Country
Crash of a Beechcraft B200 King Air off Dutch Harbor
Date & Time:
Jan 16, 2020 at 0806 LT
Operator:
Registration:
N547LM
Survivors:
Yes
Schedule:
Dutch Harbor - Adak
MSN:
BB-1642
YOM:
1998
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
756.00
Aircraft flight hours:
7058
Circumstances:
According to the pilot, when the airplane’s airspeed reached about 90 knots during the takeoff roll, he applied back pressure to the control yoke to initiate the takeoff and noted a brief positive rate of climb followed by a sinking sensation. The airspeed rapidly decayed, and the stall warning horn sounded. To correct for the decaying airspeed, he lowered the nose then pulled back on the airplane’s control yoke and leveled the wings just before impacting the ocean. The pilot stated there were no pre accident mechanical malfunctions or anomalies that would have precluded normal operation. Wind about the time of the accident was recorded as 110º downwind of the airplane at 15 knots gusting to 28 knots. The passengers recalled that the pilot’s preflight briefing mentioned the downwind takeoff but included no discussion of the potential effect of the wind conditions on the takeoff. The airplane’s estimated gross weight at the time of the accident was about 769.6 pounds over its approved maximum gross weight, and the airplane’s estimated center of gravity was about 8.24 inches beyond the approved aft limit at its maximum gross weight. It is likely that the pilot’s decision to takeoff downwind and operate the airplane over the maximum gross weight with an aft center of gravity led to the aerodynamic stall during takeoff and loss of control. Downwind takeoffs result in higher groundspeeds and increase takeoff distance. While excessive aircraft weight increases the takeoff distance and stability, and an aft center of gravity decreases controllability. Several instances of the operator’s noncompliance with its operational procedures and risk mitigations were discovered during the investigation, including two overweight flights, inaccurate and missing information on aircraft flight logs, and the accident pilot’s failure to complete a flight risk assessment for the accident flight. The operator had a safety management system (SMS) in place at the time of the accident that required active monitoring of its systems and processes to ensure compliance with internal and external requirements. However, the discrepancies noted with several flights, including the accident flight, indicate that the operator’s SMS program was inadequate to actively monitor, identify, and mitigate hazards and deficiencies.
Probable cause:
The pilot’s improper decision to takeoff downwind and to load the airplane beyond its allowable gross weight and center of gravity limits, which resulted in an aerodynamic stall and loss of control. Contributing to the accident was the inadequacy of the operator’s safety management system to actively monitor, identify, and mitigate hazards and deficiencies.
Final Report:
Ground accident of a Beechcraft 200 Super King Air in Fresno
Date & Time:
Dec 18, 2019 at 0730 LT
Registration:
N72MM
Survivors:
Yes
MSN:
BB-497
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
9838
Circumstances:
Parked at Fresno-Yosemite Airport, the twin engine airplane was stolen by a teenager aged 17. She lost control of the airplane that collided with a fence and a building. The only occupant was uninjured and arrested. The aircraft was damaged beyond repair.
Probable cause:
No investigations were conducted by the NTSB on this event.
Crash of a Beechcraft 200 King Air in Saint Jean
Date & Time:
Nov 23, 2019
Operator:
Registration:
XB-PYB
Survivors:
Yes
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft crashed in unknown circumstances in a pasture located near Saint Jean, Haiti. There were no casualties while the aircraft was damaged beyond repair. It was engaged in an illegal flight (contraband) and the registration XB-PYB is false. Local authorities were looking for both Mexican pilots and a local involved in the illegal mission.
Crash of a Beechcraft 200 Super King Air in Palajuyú
Date & Time:
Oct 25, 2019
Operator:
Survivors:
Yes
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing an illegal flight between Venezuela and Honduras. En route, the airplane was traced by Honduran and Guatemalan Authorities and the crew eventually completed a belly landing in Palajuyú, in the region of Sipacate, Guatemala. Law enforcement officers were fired upon arrival and the occupants left the crash site and were not found. The aircraft was destroyed. An important load of contraband was found on board.
Crash of a Beechcraft B200 Super King Air in Gillam
Date & Time:
Apr 24, 2019 at 1823 LT
Operator:
Registration:
C-FRMV
Survivors:
Yes
Schedule:
Winnipeg – Churchill – Rankin Inlet
MSN:
BB-979
YOM:
1982
Flight number:
KEW202
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total hours on type:
1100.00
Copilot / Total hours on type:
1350
Circumstances:
On 24 April 2019, the Keewatin Air LP Beechcraft B200 aircraft (registration C‑FRMV, serial number BB979), equipped to perform medical evacuation flights, was conducting an instrument flight rules positioning flight (flight KEW202), with 2 flight crew members and 2 flight nurses on board, from Winnipeg/James Armstrong Richardson International Airport, Manitoba, to Rankin Inlet Airport, Nunavut, with a stop at Churchill Airport, Manitoba. At 1814 Central Daylight Time, when the aircraft was cruising at flight level 250, the flight crew declared an emergency due to a fuel issue. The flight crew diverted to Gillam Airport, Manitoba, and initiated an emergency descent. During the descent, both engines flamed out. The flight crew attempted a forced landing on Runway 23, but the aircraft touched down on the frozen surface of Stephens Lake, 750 feet before the threshold of Runway 23. The landing gear was fully extended. The aircraft struck the rocky lake shore and travelled up the bank toward the runway area. It came to rest 190 feet before the threshold of Runway 23 at 1823:45 Central Daylight Time. None of the occupants was injured. The aircraft sustained substantial damage. The 406 MHz emergency locator transmitter activated. Emergency services responded. There was no fire.
Probable cause:
Findings as to causes and contributing factors:
These are conditions, acts or safety deficiencies that were found to have caused or contributed to this occurrence.
1. When the captain asked if the aircraft was ready for the flight, the first officer replied that it was, not recalling that the aircraft required fuel.
2. While performing the FUEL QUANTITY item on the AFTER START checklist, the captain responded to the first officer’s prompt with the rote response that the fuel was sufficient, without looking at the fuel gauges.
3. The aircraft departed Winnipeg/James Armstrong Richardson International Airport with insufficient fuel on board to complete the planned flight.
4. The flight crew did not detect that there was insufficient fuel because the gauges had not been included in the periodic cockpit scans.
5. When the flight crew performed the progressive fuel calculation, they did not confirm the results against the fuel gauges, and therefore their attention was not drawn to the low-fuel state at a point that would have allowed for a safe landing.
6. Still feeling the effect of the startle response to the fuel emergency, the captain quickly became task saturated, which led to an uncoordinated response by the flight crew, delaying the turn toward Gillam Airport, and extending the approach.
7. The right engine lost power due to fuel exhaustion when the aircraft was 1 nautical mile from Runway 23. From that position, a successful forced landing on the intended runway was no longer possible and, as a result, the aircraft touched down on the ice surface of Stephens Lake, short of the runway.
Findings as to risk:
These are conditions, unsafe acts or safety deficiencies that were found not to be a factor in this occurrence but could have adverse consequences in future occurrences.
1. If procedures are not developed to instruct pilots on their roles and responsibilities during line indoctrination flights, there is a risk that flight crew members may not participate when expected, or may work independently towards different goals.
Other findings:
These items could enhance safety, resolve an issue of controversy, or provide a data point for future safety studies.
1. Because emergency medical services and the fire department were not notified immediately about the declared emergency, they were not on site before the aircraft arrived at Gillam Airport.
These are conditions, acts or safety deficiencies that were found to have caused or contributed to this occurrence.
1. When the captain asked if the aircraft was ready for the flight, the first officer replied that it was, not recalling that the aircraft required fuel.
2. While performing the FUEL QUANTITY item on the AFTER START checklist, the captain responded to the first officer’s prompt with the rote response that the fuel was sufficient, without looking at the fuel gauges.
3. The aircraft departed Winnipeg/James Armstrong Richardson International Airport with insufficient fuel on board to complete the planned flight.
4. The flight crew did not detect that there was insufficient fuel because the gauges had not been included in the periodic cockpit scans.
5. When the flight crew performed the progressive fuel calculation, they did not confirm the results against the fuel gauges, and therefore their attention was not drawn to the low-fuel state at a point that would have allowed for a safe landing.
6. Still feeling the effect of the startle response to the fuel emergency, the captain quickly became task saturated, which led to an uncoordinated response by the flight crew, delaying the turn toward Gillam Airport, and extending the approach.
7. The right engine lost power due to fuel exhaustion when the aircraft was 1 nautical mile from Runway 23. From that position, a successful forced landing on the intended runway was no longer possible and, as a result, the aircraft touched down on the ice surface of Stephens Lake, short of the runway.
Findings as to risk:
These are conditions, unsafe acts or safety deficiencies that were found not to be a factor in this occurrence but could have adverse consequences in future occurrences.
1. If procedures are not developed to instruct pilots on their roles and responsibilities during line indoctrination flights, there is a risk that flight crew members may not participate when expected, or may work independently towards different goals.
Other findings:
These items could enhance safety, resolve an issue of controversy, or provide a data point for future safety studies.
1. Because emergency medical services and the fire department were not notified immediately about the declared emergency, they were not on site before the aircraft arrived at Gillam Airport.
Final Report:
