Date & Time:
Feb 10, 1995 at 1609 LT
Type of aircraft:
Antonov AN-72
Operator:
Registration:
UR-72966
Flight Phase:
Flight
Flight Type:
Test
Survivors:
Yes
Schedule:
Kiev - Kiev
MSN:
36572092847
YOM:
1992
Country:
Ukraine
Region:
Europe
Crew on board:
0
Crew fatalities:
0
Pax on board:
0
Pax fatalities:
0
Other fatalities:
0
Total fatalities:
0
Circumstances:
The aircraft departed Kiev-Gostomel Airport to assist the crew of the first AN-70 prototype in its test flight. The goal of the flight was to test the stability and controllability of the airplane for the certification program. While cruising at an altitude of 3,200 metres, the crew of the AN-70 elected to approach the AN-72 but misjudged the distance, causing both airplanes to collided. The tail of the AN-70 struck the fuselage of the AN-72. The crew of the AN-72 was able to return to Kiev-Gostomel Airport and to complete a safe landing. All crew members were uninjured but the aircraft was damaged beyond repair due to severe structural damages. Upon impact, the AN-70 lost its left stabiliser and also a part of the tail. Out of control, it entered a dive and crashed in a wooded area located in Veliky Lis, about 45 km northwest of Kiev-Gostomel Airport. All seven occupants were killed.
Probable cause:
It was determined that the collision was the consequence of errors on part of the AN-70 crew who misjudged the distance between both aircraft and initiated a hazardous maneuver without knowing the exact position of the second aircraft. The following contributing factors were reported:
- The collision occurred while both aircraft were facing sun,
- Both crew did not use appropriate radio communications,
- Loss of situational awareness,
- Loss of the left horizontal stabiliser as well as part of the tail, failure of all four hydraulic systems, loss of controllability.
- The collision occurred while both aircraft were facing sun,
- Both crew did not use appropriate radio communications,
- Loss of situational awareness,
- Loss of the left horizontal stabiliser as well as part of the tail, failure of all four hydraulic systems, loss of controllability.
