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 Pilatus PC-12/47 in Kamphaeng Saen: 1 killed

Date & Time: Mar 5, 2017 at 1916 LT
Type of aircraft:
Operator:
Registration:
VT-AVG
Flight Type:
Survivors:
Yes
Schedule:
New Delhi – Calcutta – Bangkok
MSN:
888
YOM:
2008
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The single engine aircraft departed New Delhi at 0842LT on an ambulance flight to Bangkok with two pilots and three doctors on board. A refueling stop was completed at Calcutta Airport. At 1903LT, en route to Bangkok-Don Mueang Airport, the crew contacted ATC and requested permission to divert to Kamphaeng Saen Airport due to an emergency. The permission was granted and the crew initiated the descent when the aircraft disappeared from radar screens at 1916LT. The burned wreckage was found an hour and 30 minutes later, at 2048LT, in a wooded area located few km from runway 22L threshold. All five occupants were injured while the aircraft was destroyed. Few hours later, the copilot died from his injuries.

Crash of a Cessna 421B Golden Eagle II in Cherokee County: 1 killed

Date & Time: Mar 4, 2017 at 0023 LT
Registration:
N421KL
Flight Type:
Survivors:
No
Schedule:
Tulsa - Cherokee County
MSN:
421B-0015
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4000
Aircraft flight hours:
7522
Circumstances:
The 69-year-old commercial pilot was making a personal cross-country flight in the newly purchased airplane. When the airplane was on final approach to the destination airport in night visual meteorological conditions, airport surveillance video showed it pitch up and roll to the right. The airplane then descended in a nose-down attitude to impact in a ravine on the right side of the runway. During the descent over the ravine the right wing came in contact with a powerline that briefly cut power to the airport. Postaccident examination of the airframe, engines, and their components revealed no evidence of mechanical anomalies or malfunctions that would have precluded normal operation. The pilot's toxicology findings identified five different impairing medications: clonazepam, temazepam, hydrocodone, nortriptyline, and diphenhydramine. Although the results were from cavity blood and may not accurately reflect antemortem levels, the hydrocodone, temazepam, and diphenhydramine levels were high enough to likely have had some psychoactive effects. While the exact effects of these drugs in combination are not known, it is likely that the pilot was impaired to some degree by his use of this combination of medications, which likely contributed to his failure to maintain control of the airplane.
Probable cause:
The pilot's failure to maintain control of the airplane during a night visual landing approach. Contributing to the accident was the pilot's impairment due to his use of a combination of medications.
Final Report:

Crash of a Beechcraft G18S off Metlakatla

Date & Time: Mar 3, 2017 at 0815 LT
Type of aircraft:
Operator:
Registration:
N103AF
Flight Type:
Survivors:
Yes
Schedule:
Klawock – Ketchikan
MSN:
BA-526
YOM:
1960
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10308
Captain / Total hours on type:
330.00
Aircraft flight hours:
17646
Circumstances:
The pilot of the twin-engine airplane and the pilot-rated passenger reported that, during a missed approach in instrument meteorological conditions, at 2,000 ft mean sea level, the right engine seized. The pilot attempted to feather the right engine by pulling the propeller control to the feather position; however, the engine did not feather. The airplane would not maintain level flight, so the pilot navigated to a known airport, and the passenger made emergency communications with air traffic control. The pilot was unable to maintain visual reference with the ground until the airplane descended through about 100 to 200 ft and the visibility was 1 statute mile. The pilot stated that he was forced to ditch the airplane in the water about 5 miles short of the airport. The pilot and passenger egressed the airplane and swam ashore before it sank in about 89 ft of water. Both the pilot and passenger reported that there was postimpact fire on the surface of the water. The airplane was not recovered, which precluded a postaccident examination. Thus, the reason for the loss of engine power could not be determined.
Probable cause:
An engine power loss for reasons that could not be determined because the airplane was not recovered.
Final Report:

Crash of a Piper PA-46-310P Malibu in Chichén Itzá

Date & Time: Feb 15, 2017 at 2000 LT
Operator:
Registration:
N116TH
Flight Type:
Survivors:
Yes
Schedule:
Monterrey – Cancún
MSN:
46-8608005
YOM:
1986
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While overflying the Yucatán Province, en route from Monterrey to Cancún, the pilot informed ATC that he was low of fuel and requested the permission to divert to Chichén Itzá Airport for an emergency landing. While approaching the airfield by night, the single engine aircraft descended into trees and crashed few km from the airport. The airplane was destroyed and there was no fire. All five occupants were injured.

Crash of a Beechcraft B200 Super King Air in Unalaska

Date & Time: Feb 14, 2017 at 1323 LT
Operator:
Registration:
N313HS
Survivors:
Yes
MSN:
BB-1300
YOM:
1988
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight, the aircraft belly landed at Unalaska-Tom Madsen Airport runway 13/31. The airplane slid for few dozen metres before coming to rest and was damaged beyond repair. All three occupants evacuated safely.
Probable cause:
There were no investigations about this event. Nevertheless, it was reported that the pilot was distracted and forgot to lower the landing gear on final approach.

Crash of a Cessna 402C in Virgin Gorda

Date & Time: Feb 11, 2017 at 2004 LT
Type of aircraft:
Registration:
N603AB
Survivors:
Yes
Schedule:
Charlotte Amalie – Virgin Gorda
MSN:
402C-0603
YOM:
1982
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5458
Captain / Total hours on type:
809.00
Circumstances:
The aircraft was flying from St Thomas in the US Virgin Islands to Virgin Gorda (VIJ) in the British Virgin Islands. There were eight passengers on board, together with the pilot. It was the pilot’s eleventh flight of the day, and his fourth flight to Virgin Gorda. All these flights were short, with the longest flight being about 40 minutes duration and the shortest just a few minutes. The flight from St Thomas to Virgin Gorda took 35 minutes. The weather in Virgin Gorda was excellent with a light easterly wind and little cloud. The pilot commenced his approach to Virgin Gorda using his usual turning and configuration points. The aircraft touched down normally on runway 03 and the pilot retracted the flaps before applying the brakes. The brakes responded, although the pilot commented that the right brake did not seem to respond as positively as he expected. The pilot reapplied the brakes but the left brake pedal “flopped to the floor”. Judging he had insufficient room to abort the landing, the pilot continued to pump the brakes which he did not consider to be responding. He shut down the engines before the aircraft left the paved surface, struck signage and then a low wall before coming to rest on a bank. The pilot vacated the aircraft through the side window and then opened the main door to allow the passengers to exit the aircraft. None of the occupants was injured. The aircraft was extensively damaged.
Probable cause:
The aircraft landed at Virgin Gorda in conditions (of weight, altitude, temperature and surface condition) where the landing distance required was very close to the landing distance available and without the required safety margin. Hence, when the performance of the brakes was not as expected, probably due to debris in the braking system, the aircraft could not be stopped on the runway. Analysis of the maintenance state of the aircraft involved in this accident indicated that the maintenance capability, processes and planning of its operator were not consistent with the standards expected in conducting international passenger charter services. This appeared also to be the case for the operational procedures and data management.
Final Report:

Crash of a BAe 125-800B in São Paulo

Date & Time: Feb 9, 2017 at 2211 LT
Type of aircraft:
Operator:
Registration:
PT-OTC
Survivors:
Yes
Schedule:
Brasília – São Paulo
MSN:
258194
YOM:
1991
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The airplane departed Brasilía-Presidente Juscelino Kubitschek Airport in the evening on a charter flight to São Paulo-Congonhas, carrying two pilots and one passenger, the Senator Aécio Neves da Cunha. During the takeoff roll, a tire on one of the main landing gear failed. The crew continued the flight, informed ATC about his situation and preferred to divert to São Paulo-Guarulhos Airport that offered longer runway for an emergency landing. After touchdown by night, the aircraft deviated to the right then veered off runway. The left main gear collapsed and the aircraft came to rest in a grassy area. All three occupants evacuated safely and the aircraft was damaged beyond repair.

Crash of a Beechcraft 200T Super King Air in West Palm Beach

Date & Time: Jan 27, 2017 at 1750 LT
Registration:
N60RA
Flight Type:
Survivors:
Yes
Schedule:
Treasure Cay - West Palm Beach
MSN:
BT-7
YOM:
1979
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14414
Captain / Total hours on type:
631.00
Copilot / Total flying hours:
1560
Aircraft flight hours:
15782
Circumstances:
The airline transport pilot reported that, before landing following an uneventful flight, he extended the wing flaps to the approach position and extended the landing gear; the gear indicator lights showed "3 green." After touchdown, he heard noises, and the airplane started to sink. After the airplane came to a stop on the right side of the runway, he noticed that the landing gear handle was up. The pilot stated to the copilot, "How did the gear handle get up?" then placed the handle to the down position and the flight crew exited the airplane. The copilot reported that he was acting as an observer during the flight and that he also saw three green landing gear down-and-locked indicator lights before landing. The airframe sustained substantial damage from contact with the runway. All three landing gear were found in a partially-extended position. Skid marks from all three tires were observed on the runway leading up to the main wreckage. Both propeller assemblies were damaged due to contact with the runway. The pressure vessel was compromised from contact with a propeller blade. The nose landing gear actuator was forced up, into the nose gear well and penetrated the upper nose skin. Examination of the landing gear components did not reveal evidence of a preexisting mechanical malfunction or malfunction. The skid marks leading to the wreckage and the partially-extended gear were inconsistent with the pilot's account that the gear handle was up after the airplane came to rest and was then lowered. The gear handle consisted of an electrical switch that required it to be pulled out of a detent before placing it up or down. There was no mechanical linkage between the gear handle and the landing gear, as the gear were driven by an electric motor. It is likely that the pilot realized that the gear were not extended just before touchdown and then tried to lower the gear, resulting in a touchdown with the gear only partially extended. The pilot reported that he had experienced several interruptions to his sleep the night before the accident. He also reported that he flew 7 legs on the day of the accident for a total of 5.2 hours, only eating a banana for breakfast during this time period. It is likely that the pilot's fatigue contributed to his failure to ensure that the landing gear were down and locked before landing.
Probable cause:
The pilot's failure to ensure that the landing gear were down and locked before touchdown. Contributing to the accident was the pilot's self-reported fatigue at the time of the accident.
Final Report:

Crash of a Beechcraft C90GT King Air off Paraty: 5 killed

Date & Time: Jan 19, 2017 at 1244 LT
Type of aircraft:
Operator:
Registration:
PR-SOM
Survivors:
No
Schedule:
Campo de Marte - Paraty
MSN:
LJ-1809
YOM:
2007
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
7464
Captain / Total hours on type:
2924.00
Circumstances:
The twin engine aircraft departed Campo de Marte Airport at 1301LT bound for Paraty. With a distance of about 200 km, the flight should take half an hour. The approach to Paraty Airport was completed in poor weather conditions with heavy rain falls reducing the visibility to 1,500 metres. While descending to Paraty, the pilot lost visual contact with the airport and initiated a go-around. Few minutes later, while completing a second approach, he lost visual references with the environement then lost control of the aircraft that crashed in the sea near the island of Rasa, about 4 km short of runway 28. Quickly on site, rescuers found a passenger alive but it was impossible to enter the cabin that was submerged. The aircraft quickly sank by a depth of few metres and all five occupants were killed, among them Carlos Alberto, founder of Hotel Emiliano and the Supreme Court Justice Teori Zavascki who had a central role overseeing a massive corruption investigation about the Brazilian oil Group Petrobras.
Probable cause:
Contributing factors:
- Adverse meteorological conditions - a contributor
At the moment of the impact of the aircraft, there was rain with rainfall potential of 25mm/h, covering the Paraty Bay region, and the horizontal visibility was 1,500m. Such horizontal visibility was below the minimum required for VFR landing and take-off operations. Since the SDTK aerodrome allowed only operations under VFR flight rules, the weather conditions proved to be impeding the operation within the required minimum safety limits.
- Decision-making process - a contributor
The weather conditions present in SDTK resulted in visibility restrictions that were impeding flight under VFR rules. In this context, the accomplishment of two attempts to approach and land procedures denoted an inadequate evaluation of the minimum conditions required for the operation at the Aerodrome.
- Disorientation - undetermined
The conditions of low visibility, of low height curve on the water, added to the pilot stress and also to the conditions of the wreckage, which did not show any fault that could have compromised the performance and/or controllability of the aircraft, indicate that the pilot most likely had a spatial disorientation that caused the loss of control of the aircraft.
- Emotional state - undetermined
Through the analysis of voice, speech and language parameters, variations in the emotional state of the pilot were identified that showed evidence of stress in the final moments of the flight. The pilot's high level of anxiety may have influenced his decision to make another attempt of landing even under adverse weather conditions and may have contributed to his disorientation.
- Tasks characteristics - undetermined
The operations in Paraty, RJ, demanded that pilots adapt to the routine of the operators, which was characteristic of the executive aviation. In addition, among operators, possibly because of the lack of minimum operational requirements in SDTK, the pilots who landed even in adverse weather conditions were recognized and valued by the others. Although there were no indications of external pressure on the part of the operator, these characteristics present in the operation in Paraty, RJ, may have favored the pilot's self-imposed pressure, leading him to operate with reduced safety margins.
- Visual illusions - undetermined
The flight conditions faced by the pilot favored the occurrence of the vestibular illusion due to the excess of "G" and the visual illusion of homogeneous terrain. Such illusions probably had, consequently, the pilot's sense that the bank angle was decreasing and that he was at a height above the real. These sensations may have led the pilot to erroneously correct the conditions he was experiencing. Thus, the great bank angle and the downward movement, observed at the moment of the impact of the aircraft, are probably a consequence of the phenomena of illusions.
- Work-group culture - a contributor
Among the members of the pilot group that performed routine flights to the region of Paraty, RJ, there was a culture of recognition and appreciation of those operating under adverse conditions, to the detriment of the requirements established for the VFR operation. These shared values promoted the adherence to informal practices and interfered in the perception and the adequate analysis of the risks present in the operation in SDTK.
Final Report: