Incident Overview

Date: Wednesday 9 November 1966
Aircraft Type: Britten-Norman BN-2A Islander
Owner/operator: Britten-Norman
Registration Number: G-ATCT
Location: 2 km SW of Oudega – ÿ Netherlands
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: Starboard wingStarboard wing
Category: Accident
An Islander prototype aircraft experienced a serious incident during demonstration flights in Germany. Following successful demonstration flights, it was diverted to Eelde due to IMC conditions and pilot reported serious compass trouble. The pilot attempted to ascend to high altitudes to reach clouds, but experienced severe icing and turbulence, leading to loss of control and a catastrophic breakup in a small lake.An Islander prototype aircraft experienced a serious incident during demonstration flights in Germany. Following successful demonstration flights, it was diverted to Eelde due to IMC conditions and pilot reported serious compass trouble. The pilot attempted to ascend to high altitudes to reach clouds, but experienced severe icing and turbulence, leading to loss of control and a catastrophic breakup in a small lake.

Description

The Islander prototype was flown back to England following demonstration flights in Germany. It departed Emden at 11:37 and continued over the Northern part of the Netherlands in VMC at 1500 feet, above the clouds. Weather conditions in the Schiphol Control Zone were IMC so the air traffic controller advised the flight to divert to Eelde. At 12:35 the pilot reported serious compass trouble. He circled the area and began to climb to 6000 feet and later to 8700 feet in an attempt to get on top of the clouds. The airplane continued to climb to about 10.000 feet where it would have encountered severe icing conditions. Control was lost and the airplane broke up in flight. It crashed into the Ringwiel, a small lake near Oudega. PROBABLE CAUSE: “The accident was caused by the failure of the starboard wing, as a result of overstressing during a fast descent. The descent was presumably caused by loss of control under conditions of heavy icing and turbulence, when the aircraft was flown beyond the operating limitations stipulated in its Certificate of Airworthiness.”

Primary Cause

Failure of the starboard wing due to overstressing during a fast descent, exacerbated by heavy icing and turbulence.Failure of the starboard wing due to overstressing during a fast descent, exacerbated by heavy icing and turbulence.

Share on:

Leave a Reply

Your email address will not be published. Required fields are marked *