND LANDING. THE PILOT WAS CLEARED FOR ANOTHER LANDING ON RUNWAY 07, AND AS SOON AS THE AIRPLANE TOUCHED DOWN ON THE RUNWAY SURFACE, IT VEERED TO THE RIGHT. THE AIRPLANE ROTATED 180 DEGREES IN THE CENTER OF THE RUNWAY. THE POST-ACCIDENT EXAMINATION OF THE AIRPLANE DISCLOSED THAT THE NOSE GEAR ATTACH POINT HAD FAILED. THE VISUAL EXAMINATION OF THE FRACTURE SURFACE REVEALED TYPICAL OVERLOAD D EFORMATION. PRIOR TO THIS OCCURRENCE, NO MECHANICAL PROBLEMS WITH THE AIRPLANE WERE REPORTED BY THE PILOT. REPORTEDLY, DURING THE WRECKAGE EXAMINATION, A SMALL AMOUNT OF CORROSION WAS ALSO DISCOVERED ON THE NOSE GEAR ATTACH POINT. (-23)WHILE LANDING AIRCRAFT GROUND LOOPED, STRIKING RIGHT WING TIP LEADING EDGE AND OUTBD. RIB ASSBLY. FAA INSPECTION FOUND RIGHT LOWER ENGINE MOUNT BROKEN AT NOSE GEAR STRUT ATTACH POINT. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ATL99LA057](https://openairdocs.org/ntsb/ATL99LA057), Mar 21, 1999: Beech 23 (N3621Q), Jacksonville, FL, substantial damage. Probable cause: THE OVERLOAD FAILURE OF THE LANDING GEAR ATTACH POINTS DURING TAKEOFF FROM A TURF AIRSTRIP. FACTORS ARE ROUGH AND UNEVEN TERRAIN. From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.