Casualties unknown

2018-09-01: ANTONOV, An-2 (SP-AOO) — Pilot samolotowy zawodowy — Cambrai-Niergnies (LFYG) / Francja, PL

Cambrai-Niergnies (LFYG) / Francja, PL

On September 1, 2018, an ANTONOV, An-2 (registration SP-AOO) operated by Pilot samolotowy zawodowy was involved in an aviation accident near Cambrai-Niergnies (LFYG) / Francja, PL. Investigators recorded the probable cause as: Pilot error - excessive use of wheel brakes. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Polish State Commission on Aircraft Accidents Investigation (PKBWL)Primary reportUpdated 1785092869Data APIEditorial standards

An An-2TD, registration SP-AOO, experienced a landing incident at Cambrai-Niergnies airport, France. After touchdown, excessive braking caused the aircraft to pitch forward, resulting in propeller and wingtip damage. No injuries were reported.

Incident Overview

On 1 September 2018 at 16:54 UTC, an Antonov An-2TD aircraft, registered SP-AOO, was conducting a landing approach at Cambrai-Niergnies Airport (LFYG) in France. The aircraft was operated by a private owner and was crewed by two professional pilots (citizens of Luxembourg) and one passenger.

Sequence of Events

The aircraft approached runway 08 with a configuration of 120 km/h and flaps set to 20°. Weather conditions were clear skies with wind approximately 6 knots from 060°. Touchdown occurred at 16:57 UTC at a speed of 85 km/h, approximately 100 meters past the western runway threshold. After landing, the aircraft began to drift left of the centerline, which the pilot corrected. Approximately 140–150 meters from the touchdown point, while on three wheels, the pilot initiated braking. The aircraft then pitched forward sharply, momentarily reaching an almost vertical attitude while also rolling to the left. This caused the lower left and upper left wingtips and the propeller to make violent contact with the runway surface, stopping the engine and damaging the propeller and airframe. The aircraft came to rest supported on the bent propeller with the rear fuselage elevated at an angle. The crew and passenger evacuated normally through the cabin door.

Damage

Examination of the runway revealed skid marks from the main landing gear wheels approximately 16–20 meters long and propeller blade impact marks over a distance of about 3.5 meters. Aircraft damage included a destroyed propeller, damaged leading edges of the left lower and left upper wingtips, and an engine requiring inspection after abrupt stoppage. No other damage or fluid leaks were found.

Probable Cause

The investigation determined the probable cause of the incident to be pilot error consisting of excessive use of the wheel brakes. Contributing factors included the aircraft's design with a high center of gravity, the low mass of the aircraft (only two crew and one passenger on board), and the pilot's limited experience on this type of aircraft.

Aftermath

The pilot notified the Bureau d'Enquêtes et d'Analyses pour la Sécurité de l'Aviation civile (BEA) and the aircraft owner, who then informed the Polish State Commission on Aircraft Accident Investigation (PKBWL). The BEA decided not to investigate. The PKBWL conducted a correspondence-based inquiry with the pilot, whose explanations were used in the final report. No safety recommendations were issued.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2018-2935/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.