Casualties unknown

2018-07-05: (YL-JKV) — LV

LV

On July 5, 2018, an aircraft (registration YL-JKV) was involved in an aviation accident near LV. Investigators recorded the probable cause as: The fracture of the right main landing gear shock strut attachment lugs was due to low-cycle fatigue caused by varying loads during operation. A crack developed and propagated unnoticed during routine inspections, leading to failure. 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

On 5 July 2018, a Piper PA-28-140 experienced a right main landing gear failure during flight; the pilot performed an emergency landing at Ādaži airfield. No injuries occurred. Investigation found fatigue fractures in the gear attachment lugs.

Incident Description

On 5 July 2018, at approximately 18:30 local time, a Piper PA-28-140 (registration YL-JKV) was conducting touch-and-go landing exercises at Spilve airfield. After climbing to 1,000 feet, the pilot noticed vibration on the right side of the aircraft. The passenger visually confirmed damage to the right main landing gear. To minimize the consequences, the pilot decided to land at Ādaži airfield, which has a grass runway. The emergency landing was successful.

Aircraft Damage

Post-landing inspection revealed that the right main landing gear strut fairing was bent forward, and the attachment lugs of the shock strut cylinder were fractured. The wheel was held only by the brake hose. The aircraft sustained minor structural damage, deemed repairable.

Investigation and Analysis

The Latvian Transport Accident and Incident Investigation Bureau (TAIIB) conducted the investigation. The damaged shock strut cylinder was sent to the Riga Technical University for metallurgical examination. Analysis showed that the fractures had a low-cycle fatigue character, resulting from varying loads during operation. A crack had developed in the lower part of the attachment lugs and propagated over time. The crack was not detected during routine inspections. The material was a cast alloy with a fine-grained surface layer, which may have contributed to crack initiation.

Probable Cause

The fracture of the right main landing gear shock strut attachment lugs was due to low-cycle fatigue caused by varying loads during operation. A crack developed and propagated unnoticed during routine inspections, leading to failure.

Investigation report by the Transport Accident and Incident Investigation Bureau of Latvia (TAIIB). Original record: https://www.taiib.gov.lv/lv/media/66/download?attachment. This page is a structured re-presentation; facts and quotes are in the Transporta nelaimes gadijumu un incidentu izmeklesanas birojs (TAIIB), Latvia.