Incident Overview

Date: Friday 26 March 1982
Aircraft Type: Dornier 228-100
Owner/operator: Dornier Luftfahrt GmbH
Registration Number: D-IFNS
Location: near Igenhausen – ÿ Germany
Phase of Flight: Manoeuvring (airshow, firefighting, ag.ops.)
Status: Destroyed, written off
Casualties: Fatalities: 3 / Occupants: 3
Component Affected: Aircraft’s pitch trim actuator clutch and stabilizer control system.Aircraft’s pitch trim actuator clutch and stabilizer control system.
Category: Accident
A Dornier 228-100 prototype crashed during a test flight, resulting in the deaths of all three crew members ? a Dornier test pilot and two U.K. CAA pilots. The flight occurred from Oberpfaffenhofen Airport (OBF) at 17:27, and the aircraft was trimmed into a full nose-down position to simulate a horizontal stabilizer trim-runaway. Due to excessive stick forces, both pilots were unable to maintain pitch control, preventing a retrim. The aircraft disintegrated in a nose-down attitude approximately 1200 feet above ground level. The pilot assisted the other pilot, but their joint strength was insufficient to recover the aircraft.A Dornier 228-100 prototype crashed during a test flight, resulting in the deaths of all three crew members ? a Dornier test pilot and two U.K. CAA pilots. The flight occurred from Oberpfaffenhofen Airport (OBF) at 17:27, and the aircraft was trimmed into a full nose-down position to simulate a horizontal stabilizer trim-runaway. Due to excessive stick forces, both pilots were unable to maintain pitch control, preventing a retrim. The aircraft disintegrated in a nose-down attitude approximately 1200 feet above ground level. The pilot assisted the other pilot, but their joint strength was insufficient to recover the aircraft.

Description

The Dornier 228-100 prototype, registration D-IFNS, was destroyed when it crashed during a test flight. All three crew members, a Dornier test pilot and two U.K. CAA pilots were killed in the accident. The flight was part of the UK Civil Aviation Authority’s certification programme for the type. It took off from Oberpfaffenhofen Airport (OBF) at 17:27. During the flight the aircraft was trimmed into a full nose down position to simulate a horizontal stabilizer trim-runaway. Both pilots were unable to maintain pitch control due to the excessive stick forces. For unknown reasons a retrim could not be initiated. The aircraft disintegrated in a nose down attitude about 1200 ft agl. Stick forces in excess of 50 deca-newton were pulled to counteract the mistrimmed condition. this disengaged the pitch trim actuator clutch preventing any stabilizer movement in nose-up retrim attempts. The pilot may have been distracted by the need to communicate with the telemetry station. On becoming aware of the critical flight situation he assisted the other pilot on the controls, but by this stage their joint strength was insufficient to effect recovery.

Primary Cause

Excessive stick forces during a trim-runaway maneuver caused by the aircraft’s instability.Excessive stick forces during a trim-runaway maneuver caused by the aircraft’s instability.

Share on:

Leave a Reply

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