Casualties unknown

2018-07-29: DR 400/180 (DR-400) — letališča Bovec – LJBO, SI

letališča Bovec – LJBO, SI

On July 29, 2018, a DR 400/180 (registration DR-400) was involved in an aviation accident near letališča Bovec – LJBO, SI. Investigators recorded the probable cause as: The pilot, while performing aerotow of a glider with the DR 400/180, D-EFTW, due to improper handling of the aircraft, entered a stall/spin situation from which he could not recover. This summary draws on records from the Slovenian aircraft accident investigation service, Ministry of Infrastructure (MzI).

Sourcesthe Slovenian aircraft accident investigation service, Ministry of Infrastructure (MzI)Primary reportUpdated 1785671746Data APIEditorial standards

Final report on the accident of Robin DR400/180 D-EFTW near Bovec airfield on 29 July 2018. The aircraft was destroyed during an aerotow. Probable cause: pilot's improper handling resulting in an unrecoverable stall/spin.

Introduction

The Slovenian Ministry of Infrastructure, Service for Investigation of Aviation, Maritime and Railway Accidents and Incidents, has published its final report on the accident of a Pierre Robin DR400/180, registration D-EFTW, which occurred near Bovec airfield (LJBO) on 29 July 2018.

Factual Information

The accident happened while the aircraft was performing an aerotow of a glider. The aircraft was completely destroyed. The pilot was the sole occupant. The fuel selector valve was found in the OFF position. The tow rope had separated; subsequent analysis of the rope was conducted by the Slovenian National Building and Civil Engineering Institute (ZAG). The propeller sustained damage consistent with a non-powered impact. Meteorological data from the airfield were recorded, including wind, temperature, and pressure.

Analysis

The investigation examined the tow rope failure, the fuel selector position, fuel usage, and propeller damage. The tow rope was found to have a reduced breaking strength due to abrasion at the point of failure. The fuel selector valve was in the OFF position, but engine operation at impact was inferred from propeller damage patterns. The pilot's handling during the aerotow was assessed; the aircraft entered a stall/spin from which recovery was not possible. The fuel quantity indicators and the emergency electric fuel pump were also evaluated.

Conclusions

The investigation determined that the direct cause of the accident was the pilot's improper handling of the aircraft during the aerotow, leading to an unrecoverable stall/spin. Indirect causes included factors such as the fuel selector position and the condition of the tow rope, but these were not cited as primary causes.

Probable Cause

The pilot, while performing aerotow of a glider with the DR 400/180, D-EFTW, due to improper handling of the aircraft, entered a stall/spin situation from which he could not recover.