Casualties unknown

2018-07-08: (SE-AJA) — LV

LV

On July 8, 2018, an aircraft (registration SE-AJA) was involved in an aviation accident near LV. Investigators recorded the probable cause as: The direct cause of the accident was the pilot's inability to manage the aircraft during a high-stress emergency landing maneuver at low altitude. This summary draws on records from the Transport Accident and Incident Investigation Bureau of Latvia (TAIIB).

Sourcesthe Transport Accident and Incident Investigation Bureau of Latvia (TAIIB)Primary reportUpdated 1785062164Data APIEditorial standards

A Bücker Bü 133C Jungmeister crashed in Latvia after an engine failure caused by insufficient oil supply, resulting in the death of the pilot.

What happened

On July 8, 2018, a Bücker Bü 133C Jungmeister, registration SE-AJA, departed from Birzai, Lithuania, as part of a three-aircraft formation flying to Spilve, Latvia. While entering Latvian airspace, the pilot reported low oil pressure and initiated an emergency landing procedure.

During the attempt to land, the aircraft performed a U-turn and subsequently collided with the ground in the Bauska district. The impact caused substantial damage to the engine and fuselage. The pilot, who was the sole occupant, sustained fatal injuries.

The investigation

The TAIIB examined the wreckage and the engine, a Siemens/Bramo SH 1 and A4. The investigation included an inspection of the engine components at a workshop in Germany. Investigators found that the engine showed clear evidence of overheating and inadequate lubrication on the piston rod bearings.

Technical analysis revealed that the engine's oil system had been modified with a separate oil tap, but no supporting documentation for this modification was available. Furthermore, a "ROTAX" oil filter had been installed on the aircraft's fire bulkhead, which did not comply with the engine's type certification. This non-compliant filter potentially restricted oil flow. Additionally, the investigation noted that the pilot's blood contained an alcohol concentration of 0.51‰, which exceeded the legal limit of 0.2‰.

Findings

  • The engine failed due to reduced lubricant supply, which led to a loss of engine power.
  • The installation of a non-compliant oil filter may have restricted the flow of oil to the engine.
  • The pilot was unable to maintain control of the aircraft during the emergency landing maneuver, which occurred at low altitude and low airspeed during a U-turn.
  • The pilot's physiological and psychological state was affected by alcohol consumption, as blood alcohol levels were found to be above the legal limit.
  • The engine showed traces of overheating and bearing wear consistent with insufficient oil supply.

Probable cause

The direct cause of the accident was the pilot's inability to manage the aircraft during a high-stress emergency landing maneuver at low altitude. The root cause was an engine failure resulting from insufficient oil supply to the engine lubrication system, compounded by the use of a non-compliant oil filter.

Investigation report by the Transport Accident and Incident Investigation Bureau of Latvia (TAIIB). Original record: https://www.taiib.gov.lv/lv/media/65/download?attachment. This page is a structured re-presentation; facts and quotes are in the Transporta nelaimes gadijumu un incidentu izmeklesanas birojs (TAIIB), Latvia.