|Aircraft registration number||RA-67047|
|Accident site||in the Khabarovsk Territory|
|Aircraft operator||Khabarovsk Airlines|
|The date of the completion of the investigation (report)|
|Number of fatalities||6|
|Degree of aircraft destruction||aircraft substantially damaged|
On 15.11.2017 in the Khabarovsk Territory the accident with L-410 RA-67047 aircraft operated by Khabarovsk Airlines occurred.
According to the available information 2 crew members and 5 passengers were on board. 2 crew members and 4 passengers were killed, one passenger was seriously injured, the aircraft sustained substantial damage.
In accordance with the RF aviation legislation, the Interstate Aviation Committee assigned an Investigation team. The Investigation team starts its work.
Interstate Aviation Committee informs that the Investigation team of the fatal accident with L410 UVP-E20 RA-67047 aircraft continues its work at the accident site.
A wreckage plot was drawn by the Investigation team. The aircraft crashed onto the forested area at a distance of 1200 m from RWY 41 threshold of Nelkan aerodrome. The ground collision occurred almost without a forward speed. During the ground impact the aircraft sustained substantial damage. Investigators took the fuel and oil samples in order to send them for further research.
Flight recorders (FDR and CVR) were found at their normal places in satisfactory condition. Flight recorders are dismounted and prepared for data downloading.
The Investigation team of the L410 UVP-E20 RA-67047 aircraft fatal accident continues its work at the accident site. Preparations for the aircraft and engines transportation to the examination facilities are being conducted. The team of experts from the Czech Republic, participating in the investigation work, includes the representatives from Ge Aviation Czech (engine manufacturer).
The Investigation team has performed the downloading and readout of the flight recorders' data. The obtained flight data and voice records are being analyzed by experts of the IAC laboratory.
Based on the preliminary information it is found that during the final stage of the approach to Nelkan landing site, at height of 150 meters, the abnormal situation developed, related to the right power plant operation. Further, the aircraft lost the speed, the right roll was developed (the FDR recorded the bank angle over 180 degrees), and with-the-ground collision occurred. The flight crew attempts to counteract the roll tendency had failed.
The left engine was operating normally. There was no engines' in-flight shutdown.
All the necessary information for the flight safety measures implementation has been provided to the competent civil aviation authorities.The Investigation team together with the accredited representative of the Czech Republic and specialists from the aircraft (Aircraft Industries) and engine manufacturers continues to work out all possible circumstances of the fatal accident.