No fatalities

1999-12-28: Cessna 208A Caravan (C-FGGG) — Seair Seaplanes - Seair Services — Abbotsford, Canada

Abbotsford, CanadaTakeoff (climb)

On December 28, 1999, a Cessna 208A Caravan (registration C-FGGG) operated by Seair Seaplanes - Seair Services was involved in an aviation accident near Abbotsford, Canada during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The pilot took off with frost adhering to the aircraft's lifting surfaces, which increased drag and reduced the ability of the wings to produce lift. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781203828Data APIEditorial standards

A Cessna 208 Caravan crashed shortly after takeoff from Abbotsford Airport when the pilot retracted flaps, leading to a stall. The investigation found frost on wings and overweight conditions.

Accident Details

At 0916 Pacific standard time, a Cessna 208 Caravan amphibious aircraft, serial number 20800310, departed from runway 19 at Abbotsford Airport, British Columbia, on the initial leg of a private flight to the Bahamas. The aircraft carried one pilot and five passengers. About one minute after takeoff, while climbing through approximately 400 feet above ground level, the pilot retracted the flaps from 10 to zero degrees. The aircraft then became uncontrollable, banking left, descending rapidly, and impacting a field approximately half a mile south of the runway threshold. The impact attitude was a left bank with a near-level pitch. The aircraft was destroyed. The pilot sustained serious injuries, two passengers also suffered serious injuries, and three passengers received minor injuries. Daylight visual meteorological conditions prevailed, and there was no post-crash fire.

Probable Cause

The investigation determined the probable cause of the accident was the pilot's decision to take off with frost adhering to the aircraft's lifting surfaces, which increased drag and diminished the wings' lift-generating capability. Additionally, the aircraft was approximately 510 pounds above its maximum takeoff weight at departure, which adversely affected performance. When the flaps were retracted from 10 to zero degrees, the wing's lift production decreased further, resulting in an aerodynamic stall and loss of control.

Other Findings

The investigation noted that appropriate entries were not recorded in the aircraft's journey and maintenance logs, and the weight and balance documentation was not updated. The floats were found to have absorbed much of the impact energy, likely enhancing the survivability of the accident.