Crash of a Cessna 404 Titan II on Roseau

Date & Time: Feb 8, 2015
Type of aircraft:
Operator:
Registration:
YV1139
Flight Type:
Survivors:
Yes
MSN:
404-628
YOM:
1980
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Roseau-Canefield, the pilot encountered difficulties to stop the aircraft that overran. It collided with a fence and came to rest against various obstacles. All seven occupants evacuated safely and the aircraft was damaged beyond repair.

Crash of a Canadair CL-601 Challenger off Aruba: 3 killed

Date & Time: Jan 29, 2015
Type of aircraft:
Operator:
Registration:
N214FW
Flight Phase:
Flight Type:
Survivors:
No
MSN:
3008
YOM:
1983
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft left an airfield located somewhere in the State of Apure, Venezuela, apparently bound for the US with three people on board. While flying north of Punto Fijo, above the sea, the crew was contacted by ATC but failed to respond. Convinced this was an illegal flight, the Venezuelan Authorities decided to send a fighter to intercept the Challenger that was shot down. Out of control, it dove into the Caribbean Sea and crashed off the coast of Aruba Island. All three occupants were killed and on site, more than 400 boxes containing cocaine were found.
Probable cause:
Shot down by the pilot of a Venezuelan Air Force fighter.

Crash of a Learjet 25D in Champotón: 2 killed

Date & Time: Dec 19, 2014 at 1800 LT
Type of aircraft:
Operator:
Registration:
N265TW
Flight Type:
Survivors:
No
MSN:
265
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was performing a flight from Texas and the aircraft was carrying a load consisting of six fuel drums according to a Campeche daily newspaper. The Learjet 25D was flying at a very low altitude, maybe in an attempt to land, when it crashed and burned in an open field located in Champotón, some 40 km south of Campeche. Both crew members were killed. Illegal flight suspected.

Crash of a Cessna 208B Grand Caravan off Belize City

Date & Time: Dec 4, 2014 at 1420 LT
Type of aircraft:
Operator:
Registration:
V3-HHU
Survivors:
Yes
Schedule:
San Pedro – Belize City
MSN:
208B-2025
YOM:
2008
Flight number:
9N281
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Belize City-Sir Barry Bowen Municipal Airport in marginal weather conditions, the single engine aircraft was unable to stop within the remaining distance. It overran, lost its right main gear, plunged into the sea and came to rest in shallow water. All six occupants were rescued and the aircraft was damaged beyond repair.

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 Piper PA-31-425 Pressurized Navajo in Conrado Castillo: 6 killed

Date & Time: Nov 14, 2014 at 1730 LT
Type of aircraft:
Operator:
Registration:
XB-ZAX
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
San Luis Potosí – Ciudad Victoria – Torreón
MSN:
31-46
YOM:
1967
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The twin engine aircraft departed San Luis Potosí on a flight to Torreón with an intermediate stop in Ciudad Victoria, carrying five passengers and one pilot. At the end of the afternoon, while descending to Ciudad Victoria Airport, the pilot encountered poor weather conditions. Too low, the aircraft impacted trees and crashed in a hilly terrain located near Conrado Castillo. The wreckage was found the following morning about 60 km northwest of Ciudad Victoria Airport. The aircraft disintegrated on impact and all six occupants were killed.
Pilot:
Juan José Castro Maldonado
Passengers:
Maribel Lumbreras,
Paulina García Lumbreras,
Lucero Salazar Méndez,
Juana Lumbreras Ruiz,
Guadalupe Lumbreras Ruiz.

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 Short 360-200 off Sint Maarten: 2 killed

Date & Time: Oct 29, 2014 at 1840 LT
Type of aircraft:
Operator:
Registration:
N380MQ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sint Maarten - San Juan
MSN:
3702
YOM:
1986
Flight number:
SKZ7101
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5318
Captain / Total hours on type:
361.00
Copilot / Total flying hours:
1040
Copilot / Total hours on type:
510
Aircraft flight hours:
25061
Aircraft flight cycles:
32824
Circumstances:
On October 29, 2014, at about 1840 Atlantic Standard Time, a Shorts SD3-60, United States registered N380MQ was destroyed when it crashed into the sea shortly after takeoff from Runway 28 at Princess Juliana International Airport, Sint Maarten, Dutch Antilles, Kingdom of the Netherlands. The two crewmembers on board sustained fatal injuries. The aircraft was operated by SkyWay Enterprises Inc. on a scheduled FedEx contract cargo flight to Luis Munoz Marin International Airport, San Juan, Puerto Rico. At 1839 local, Juliana Tower cleared the aircraft for takeoff Runway 28 - maintain heading 230 until passing 4000 feet. At 1840 local, Tower observed the aircraft descending visually and the radar target and data block disappeared. There were no distress calls. Night conditions and rain prevailed at the time of the accident. Coast Guard search crews discovered aircraft debris close to the shoreline about 1 ½ hours later. The Sint Maarten Civil Aviation Authority initiated an investigation in accordance with ICAO Annex 13. Local investigation authority personnel were joined by Accredited Representatives and advisors from the following states: the USA (NTSB/FAA), United Kingdom (AAIB and Shorts Brothers PLC), and Canada (TSB, TC, PWC). Organization of the investigation included the following groups: Operations, Accident Site and Wreckage, Powerplants, Aircraft Maintenance, Air Traffic Services, Meteorology, and GPS Study. The operator made available personnel for interviews but deferred to participate in the groups. Flight recorders were not installed nor required on this cargo configured aircraft. The original FDR and CVR were removed following conversion to cargo only operations. A handheld GPS recovered from submerged wreckage was successfully downloaded. Data revealed the aircraft past the departure runway threshold on takeoff and attained a maximum GPS recorded altitude of 433 feet at 119 knots groundspeed at 18:39:30. The two remaining data points were over the sea and recorded decreasing altitude and increasing airspeed. The wreckage was recovered from the sea and examined by technical experts. Assessment of the evidence concluded there were no airframe or engine malfunctions that would have affected the airworthiness of the aircraft. The experts concluded that the aircraft struck the sea while under normal engine operation. Operations and human performance investigators evaluated the evidence and analyzed extensive interviews. The investigation concluded that the aircraft departed from the expected flight path in an unusual attitude. The pilot flying most likely experienced a somatographic illusion as a result of a stressful takeoff and acceleration from flap retraction. The pilot’s reaction to pitch down while initiating a required heading change led to an extreme unusual attitude. Circumstances indicate the pilot monitoring did not perceive/respond/intervene to correct the flight path and recover from the unusual attitude. The aircraft exceeded the normal maneuvering parameters, the crew experienced a loss of control, and lacking adequate altitude for recovery, the aircraft crashed into the sea.
Probable cause:
The investigation believes the PF experienced a loss of control while initiating a turn to the required departure heading after take-off. Flap retraction and its associated acceleration combined to set in motion a somatogravic illusion for the PF. The PF’s reaction to pitch down while initiating a turn most likely led to an extreme unusual attitude and the subsequent crash. PM awareness to the imminent loss of control and any attempt to intervene could not be determined. Evidence show that Crew resource management (CRM) performance was insufficient to avoid the crash. Contributing factors to the loss of control were environmental conditions including departure from an unfamiliar runway with loss of visual references (black hole), night and rain with gusting winds.
Final Report:

Crash of a Cessna 208 Caravan I in the Laguna de Tres Palos

Date & Time: Oct 24, 2014 at 1600 LT
Type of aircraft:
Operator:
Registration:
XA-WET
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Laguna de Tres Palos - Acapulco
MSN:
208-0294
YOM:
1998
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5240
Captain / Total hours on type:
201.00
Copilot / Total flying hours:
23837
Aircraft flight hours:
1760
Aircraft flight cycles:
1105
Circumstances:
The crew departed Laguna de Tres Palos on a positioning flight to the Acapulco-General Juan N. Álvarez International Airport. During the takeoff procedure, the seaplane started to oscillate from left to right. At a speed of about 45 knots, the crew abandoned the takeoff procedure when the aircraft nosed down, plunged into water and came to rest, inverted and submerged. Both pilots evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Loss of control of the aircraft during a takeoff run from a watery surface due to cross winds.
Final Report:

Crash of a BAe 3101 Jetstream 31 in Punta Cana

Date & Time: Oct 12, 2014 at 2025 LT
Type of aircraft:
Operator:
Registration:
HI816
Survivors:
Yes
Schedule:
San Juan - Punta Cana
MSN:
694
YOM:
18
Crew on board:
3
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3850
Captain / Total hours on type:
3000.00
Aircraft flight hours:
29780
Circumstances:
The twin engine aircraft departed San Juan-Luis Muñoz Marín (Isla Verde) Airport, Puerto Rico, on a charter flight to Punta Cana, carrying two pilots, one flight attendant and 10 crew members from Air Europa positioning to Punta Cana. Following an uneventful flight, the crew completed the approach and landing on runway 08. After a roll of about 1,500 feet, the aircraft deviated to the left, made a 45° turn, veered off runway and came to rest in a wooded area, bursting into flames. All 13 occupants evacuated safely, among them two passengers were slightly injured. The aircraft was destroyed.
Probable cause:
The accident was the consequence of the combination of human and technical factor. During the approach to land, the crew observed a fluctuation in oil pressure in the instrument panel of the #2 (right) engine. After landing, the crew activated the thrust reversers on both engines without waiting for the Beta light, an essential indication to ensure a proper operation of those system. This configuration caused the aircraft to turn sharply to the left at an angle of 45° because the thrust reverser system activated on the left engine only. The fluctuation in the oil pressure observed by the crew on final approach and the malfunction of the right engine was the consequence of an oil leak in flight.
Final Report: