No fatalities

Float-Equipped Airplane Sustains Wing Damage After Wind Gust During Landing

Ketchikan, AK, United States

On June 1, 2018, a DEHAVILLAND BEAVER DHC 2 I operated by RDM PILOT/GUIDE LTD was involved in an aviation accident near Ketchikan, AK. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain pitch and directional control during a water landing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1785761257Data APIEditorial standards

A float-equipped airplane encountered a strong wind gust after touchdown, causing the right float struts to collapse and both wings to impact the water, resulting in substantial damage.

Landing Sequence

The pilot of a float-equipped airplane reported that during approach to an ocean bay, the aircraft encountered very light turbulence. The touchdown was normal, but seconds later the pilot felt a strong wind on the tail from the left, which lifted the tail of the airplane. As a result, the front of the right float submerged. The pilot immediately pulled back and left on the controls, but there was no response.

Subsequent Events

Following the lack of control response, the right float struts collapsed and the right wing impacted the water. The airplane then spun approximately 90° to 120° to the right, and the left wing impacted the water. The airplane came to rest upright on the floats.

Damage

The airplane sustained substantial damage to both wings.

Mechanical Status

The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Weather Conditions

An automated weather observation system located about 20 nautical miles from the accident site reported that around the time of the accident, the wind was from 160° at 9 knots. The pilot had landed to the south.

Contributing factors

Causes

Pitch control — Not attained/maintainedDirectional control — Not attained/maintainedPilot

Other contributing factors

Response/compensationEffect on operation