Incident Overview

Date: Wednesday 29 November 2006
Aircraft Type: Grob G.180A SPn
Owner/operator: Grob Aerospace
Registration Number: D-CGSP
Location: 1,4 km ESE of Mindelheim-Mattsies Airport – ÿ Germany
Phase of Flight: Manoeuvring (airshow, firefighting, ag.ops.)
Status: Destroyed, written off
Casualties: Fatalities: 1 / Occupants: 1
Component Affected: Control surfaces of the Grob SPn business jet prototype.Control surfaces of the Grob SPn business jet prototype.
Investigating Agency: BFUBFU
Category: Accident
A Grob SPn business jet prototype was destroyed in an accident near Mindelheim-Mattsies Airport, Germany, on November 29, 2006. Chief test pilot Gerard Guillaumaud was killed. The aircraft conducted a 60-minute test flight from the factory airfield, including maneuvers and system tests, and landed at 11:40. The pilot executed a right-hand circuit in and out of clouds, and lost control, impacting a field. The probable speed was between 240 and 270 knots, below the maximum allowed flutter speed of 297 knots. The design change was related to anti-icing requirements and increased roll authority.A Grob SPn business jet prototype was destroyed in an accident near Mindelheim-Mattsies Airport, Germany, on November 29, 2006. Chief test pilot Gerard Guillaumaud was killed. The aircraft conducted a 60-minute test flight from the factory airfield, including maneuvers and system tests, and landed at 11:40. The pilot executed a right-hand circuit in and out of clouds, and lost control, impacting a field. The probable speed was between 240 and 270 knots, below the maximum allowed flutter speed of 297 knots. The design change was related to anti-icing requirements and increased roll authority.

Description

The second prototype of the Grob SPn business jet was destroyed in an accident near Mindelheim-Mattsies Airport, Germany. Chief test pilot Gerard Guillaumaud was killed in the accident. On the day of the accident, November 29, 2006, the airplane had conducted a 60-minute test flight from the factory airfield of manufacturer, Mindelheim-Mattsies Airport. Various flight maneuvers and system tests were completed and the airplane landed at 11:40. The aircraft was parked on the apron and prepared for the next flight. This flight would be a demonstration flight for a group of visitors with several fly-bys. The jet took off from runway 33 at 13:12 and the pilot flew a right hand circuit in and out of clouds. As it was lining up for a fly-by parts from the stabilizer separated. The pilot lost control and the airplane impacted a field. Given the weather circumstances, the flight should have been conducted using Reduced Flight Display specifications. These included a maximum speed of 200 knots. The probable speed of the accident airplane was between 240 and 270 knots. This speed was below the maximum allowed speed for flutter tests, 297 kts. The manufacturer had changed the design of the control surfaces on this second prototype due to anti-icing requirements and to provide more roll authority. PROBABLE CAUSE: The accident occurred because there was an in-flight separation of the tailplane due to flutter and the plane subsequently was no longer controllable. The circumstances that led to the flutter could not be determined clearly due to lack of flight data and limited investigation.

Primary Cause

In-flight tailplane separation due to flutter.In-flight tailplane separation due to flutter.

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