Casualties unknown

2003-09-21: Piper Cub 3 (OK-DUO) — LKCE, CZ

LKCE, CZ

On September 21, 2003, a Piper Cub 3 (registration OK-DUO) was involved in an aviation accident near LKCE, CZ. Investigators recorded the probable cause as: Main cause: failure to maintain minimum height above obstacles. Contributing causes: piloting under influence of alcohol, exceeding takeoff weight by at least 26%, relatively high air temperature. This summary draws on records from the Czech Air Accidents Investigation Institute (UZPLN).

Sourcesthe Czech Air Accidents Investigation Institute (UZPLN)Primary reportUpdated 1785693429Data APIEditorial standards

On 21 September 2003, an ultralight Piper Cub 3 (OK-DUO 04) struck trees and crashed at Česká Lípa airport after a low pass. The pilot was seriously injured; the passenger died. The investigation found the pilot had alcohol in his blood, the aircraft was overweight, and the flight was conducted at low altitude.

Accident Overview

On 21 September 2003 at 12:34 UTC, an ultralight Piper Cub 3, registration OK-DUO 04, crashed near Česká Lípa airport. The aircraft was destroyed. The pilot sustained serious injuries, and the passenger died. The accident was investigated by the Czech accident investigation body (ÚZPLN) in cooperation with the Police of the Czech Republic.

Flight Sequence

After a low pass over the airport, the aircraft entered a gentle climb. Approximately 500 meters from the threshold of runway 13, it struck tree tops and impacted the ground. Witnesses reported that after takeoff, the aircraft climbed to about 20 meters, then turned left and right, continuing at low altitude between airport buildings. It began a shallow climb at 90 km/h, but insufficient height gain led to the tree collision.

Injuries and Damage

The pilot suffered serious injuries. The passenger died. The aircraft was completely destroyed. No other damage was reported.

Aircraft Information

The aircraft was an amateur-built UL Piper Cub 3 (year of manufacture 1999), powered by a Micron engine (Walter, 1965) with a Křemen propeller (1999). The empty weight was 376 kg. The technical permit limited the aircraft to one crew member. At the time of the accident, the aircraft carried two persons (estimated 170 kg) and about 20 kg of fuel, resulting in a takeoff weight of approximately 566 kg—at least 116 kg (26%) over the maximum permitted takeoff weight. The aircraft's last inspection was valid until 30 September 2003.

Pilot Information

The pilot, aged 56, held a valid airline transport pilot license and an ultralight pilot license. He had about 8,000 hours on airplanes, but only 1 hour 50 minutes on ultralights. A medical examination was performed on 17 September 2003. A blood alcohol test after the accident revealed a level of 0.78 g/kg.

Meteorological Conditions

The weather at 12:30 UTC was partly cloudy, wind 130–150° at 2–3 m/s, visibility over 10 km, and temperature 30–32°C. The high temperature negatively affected climb performance.

Conclusions and Probable Cause

The investigation concluded that the main cause of the accident was the pilot's failure to maintain minimum flight altitude above surrounding obstacles. Contributing factors included piloting under the influence of alcohol, exceeding the maximum takeoff weight by at least 26%, and the relatively high air temperature. Additionally, the aircraft was operated with a passenger contrary to the technical permit.

Investigation report by the Czech Air Accidents Investigation Institute (UZPLN). Original record: https://uzpln.gov.cz/incident/37. This page is a structured re-presentation; facts and quotes are in the Ustav pro odborne zjistovani pricin leteckych nehod (UZPLN), Czech Republic.