No fatalities

1996-09-24: De Havilland DHC-2 Beaver (N67207) — Branch River Air Service — Lake Brooks, United States of America

Lake Brooks, United States of AmericaTakeoff (climb)

On September 24, 1996, a De Havilland DHC-2 Beaver (registration N67207) operated by Branch River Air Service was involved in an aviation accident near Lake Brooks, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: Failure of the pilot to maintain sufficient airspeed during the initial climb after takeoff, which resulted in an inadvertent stall and collision with the terrain (water). Turbulence was a related factor. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781206692Data APIEditorial standards

A pilot and three passengers departed a remote lake in a float-equipped airplane. After takeoff, during a left turn in turbulence, the airplane stalled and the left wing struck the lake surface, causing structural damage.

Accident Summary

A pilot and three passengers were departing a remote lake in a float-equipped airplane. The pilot had positioned the hydraulic actuated flaps to 20 degrees before takeoff. After becoming airborne, at about 150 ft above the water, the pilot moved the flap lever to the 'UP' position in preparation for pumping the flaps up, but stated that he did not move the pump handle. Turbulence was present during the takeoff.

Sequence of Events

While in a left turn, the pilot encountered a severe gust at the moment he positioned the flap lever. The airplane stalled in the left turn, which steepened to almost a 90-degree bank. The airplane descended, and the left wing contacted the surface of the lake. The impact tore the left wing from the fuselage and crushed the floats upward. The right wing flap and right aileron were observed at the accident scene to be extended to an intermediate position.

Weather Conditions

The weather at the time included wind at 20 knots, turbulence, and rain. The pilot expressed concern that the flaps may have retracted without being pumped to the up position.

Post-Accident Examination

An examination of the flap system and the ratchet valve assembly was conducted after the airplane was recovered and the wings were removed. Leakage of hydraulic fluid and air was observed through the ratchet valve. However, additional testing of the ratchet valve at an overhaul facility did not reveal any leakage.

Probable Cause

The official probable cause was stated as: Failure of the pilot to maintain sufficient airspeed during the initial climb after takeoff, which resulted in an inadvertent stall and collision with the terrain (water). Turbulence was a related factor.