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:

Crash of a Piper PA-31-350 Navajo Chieftain off Aguadilla

Date & Time: Oct 27, 2010 at 1740 LT
Operator:
Registration:
N350RL
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Punta Cana - San Juan
MSN:
31-8252049
YOM:
1982
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1902
Captain / Total hours on type:
38.00
Aircraft flight hours:
4736
Circumstances:
The pilot stated he experienced a high temperature in the right engine and a partial loss of engine rpm while at 9,000 feet mean sea level in cruise flight. He requested and received clearance from air traffic control to descend and divert to another airport. He leveled the airplane at 2,500 feet and both engines were operating; however, the right engine experienced a loss of rpm which made it difficult to maintain altitude. The pilot reduced power in both engines, turned the fuel boost pump on, opened the cowl flaps and the engine continued to run with a low rpm. The pilot elected to ditch the airplane in the ocean, instead of landing as soon as practical at the nearest suitable airport, as instructed in the Pilot's Operating Handbook (POH). Additionally, he shut down the right engine before performing the troubleshooting items listed in the POH. He attributed his decision to ditch the airplane to poor single-engine performance and windy conditions. The wind at the destination airport was from 060 degrees at 6 knots and runway 8 was in use at the time of the accident. The airplane was not recovered.
Probable cause:
The pilot's improper decision to ditch the airplane after a reported partial loss of engine power and overheat on one engine for undetermined reasons.
Final Report:

Crash of a Britten-Norman BN-2A-26 Islander in El Prado

Date & Time: Feb 7, 2008 at 1720 LT
Type of aircraft:
Operator:
Registration:
HI-653CA
Flight Phase:
Survivors:
Yes
Schedule:
Santiago de los Caballeros – Punta Cana
MSN:
8
YOM:
1967
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
21405
Circumstances:
The twin engine aircraft was completing a touristic flight from Punta Cana to Santiago de los Caballeros and back. During the return flight to Punta Cana, the pilot elected to make a fuel stop at La Romana because he failed to refuel at Santiago de los Caballeros and was aware that the left tank fuel gage was inoperative. En route, the left engine failed. The pilot elected to restart it but without success. He decided to attempt an emergency landing in a sugarcane field located in El Prado. Upon landing, the aircraft lost its undercarriage and slid for few dozen metres before coming to rest. All nine occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The accident occurred due to the fact that engine # 1 was turned off due to lack of fuel and when making the emergency landing the captain could not keep the aircraft in the correct path of the selected lane for said landing.
Final Report: