Casualties unknown

2015-08-06: Diamond DA40 NG — Lądowisko Żerniki, PL

Lądowisko Żerniki, PL

On August 6, 2015, a Diamond DA40 NG was involved in an aviation accident near Lądowisko Żerniki, PL. Investigators recorded the probable cause as: Error in planning the approach to landing in conditions of weak variable wind, resulting in touchdown with a 300 m float. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL).

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

On 6 August 2015, a Diamond DA40NG touched down with a 300 m float on a 618 m runway at Żerniki, overran by 10 m, causing nose gear and propeller damage. The cause was an approach planning error in weak variable wind.

Incident Overview

On 6 August 2015, a Diamond DA40NG aircraft landed on runway 06 (DS 06) at the Żerniki airstrip. The aircraft touched down with a float of approximately 300 m, which placed the touchdown point at around the midpoint of the runway. Despite immediate braking, the landing roll ended 10 m beyond the end of the runway. The overrun resulted in a fracture of the nose gear leg and damage to the propeller. After touchdown, the pilot retracted the flaps to increase braking effectiveness.

Occupants and Injuries

The aircraft was occupied by four persons. All four sustained no injuries.

Cause and Contributing Factors

The cause of the incident was an error in planning the approach to landing under conditions of weak, variable wind, which led to a touchdown with a 300 m float.

Contributing factors included:

  • An approach speed of 85 kt instead of the recommended 77 kt. According to the Aircraft Flight Manual (AFM), higher approach speeds result in significantly longer landing distance during the flare.
  • High density altitude of 817 m (actual airstrip elevation is 82 m) due to a high ambient temperature of 35 °C.
  • Landing with a mass close to the maximum takeoff weight (MTOW) on a 618 m long runway. The AFM specifies that the landing distance from a 15 m obstacle with MTOW under standard conditions is 639 m, with a landing roll of 310 m.

Damage

The incident resulted in structural damage: the nose gear leg was broken and the propeller was damaged.

Preventive Measures and Recommendations

No preventive measures were proposed, and the investigative commission did not formulate any safety recommendations.

Probable cause

Error in planning the approach to landing in conditions of weak variable wind, resulting in touchdown with a 300 m float.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2015-1620/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.