Crash of a Pilatus PC-12/47E in Cat Cay

Date & Time: Mar 8, 2017 at 1246 LT
Type of aircraft:
Operator:
Registration:
N8TS
Flight Type:
Survivors:
Yes
Schedule:
Saint Petersburg - Cat Cay
MSN:
1650
YOM:
2016
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Pilot advised that upon making his approach to land at Cat Cay (MYCC), on short final he experienced an unexpected accelerated sink rate. To compensate for the sink rate he increased the pitch of the aircraft. While going over the threshold, a slight impact was felt as the landing gear came into contact with the seawall. He flew the aircraft until it came to a stop about 600 feet down the runway. No injuries were sustained, aircraft received substantial damage.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain off Nassau: 1 killed

Date & Time: Dec 2, 2014 at 0845 LT
Operator:
Registration:
C6-REV
Flight Phase:
Survivors:
Yes
Schedule:
Governor’s Harbour – Nassau
MSN:
31-7652062
YOM:
1976
Flight number:
302
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
7650
Aircraft flight hours:
11744
Circumstances:
On Tuesday December 2nd, 2014 at approximately 8:45 am (1345Z) a Ferg’s Air Limited, Piper PA-31-350 Navajo aircraft, registration C6-REV, operated as Southern Air Limited Flight 302, ditched in waters approximately 6nm from shore in the southwestern district of New Providence. The flight originated at Governor’s Harbour, Eleuthera (MYEM) with 10+1 persons on board at approximately 8:15 am in Visual Meteorological Conditions (VMC). At around 8:30am, the aircraft 15 nautical miles east of Lynden Pindling International Airport at 4,500 feet contacted Nassau Air Traffic Control Tower. The aircraft was instructed that runway 09 was in use and they can expect a landing on that runway. Upon final approach to runway 09, with the landing gears selected to the “EXTEND” position, only the nose and right main landing gear lights indicated the “down and locked” position. The left main landing gear light did not illuminate to indicate the “down and locked” position, so the landing was aborted and the pilot requested to go around so he could recycle and troubleshoot the landing gear issue. The pilot made a left turn, flew over the north western shoreline and recycled the landing gears a few times and also tried the emergency hand pump in an attempt to extend the gear. Despite all efforts, the left main landing gear light still did not illuminate to indicated the gear was in the safe “down and locked” position. At this time the aircraft was allowed to fly by the tower so that the controller may make a visual check of the landing gears to see if they were in the extended position. The controller advised the pilot that all gears “appeared to be extended”. Once again the pilot proceeded outbound to make another attempt for landing. For this approach the pilot made a right turn over the southwestern shoreline and proceeded downwind to runway 09. While on the downwind to runway 09 the pilot stated he began to experience problems with the right engine. The engine eventually stopped and all attempts to restart were unsuccessful. As a result of single engine operation, level flight could not be maintained even after retracting the gears and cleaning up the airplane. The decision was made by the pilot to ditch in the water vs. attempting to make the airport where numerous trees and obstacles would make the landing more difficult if the runway could not be made. After touching down on the water the most of the occupants were able to evacuate the aircraft through the normal and emergency exits before the aircraft sank into the ocean. One passenger died during the process. Witness stated that “the plane skipped across the water three times before rotating and hitting with a severe impact. The port (left) tail section received the bulk of the impact as did the port side of the plane.” Eye witness further stated that the passenger that died and “luggage from the baggage compartment were ejected from the rear of the plane on the port side.” “Multiple passengers could not swim or were extremely limited in their ability to swim.” Despite the plane having the full complement of survival equipment (life vests), only two were taken out of the aircraft. Passengers were holding on to bags and other debris that floated out of the aircraft as it submerged. Passengers helped each other until rescuers arrived to assist. Estimates from eye witness were that “the entire plane disappeared under water from 30 to 60 seconds after impact.” The depth where the aircraft came to rest on the water was reported as in excess of 6,500 feet. Once the aircraft settled, it submerged and was not able to be recovered. Safety concerns raised by eye witness could not be confirmed as the plane was never recovered.
Probable cause:
The AAIPU determines that the probable causes of this accident as:
- Engine failure and the inability of the aircraft to maintain a safe altitude.
Contributing Factors includes:
- Failure of the left main landing gear.
The following findings were identified:
1. Weather was not a factor in the accident.
2. Air Traffic Services were proper and did not contribute to the cause of the accident.
3. The pilot was properly certified, trained and qualified for the flight.
4. The loss of power on the right engine resulted in the aircraft inability to maintain a safe altitude.
5. The Police and other emergency services response were timely and effective.
6. The depth of the water where the aircraft came to rest made it impossible for the aircraft to be recovered.
7. The aircraft was properly maintained in accordance with Bahamas and United States regulations and maintenance practices.
Final Report:

Crash of a Learjet 35A in Freeport: 9 killed

Date & Time: Nov 9, 2014 at 1652 LT
Type of aircraft:
Registration:
N17UF
Survivors:
No
Site:
Schedule:
Nassau - Freeport
MSN:
258
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
13800
Copilot / Total flying hours:
996
Aircraft flight hours:
12046
Aircraft flight cycles:
10534
Circumstances:
The aircraft crashed into a garbage and metal recycling plant after striking a towering crane in the Grand Bahama Shipyard, while attempting a second landing approach to runway 06 at Freeport International Airport (MYGF), Freeport, Grand Bahama, Bahamas. The aircraft made an initial ILS instrument approach to Runway 06 at the Freeport International Airport but due to poor visibility and rain at the decision height, the crew executed a go around procedure. The crew requested to hold at the published holding point at 2,000 feet while they waited for the weather to improve. Once cleared for the second ILS approach, the crew proceeded inbound from the holding location to intercept the localizer of the ILS system associated with the instrument approach. During the approach, the crew periodically reported their position to ATC, as the approach was not in a radar environment. The crew was given current weather conditions and advised that the conditions were again deteriorating. The crew continued their approach and descended visually while attempting to find the runway, until the aircraft struck the crane positioned at Dock #2 of the Shipyard at approximately 220 feet above sea level, some 3.2 nautical miles (nm) from the runway threshold. A fireball lasting approximately 3 seconds was observed as a result of the contact between the aircraft and the crane. The right outboard wing, right landing gear and right wingtip fuel tank, separated from the aircraft on impact. This resulted in the aircraft travelling out of control, some 1,578 feet (526 yards) before crashing inverted into a pile of garbage and other debris in the City Services Garbage and Metal Recycling Plant adjacent to the Grand Bahama Shipyard. Both crew and 7 passengers were fatally injured. No person on the ground was injured. The crane in the shipyard that was struck received minimal damages while the generator unit and other equipment in the recycling plant received extensive damages.
Probable cause:
The Air Accident Investigation & Prevention Unit (AAIPU) determines that the probable cause(s) of this accident were:
- The poor decision making of the crew in initiating and continuing a descent in IMC below the authorized altitude, without visual contact with the runway environment.
Contributing Factors includes:
- Improper planning of the approach,
- Failure of the crew to follow the approved ILS approach while in IMC conditions,
- Insufficient horizontal or vertical situational awareness,
- Poor decision making,
- Deliberate actions of the crew by disabling the terrain alert warning system,
- Inadequate CRM practice.
Final Report:

Crash of a Cessna 340A off Freeport: 4 killed

Date & Time: Aug 18, 2014 at 1002 LT
Type of aircraft:
Registration:
N340MM
Flight Type:
Survivors:
No
Schedule:
Ormond Beach - Freeport
MSN:
340A-0635
YOM:
1978
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Aircraft flight hours:
5572
Circumstances:
On 18 August, 2014 at 10:02am local time (1402Z) UTC a fixed wing, twin-engine, Cessna 3 4 0 A aircraft, United States registration N340MM, serial number 340A0635, crashed into waters while on a left base to runway 06 at Grand Bahama International Airport (MYGF) Freeport, Grand Bahama, Bahamas. The aircraft departed Ormond Beach Municipal Airport (KOMN) at 8:51am local time (1251Z) for Grand Bahama International Airport (MYGF) on an Instrument Flight Rules (IFR) flight plan with the pilot and three passengers aboard. Sometime after 9:00am (1300Z) an IFR inbound flight plan on N340MM was received by Freeport Approach Control from Miami Center. Upon initial contact with Freeport Approach Control the pilot was given weather advisory, re-cleared to Freeport VOR and told to maintain four thousand feet and report at JAKEL intersection. He was also advised to expect an RNAV runway six approach. After the pilot’s acknowledgement of the information he later acknowledged his position crossing JAKEL. Freeport Approach then instructed the aircraft to descend to two thousand feet and cleared him direct to JENIB intersection for the RNAV runway six (6) approach. After descending to two thousand feet the pilot indicated to Freeport Approach that he had the field in sight and was able to make a visual approach. Freeport Approach re-cleared the aircraft for a visual approach and instructed the pilot to contact Freeport Control Tower on frequency 118.5. At 9:57am (1357Z) N340MM established contact with Freeport Tower and was cleared for the visual approach to runway six; he was told to join the left base and report at five (5) DME. At 10:01am (1401Z) the pilot reported being out of fuel and his intention was to dead stick the aircraft into the airport from seven miles out at an altitude of one thousand five hundred feet. A minute later the pilot radioed ATC to indicate they “were going down and expected to be in the water about five miles north of the airport.” Freeport Tower tried to get confirmation of the last transmission but was unable to. Several more calls went out from Freeport Tower to N340MM but communication was never reestablished. Freeport Control Tower then made request of aircrafts departing and arriving to assist in locating the lost aircraft by over flying the vicinity of the last reported position to see if visual contact could be made. An inbound aircraft reported seeing an aircraft down five miles from the airport on the 300 degree radial of the ZFP VOR. Calls were made to all the relevant agencies and search and rescue initiated. The aircraft was located at GPS coordinates 26˚ 35.708’N and 078˚ 47. 431 W. The aircraft received substantial damage as a result of the impact and crash sequence. There were no survivors.
Probable cause:
The probable cause of this accident has been determined as a lack of situational awareness resulting in a stalled condition and loss of control while attempting to remedy a fuel exhaustion condition at a very low altitude.
Contributing factors:
- The pilot’s incorrect fuel calculations which resulted in fuel exhaustion to both engines.
- Stalled aircraft.
- Loss of situational awareness.
Final Report:

Crash of a Cessna 501 Citation I/SP in Stella Maris

Date & Time: Feb 15, 2014 at 1640 LT
Type of aircraft:
Operator:
Registration:
C-GKPC
Survivors:
Yes
Schedule:
Fort Lauderdale - Stella Maris
MSN:
501-0253
YOM:
1983
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
4579
Circumstances:
The aircraft belly landed at Stella Maris-Estate Airport, Bahamas. No one was hurt but the aircraft was damaged beyond repair. Apparently, the approach checklist was interrupted by the crew for unknown reason and the landing procedure was performed with the landing gear still retracted. The aircraft was owned by the private Canadian company Kelly Panteluk Construction and the airplane was inbound from Fort Lauderdale-Executive.

Crash of a Piper PA-46R-350T Matrix off Cat Cay

Date & Time: Aug 25, 2013 at 1406 LT
Registration:
N720JF
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Cat Cay - Kendall-Miami
MSN:
46-92004
YOM:
2008
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12250
Captain / Total hours on type:
210.00
Aircraft flight hours:
1000
Circumstances:
According to the pilot, he applied full power, set the flaps at 10 degrees, released the brakes, and, after reaching 80 knots, he rotated the airplane. The pilot further reported that the engine subsequently lost total power when the airplane was about 150 ft above ground level. The airplane then impacted water in a nose-down, right-wing-low attitude about 300 ft from the end of the runway. The pilot reported that he thought that the runway was 1,900 ft long; however, it was only 1,300 ft long. Review of the takeoff ground roll distance charts contained in the Pilot’s Operating Handbook (POH) revealed that, with flap settings of 0 and 20 degrees, the ground roll would have been 1,700 and 1,150 ft, respectively. Takeoff ground roll distances were not provided for use of 10 degrees of flaps; however, the POH stated that 10 degrees of flaps could be used. Although the distance was not specified, it is likely that the airplane would have required more than 1,300 ft for takeoff with 10 degrees of flaps. Examination of the engine revealed saltwater corrosion throughout it; however, this was likely due to the airplane’s submersion in water after the accident. No other mechanical malfunctions or abnormalities were noted. Examination of data extracted from the multifunction display (MFD) and primary flight display (PFD) revealed that the engine parameters were performing in the normal operating range until the end of the recordings. The data also indicated that, 7 seconds before the end of the recordings, the airplane pitched up from 0 to about 17 degrees and then rolled 17 degrees left wing down while continuing to pitch up to 20 degrees. The airplane then rolled 77 degrees right wing down and pitched down about 50 degrees. The highest airspeed recorded by the MFD and PFD was about 70 knots, which occurred about 1 second before the end of the recordings. The POH stated that, depending on the landing gear position, flap setting, and bank angle, the stall speed for the airplane would be between 65 and 71 knots. Based on the evidence, it is likely that the engine did not lose power as reported by the pilot. As the airplane approached the end of the runway and the pilot realized that it was not long enough for his planned takeoff, he attempted to lift off at an insufficient airspeed and at too high of a pitch angle, which resulted in an aerodynamic stall at a low altitude. If the pilot had known the actual runway length, he might have used a flap setting of 20 degrees, which would have provided sufficient distance for the takeoff.
Probable cause:
The pilot’s attempt to rotate the airplane before obtaining sufficient airspeed and his improper pitch control during takeoff, which resulted in the airplane exceeding its critical angle-of-attack and subsequently experiencing an aerodynamic stall at a low altitude. Contributing to the accident was the pilot’s lack of awareness of the length of the runway, which led to his attempting to take off with the airplane improperly configured.
Final Report:

Crash of a Saab 340 in Marsh Harbour

Date & Time: Jun 13, 2013 at 1345 LT
Type of aircraft:
Operator:
Registration:
C6-SBJ
Survivors:
Yes
Schedule:
Fort Lauderdale – Marsh Harbour
MSN:
316
YOM:
1992
Flight number:
SBM9561
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
21
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8500
Captain / Total hours on type:
4700.00
Aircraft flight hours:
45680
Aircraft flight cycles:
49060
Circumstances:
On Thursday June 13, 2013 at approximately 1750UTC (1:50pm local time), a fixed wing, twin turboprop regional airliner, was involved in an accident as a result of a runway excursion while landing during heavy rain showers at Marsh Harbor Int’l Airport, Marsh Harbor, Abaco, Bahamas. The aircraft, a SAAB 340B aircraft was operated by SkyBahamas Airlines and bore Bahamas registration C6-SBJ, serial number 316. C6-SBJ departed Fort Lauderdale Int’l Airport (KFLL), Fort Lauderdale, Florida in the USA as Tropical Sky 9561. The airline, SkyBahamas Airline is a Bahamas Air Operator Certificate Holder with approved scheduled operations to and from Fort Lauderdale International Airport, Florida USA (KFLL) and Marsh Harbor Int’l Airport, Marsh Harbor, Abaco in the Bahamas. The crew received weather information and IFR route clearance from KFLL Control Tower. This passenger carrying flight departed KFLL at 1706UTC (1:06pm local) on an instrument flight rules (IFR) flight plan. The point of intended landing was Marsh Harbor International Airport, Abaco, Bahamas (MYAM). The crew selected runway 09 at MYAM for landing. At 17:45:30, the aircraft leveled off at 1,500 feet ASL on a heading of 096 degrees magnetic, with airspeed of 236 knots indicated (KIAS). The flaps were extended to 15 degrees at 17:47:18 with the aircraft level at 1,300 feet ASL, approximately 4.2 nm on the approach. The autopilot was disconnected at 17:47:26 with the aircraft level at 1,300 feet ASL, approximately 3.8 nm on the approach. Heading was 097 degrees magnetic and airspeed was 166 KIAS. The Landing Gear was extended and in the down and locked position by 17:48:01 as the aircraft descended through 730 feet ASL. At 17:48:03, the flaps were extended to landing flap 20 degrees with the aircraft approximately 1.9 nm from the runway on the approach. At 17:48:47, as the aircraft approached the threshold, the power levers were retarded (from 52 degrees) and the engine torques decreased from approximately 20%. Approximately one second later, the aircraft crossed the threshold at a radio altitude of 50 feet AGL on a heading 098 degrees magnetic and airspeed of 171 KIAS. The crew encountered rain showers and a reduction in visibility. The aircraft initially touched down at 17:49:02 with a recorded vertical load factor of +2.16G, approximately 14 seconds after crossing the threshold. There were no indications on the runway to indicate where the initial touchdown had occurred. Upon initial landing however, the aircraft bounced and became airborne, reaching a calculated maximum height of approximately 15 feet AGL. The aircraft bounced a second time at 17:49:07 with a recorded vertical load factor of +3.19* G. During this second bounce, the pitch attitude was 1.8 degrees nose down, heading 102 degrees magnetic and airspeed 106 KIAS. The aircraft made consecutive contact with the runway approximately three times. The third and final bounce occurred at 17:49:14 with a recorded vertical load factor of +3.66G*. During the third bounce, the pitch attitude was 2.2 degrees nose down, heading 099 degrees magnetic and airspeed 98 KIAS. As a result of the hard touchdown, damage was sustained to the right wing and right hand engine/propeller. The right hand engine parameters recorded a rapid loss of power with decreasing engine speed and torque, and subsequent propeller stoppage. The aircraft veered off to the right at approximate time of 17:49:20 on a heading of 131 degrees magnetic at a point approximately 6,044 feet from the threshold of runway 09. The recorded airspeed was 44 KIAS with the left hand engine torque at 26 % and the right hand engine torque at 0%. The aircraft came to a full stop at approximate time 17:49:25 on a heading of 231 degrees magnetic. When the aircraft came to a stop, the flight and cabin crew and twenty-one (21) passengers evacuated the aircraft. The evacuation was uneventful using the main entrance door. Due to the damage sustained by the right wing and engine, evacuation on the right side was not considered. The evacuation occurred during heavy rainfall. No injuries were reported as a result of the accident or evacuation process. The airplane sustained substantial damage as a result of the impact sequence. The elevation of the accident site was reported as approximately 10 feet Mean Sea Level (MSL). Instrument Meteorological Conditions (IMC) prevailed at the time of the accident. The cockpit voice recorder (CVR) uncovered that this crew used no crew resource management or adherence to company standard operating procedures. During the final seconds of the flight, there was complete confusion on the flight deck as to who was in control of the aircraft. After failure of the windshield wiper on the left side of the aircraft, the captain continued to maneuver the aircraft despite having no visual contact of the field due to heavy rain. Sterile Cockpit procedures were not adhered to by this crew as they continued with non-essential conversation throughout the flight regime from engine start up in KFLL up until the “before landing checklist” was requested prior to landing.
Probable cause:
Contributing factors:
- Inexperienced and undisciplined crew,
- Lack of crew resource management training,
- Failure to follow company standard operating procedures,
- Condition known as “get-home-itis” where attempt is made to continue a flight at any cost, even if it means putting aircraft and persons at risk in order to do so,
- Failure to retrieve, observe and respect weather conditions,
- Thunderstorms at the airfield.
Final Report:

Crash of a Cessna 402C II in Mayaguana: 3 killed

Date & Time: Apr 4, 2013 at 0100 LT
Type of aircraft:
Operator:
Registration:
C6-BGJ
Flight Type:
Survivors:
Yes
Schedule:
Nassau - Mayaguana
MSN:
402C-0106
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
On Thursday April 4, 2013 at approximately1:00AM DST (0500 UTC) a fixed wing, twin-engine, Cessna 402C aircraft Bahamas registration C6-BGJ, serial number 402C0106, crashed into obstacles (vehicles) while landing on Runway 06 at Mayaguana International Airport (MYMM), Abraham’s Bay, Mayaguana, Bahamas. The pilot in command stated that on April 3, 2013, he received a call at approximately 9:30PM from the Princess Margaret Hospital requesting emergency air ambulance services out of Mayaguana. The local police on the island was contacted to confirm lighting approval and availability in order to conduct the emergency flight. After confirming lighting arrangements with Nassau Air Traffic Control Services, and obtaining the necessary clearance, the pilot in command, along with a copilot and one passenger, (a nurse), proceeded with the flight to Mayaguana. The flight departed Lynden Pindling International Airport at approximately 1:30PM DST (0330UTC). The destination was Abraham’s Bay, Mayaguana, Bahamas. The pilot in command also reported “about 1 hour and 40 minutes later we arrived at Mayaguana Airport, leveled off at 1500 feet and about 4 miles left base Runway 06, we had the runway in sight via lighting from vehicles.” The crew continued with the landing procedures. The aircraft touch down approximately 300 feet from the threshold on runway 06, the pilot in command reported that prior to the nose gear making contact with the runway “the right wing hit an object (vehicle), causing the aircraft to veer out of control to the right eventually colliding with a second vehicle approximately 300 to 400 feet on the right side (southern) of Runway 06.” The impact of the right wing of the aircraft with the second vehicle, caused the right wing (outboard of the engine nacelle) and right fuel sealed wet wing tank to rupture releasing the aircraft fuel in that wing, which caused an explosion engulfing the vehicle in flames. The force of the impact with the second vehicle caused the right main gear to break away from the aircraft and it was flung ahead and to the left side of the runway approximately 200 feet from the point of impact with the truck. As the right main gear of the aircraft was no longer attached, the aircraft collapsed on its right side, slid onto the gravel south (right) of the runway and somewhere during this process, the nose gear also collapsed. The pilot immediately shut off the fuel valve of the aircraft and once the engines and the aircraft came to a stop, the three occupants evacuated the aircraft. The occupants of the aircraft did not sustain any visible injuries requiring medical attention or hospitalization. However, three (3) occupants of the second vehicle that was struck, were fatally injured. The airplane sustained substantial damages as a result of the impact and post impact crash sequence. The impact with the first vehicle occurred at approximately 427 feet from the threshold of runway 06 and at coordinates 28˚ 22’30”N and 073˚ 01’15’W. The flight was operated on an Instrument Flight Rules flight plan. Instrument Meteorological Conditions (night) prevailed at the time of the accident.
Probable cause:
Breakdown in communication during the planning and execution of an unapproved procedure has been determined to be the probable cause of this accident.
Other contributing factors:
- Use of an unapproved procedure to aid in a maneuver that was critical,
- Too many persons were planning the maneuver and not coordinating their actions,
- Failure of planners of the maneuver to verify whether participants were in the right position,
- Inexperienced persons used in the execution of a maneuver that was not approved,
- Vehicle parked to close to the side of the runway,
- Vehicle left with engine running while parked near the runway.
Final Report:

Crash of a Beechcraft A100 King Air in Deadmans Cay

Date & Time: Mar 9, 2012 at 1410 LT
Type of aircraft:
Operator:
Registration:
N70JL
Survivors:
Yes
Schedule:
Nassau - Deadmans Cay
MSN:
B-87
YOM:
1971
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft was operating a taxi flight from Nassau-Lynden Pindling Airport to Deadmans Cay, and departed Nassau around 1 pm. On approach to Deadmans Cay, the crew encountered technical problems and was unable to lower the gear. The captain decided to perform a belly landing. The aircraft skidded on runway for several yards then veered off runway before coming to rest. There was no fire. While all occupants escaped uninjured, the aircraft was damaged beyond repair.

Crash of a Beechcraft C-45 Expeditor off Nassau: 2 killed

Date & Time: Dec 14, 2010 at 1510 LT
Type of aircraft:
Operator:
Registration:
N38L
Flight Type:
Survivors:
No
Schedule:
Fort Lauderdale – Nassau
MSN:
6323
YOM:
1944
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
While approaching Nassau-Lynden Pindling Airport runway 27 in poor weather conditions (cold front), the twin engine aircraft crashed into the sea few km offshore. Some debris were found floating on water north of Nassau. Both pilots were killed.