Crash of a Cessna 208B Grand Caravan near Guaymaral: 8 killed

Date & Time: May 1, 2017 at 1630 LT
Type of aircraft:
Operator:
Registration:
EJC-1130
Flight Type:
Survivors:
No
Site:
Schedule:
Tolemaida - Bogotá
MSN:
208B-1194
YOM:
2006
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The single engine aircraft was performing a short flight from Tolemaida AFB to Guaymaral Airport in Bogotá. While approaching the airport from the west, the crew encountered limited visibility due to marginal weather conditions when the aircraft impacted trees and crashed on the slope of Cerro Manjui, about 5 km west of the airport. The aircraft was destroyed and all 8 occupants were killed, among them three civilians.

Crash of a Cessna 208B Grand Caravan near Chignik: 1 killed

Date & Time: May 1, 2017 at 1350 LT
Type of aircraft:
Operator:
Registration:
N803TH
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Port Heiden - Perryville
MSN:
208B-0321
YOM:
1992
Flight number:
GV341
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4989
Captain / Total hours on type:
904.00
Aircraft flight hours:
17990
Circumstances:
The airline transport pilot was conducting a commercial visual flight rules (VFR) flight. A passenger who was on the first segment stated that the pilot flew the airplane lower than usual for that route, and that the airplane flew through clouds during the flight. The passenger disembarked and the pilot departed on the second segment of the flight with a load of mail. The route included flight across a peninsula of mountainous terrain to a remote coastal airport that lacked official weather reporting or instrument approach procedures. About 28 minutes after departure, an emergency locator transmitter (ELT) signal from the airplane was received and a search and rescue operation was initiated. The wreckage was located about 24 miles from the destination in deep snow on the side of a steep, featureless mountain at an elevation about 3,000 ft mean sea level. The accident site displayed signatures consistent with impact during a left turn. Examination of the airplane revealed no evidence of mechanical malfunctions or anomalies that would have precluded normal operation. The airplane was not equipped with any recording or flight tracking devices, nor was it required to be; therefore, the airplane's flight track before the accident could not be determined. The airplane was certified for instrument flight and flight in icing conditions and was equipped with a terrain avoidance warning system (TAWS) which was not inhibited during the accident. Although the TAWS should have provided the pilot with alerts as the airplane neared the terrain, it could not be determined if this occurred or if the pilot heeded the alerts. A review of nearby weather camera images revealed complete mountain obscuration conditions with likely rain shower activity in the vicinity of the accident site. Visible and infrared satellite imagery indicated overcast cloud cover over the accident site at the time of the accident. The graphical forecast products that were available to the pilot before the flight indicated marginal VFR conditions for the entire route. There was no evidence that the pilot obtained an official weather briefing, and what weather information he may have accessed before the flight could not be determined. Additionally, the cloud conditions and snow-covered terrain present in the area likely resulted in flat light conditions, which would have hindered the pilot's ability to perceive terrain features and closure rates. Based on the weather camera, surface, and upper air observations, it is likely that the pilot encountered instrument meteorological conditions inflight, after which he performed a left turn to return to visual meteorological conditions and did not recognize his proximity to the mountain due to the flat light conditions. The pilot and the dispatch agent signed a company flight risk assessment form before the flight, which showed that the weather conditions for the flight were within the company's acceptable risk parameters. Although the village agents at the departure and destination airports stated that the weather at those coastal locations was good, the weather assessment for the accident flight was based on hours-old observations provided by a village agent who was not trained in weather observation and did not include en route weather information, the area forecast, or the AIRMET for mountain obscuration effective during the dispatch time and at the time of the accident. Since acquiring the accident route from another operator years earlier, the company had not performed a risk assessment of the route and its associated hazards. Multiple company pilots described the accident route of flight as hazardous and considered it an undesirable route due to the terrain, rapidly changing weather, and lack of weather reporting infrastructure; however, the company did not address or attempt to mitigate these known hazards through its risk assessment processes. The company's controlled-flight-into-terrain (CFIT)-avoidance program stated that each pilot shall have one classroom training session and one CFIT-avoidance training session in an aviation training device (ATD) each year; however, the pilot's training records indicated that his most recent ATD session was 15 months prior. More recent CFIT avoidance training may have resulted in the pilot recognizing and responding to the reduced visibility and flat light conditions sooner.
Probable cause:
The pilot's continued visual flight rules flight into an area of mountainous terrain and instrument meteorological conditions, which resulted in controlled flight into terrain (CFIT). Contributing to the accident was the company's failure to provide the pilot with CFIT-avoidance recurrent simulator training as required by their CFIT avoidance program and the company's inadequate flight risk assessment processes, which did not account for the known weather hazards relevant to the accident route of flight.
Final Report:

Crash of a Cessna 208B Grand Caravan near Togiak: 3 killed

Date & Time: Oct 2, 2016 at 1157 LT
Type of aircraft:
Operator:
Registration:
N208SD
Flight Phase:
Survivors:
No
Site:
Schedule:
Quinhagak – Togiak
MSN:
208B-0491
YOM:
1995
Flight number:
HAG3153
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
6481
Captain / Total hours on type:
781.00
Copilot / Total flying hours:
273
Copilot / Total hours on type:
84
Aircraft flight hours:
20562
Circumstances:
On October 2, 2016, about 1157 Alaska daylight time, Ravn Connect flight 3153, a turbine powered Cessna 208B Grand Caravan airplane, N208SD, collided with steep, mountainous terrain about 10 nautical miles northwest of Togiak Airport (PATG), Togiak, Alaska. The two commercial pilots and the passenger were killed, and the airplane was destroyed. The scheduled commuter flight was operated under visual flight rules by Hageland Aviation Services, Inc., Anchorage, Alaska, under the provisions of Title 14 Code of Federal Regulations Part 135. Visual meteorological conditions prevailed at PATG (which had the closest weather observing station to the accident site), but a second company flight crew (whose flight departed about 2 minutes after the accident airplane and initially followed a similar route) reported that they observed unexpected fog, changing clouds, and the potential for rain along the accident route. Company flight-following procedures were in effect. The flight departed Quinhagak Airport, Quinhagak, Alaska, about 1133 and was en route to PATG.
Probable cause:
The flight crew's decision to continue the visual flight rules flight into deteriorating visibility and their failure to perform an immediate escape maneuver after entry into instrument meteorological conditions, which resulted in controlled flight into terrain (CFIT). Contributing to the accident were:
- Hageland's allowance of routine use of the terrain inhibit switch for inhibiting the terrain awareness and warning system alerts and inadequate guidance for uninhibiting the alerts, which reduced the margin of safety, particularly in deteriorating visibility;
- Hageland's inadequate crew resource management (CRM) training;
- The Federal Aviation Administration's failure to ensure that Hageland's approved CRM training contained all the required elements of Title 14 Code of Federal Regulations 135.330;
- Hageland's CFIT avoidance ground training, which was not tailored to the company's operations and did not address current CFIT-avoidance technologies.
Final Report:

Crash of a Cessna 208B Grand Caravan in San Antonio de Prado: 4 killed

Date & Time: Sep 30, 2016 at 1204 LT
Type of aircraft:
Registration:
HK-3804
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Medellín – Juradó
MSN:
208B-0315
YOM:
1992
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3534
Captain / Total hours on type:
335.00
Copilot / Total flying hours:
6378
Copilot / Total hours on type:
1245
Aircraft flight hours:
2867
Circumstances:
The single engine aircraft departed Medellín-Enrique Olaya Herrera Airport on a charter flight to Juradó, carrying nine passengers and two pilots. Shortly after takeoff, the crew encountered difficulties to gain sufficient altitude and apparently attempted an emergency landing when the aircraft impacted a hill and eventually crashed into trees. The copilot and three passengers were killed and seven others occupants were injured, some seriously. The aircraft was destroyed.
Probable cause:
The following findings were identified:
- Execution of a take-off with a weight approximately 17% higher than the maximum gross operating weight (MTOW) established for the C208B aircraft.
- Limited climb rate with signs of lift loss due to the low performance given by the overweight during the initial climb phase.
- Forced landing in mountainous terrain due to loss of lift caused by overweight during the initial climb.
- Absence in the identification of the risks associated to an overweight operation of the aircraft.
- Lack of supervision by the Aircraft Operator in relation to the dispatch of aircraft operating from the outside at the main base of operation.
Final Report:

Crash of a Cessna 208B Grand Caravan in Russian Mission: 3 killed

Date & Time: Aug 31, 2016 at 1001 LT
Type of aircraft:
Operator:
Registration:
N752RV
Flight Phase:
Survivors:
No
Schedule:
Russian Mission – Marshall
MSN:
208B-5088
YOM:
2014
Flight number:
HAG3190
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
18810
Captain / Total hours on type:
12808.00
Aircraft flight hours:
3559
Circumstances:
The Cessna had departed about 3 minutes prior on a scheduled passenger flight and the Piper was en route to a remote hunting camp when the two airplanes collided at an altitude about 1,760 ft mean sea level over a remote area in day, visual meteorological conditions. The airline transport pilot and two passengers onboard the Cessna and the commercial pilot and the passenger onboard the Piper were fatally injured; both airplanes were destroyed. Post accident examination revealed signatures consistent with the Cessna's outboard left wing initially impacting the Piper's right wing forward strut while in level cruise flight. Examination revealed no mechanical malfunctions or anomalies that would have precluded normal operation of either airplane. Neither pilot was in communication with an air traffic control facility and they were not required to be. A performance and visibility study indicated that each airplane would have remained a relatively small, slow-moving object in the other pilot's window (their fuselages spanning less than 0.5° of the field of view, equivalent to the diameter of a penny viewed from about 7 ft away) until about 10 seconds before the collision, at which time it would have appeared to grow in size suddenly (the "blossom" effect). From about 2 minutes before the collision, neither airplane would have been obscured from the other airplane pilot's (nominal) field of view by cockpit structure, although the Cessna would have appeared close to the bottom of the Piper's right wing and near the forward edge of its forward wing strut. The Cessna was Automatic Dependent Surveillance-Broadcast (ADS-B) Out equipped; the Piper was not ADS-B equipped, and neither airplane was equipped with any cockpit display of traffic information (CDTI). CDTI data would have presented visual information regarding the potential conflict to both pilots beginning about 2 minutes 39 seconds and auditory information beginning about 39 seconds before the collision, providing adequate time for the pilots to react. The see-and-avoid concept requires a pilot to look through the cockpit windows, identify other aircraft, decide if any aircraft are collision threats, and, if necessary, take the appropriate action to avert a collision. There are inherent limitations of this concept, including limitations of the human visual and information processing systems, pilot tasks that compete with the requirement to scan for traffic, the limited field of view from the cockpit, and environmental factors that could diminish the visibility of other aircraft. Given the remote area in which the airplanes were operating, it is likely that the pilots had relaxed their vigilance in looking for traffic. The circumstances of this accident underscore the difficultly in seeing airborne traffic by pilots; the foundation of the "see and avoid" concept in VMC, even when the cockpit visibility offers opportunities to do so, and particularly when the pilots have no warning of traffic in the vicinity. Due to the level of trauma sustained to the Cessna pilot, the autopsy was inconclusive for the presence of natural disease. It was undetermined if natural disease could have presented a significant hazard to flight safety.
Probable cause:
The failure of both pilots to see and avoid each other while in level cruise flight, which resulted in a midair collision.
Final Report: