3 fatalities

2019-10-26: De Havilland DHC-3 Otter (C-GBTU) — Blue Water Aviation - Manitoba Air Charter Services — Little Grand Rapids, Canada

Little Grand Rapids, CanadaLanding (descent or approach)

On October 26, 2019, a De Havilland DHC-3 Otter (registration C-GBTU) operated by Blue Water Aviation - Manitoba Air Charter Services was involved in an aviation accident near Little Grand Rapids, Canada during landing or approach. 3 people were killed. Investigators recorded the probable cause as: A fatigue fracture originated in the bolt hole bore of the right-hand wing lift strut's upper outboard lug plate, eventually leading to an overstress fracture of the right-hand wing lift strut's upper outboard and inboard lug plates during the left turn prior… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781190701Data APIEditorial standards

On October 26, 2019, a DHC-3 Otter on approach to Family Lake suffered right wing separation. The pilot and two passengers sustained fatal injuries, and the aircraft was destroyed.

Accident Details

On October 26, 2019, at approximately 0745 Central Daylight Time, a float-equipped de Havilland DHC-3 Otter (registration C‑GBTU, serial number 209) operated by Blue Water Aviation departed Bissett Water Aerodrome, Manitoba. On board were the pilot, two passengers, and approximately 800 pounds of freight. The intended destination was Little Grand Rapids, Manitoba, located on the eastern shore of Family Lake.

At approximately 0845, while on approach to Family Lake, the aircraft’s right wing separated from the fuselage. The aircraft subsequently entered a nose‑down attitude and struck the water surface. The pilot and the two passengers sustained fatal injuries. The aircraft was destroyed by impact forces. The emergency locator transmitter activated momentarily.

Investigation Findings

The official investigation determined that a fatigue fracture originated in the bolt hole bore of the right‑hand wing lift strut’s upper outboard lug plate. This fatigue crack eventually caused an overstress fracture of both the right‑hand wing lift strut’s upper outboard and inboard lug plates during the left turn prior to the final approach. The failure of these lug plates led to the separation of the right‑hand wing lift strut from the wing, and subsequently, the separation of the right wing from the aircraft.

Additional Observations

The investigation also noted that when operational flight plan data and load calculations are not available, there is a risk that important aircraft information—including the number of occupants, route, cargo, and weight‑and‑balance details—will not be accessible for search‑and‑rescue operations or accident investigation. Furthermore, the detailed visual inspection prescribed in the Viking Air Ltd. Supplementary Inspection and Corrosion Control Manual, and required by Airworthiness Directive CF2018‑4, did not identify cracks that could form in the right‑hand wing strut’s upper outboard lug plate.

Probable cause

A fatigue fracture originated in the bolt hole bore of the right-hand wing lift strut's upper outboard lug plate, eventually leading to an overstress fracture of the right-hand wing lift strut's upper outboard and inboard lug plates during the left turn prior to final approach. The failure of these lug plates caused the separation of the right-hand wing lift strut from the wing and subsequently the separation of the right wing from the aircraft.