Nassau – Cockburn Town

On October 5, 2010 at 12:36 PM, Nassau – Cockburn Town experienced a crash involving Cessna 402, operated by Acklins Blue Charters - ABC Charters, with the event recorded near Nassau-Lynden Pindling New Providence.

The flight was categorized as charter/taxi (non scheduled revenue flight) and the reported phase was takeoff (climb) at a lake, sea, ocean, river crash site.

9 people were known to be on board, 9 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.

Crew on board: 2, crew fatalities: 2, passengers on board: 7, passenger fatalities: 7, other fatalities: 0.

The listed crash cause is technical failure. On October 5, 2010 about 1636 UTC / 12:36pm Eastern Daylight Time (EDT), C6-NLH a Cessna 402C aircraft registered to Lebocruise Air Limited and operated by Acklins Blue Air Charter/Nelson Hanna crashed into lake Killarney shortly after becoming airborne from runway 14 at Lynden Pindling International Airport, Nassau, New Providence, Bahamas. The airplane sustained substantial damages by impact forces. The pilot, copilot and seven (7) passengers aboard the airplane received fatal injuries. The aircraft was on a passenger carrying flight from Lynden Pindling Intl Airport (MYNN) to Cockburn Town, San Salvador, Bahamas (MYSM). The aircraft was on a visual flight rules flight plan. Visual meteorological conditions prevailed at the time of the accident. The official notification of the accident was made to the Manager of the Flight Standards Inspectorate at Lynden Pindling Intl Airport, Nassau, N. P., Bahamas shortly thereafter. The investigation began the same day at approximately 1655 UTC upon notification of the IIC. The investigation was conducted by the Bahamas Civil Aviation Department [BCAD], Inspector Delvin R. Major (Investigator-in-Charge) of the Air Accident Investigation and Prevention Unit (AAIPU), Management of BCAD and Flight Standards Inspectorate (FSI), Airworthiness Inspectors, Operations Inspectors, Human Factors and other administrative staff. Valuable assistance was also received from the National Transportation Safety Board (NTSB), the Federal Aviation Administration (FAA) and Manufacturers of the aircraft and engine components. Three (3) Air Operator Certificate (AOC) holders at the Domestic Section of Lynden Pindling Intl Airport stated that on the day of the accident flight; one of the victims of the accident aircraft approached each of them individually at different times, requesting a quote and their availability to conduct a charter flight to Cockburn Town, San Salvador, Bahamas. Each AOC holder reported that they declined to conduct the charter because by looking at the amount of luggage and other equipment that accompanied the passengers and the size of the passengers that wanted to travel, in their estimation the combined weight appeared to be in excess of the weight that their respective aircraft (Cessna 402C and Hawker Beechcraft B100) can accommodate. After the AOC holders declined to conduct the charter, sometime thereafter, the same individual that was arranging the flight with the previous AOC holders made contact with Nelson Hanna / Acklins Blue Air Charter where arrangements were made to conduct the charter flight. The aircraft type certificate allowed for the aircraft to be operated by one (1) pilot, but the fatal flight was operated by a crew of two (2) pilots (according to eyewitness reports). The aircraft actual weight and center of gravity was unknown. As far as could be determined, the takeoff weight exceeded the maximum weight allowed of 6,850 pounds by more than 500 pounds. This excess in weight also placed the center of gravity of the aircraft outside of the safe envelope / limits for flight allowed by the manufacturer. The flight crew was given instructions by ATC to taxi from the business aviation apron (Executive Flight Support) for a takeoff on Runway 14 at intersection Foxtrot. (Intersection Foxtrot is 2,000 feet beyond the threshold of Runway 14, with a take-off run available of 9,353 feet. (Runway 14 - 11,353 feet long by 150 feet wide, see Appendix 5.15). According to eyewitness reports, from the initiation of takeoff power up to the point when the aircraft lost control white smoke was observed trailing behind the left engine of the aircraft. Eyewitnesses also reported that the take off appeared normal with gear being retracted shortly after takeoff and the aircraft seemed to be struggling to climb. The aircraft was seen at a low height, turning in a left direction over the lake as if trying to return for a landing at the airport. The bank of the aircraft changed from shallow to very steep to almost perpendicular to the ground, gears were extended and almost immediately the aircraft lost control and nose dived into the lake inverted. It cart wheeled, coming to rest upright, approximately ¼ mile from the approach end of runway 27. The aircraft came to rest on an approximate heading of 210 degrees. Eyewitness also reported hearing the engine run for a few seconds after the aircraft made contact with the water of the lake. There were no reports from the pilot to ATC of an emergency or any abnormalities with the aircraft or its systems after takeoff. The flight plan form filed for this flight listed one (1) soul on board; however, there were 7 additional occupants including a “second pilot” discovered onboard the accident flight the day of the accident. The aircraft's recovery and search for luggage, equipment and additional victims commenced shortly after the accident. This effort however, was hampered by inclement weather, rough lake conditions and darkness. On October 6th, the day after the crash, aircraft recovery continued. Family members of an additional person believed to be on board, advised the authorities that there was a ninth (9th) person on board. Search to recover any additional bodies continued but search and recovery efforts proved fruitless. On October 7th, the second day after the crash, the body of the ninth (9th) victim was found in the marshes and recovered from the southwestern end of the lake in the vicinity of where the fatal crash occurred.

Aircraft reference details include registration C6-NLH, MSN 402C-0458, year of manufacture 1981.

Geospatial coordinates for this crash are approximately 25.0493°, -77.4658°.