Crash of a PZL-Mielec AN-2 in Borogon

Date & Time: Mar 25, 1985 at 1101 LT
Type of aircraft:
Operator:
Registration:
CCCP-44905
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Borogon - Tiksi
MSN:
1G24-05
YOM:
1962
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After completing a cargo flight from Tiksi to Borogon, the crew was returning to Tiksi on a ferry flight. There were no passengers and no cargo on board. After takeoff from Borogon, while climbing to a height of 8 meters at a speed of 120 km/h, the flaps retracted automatically from 30° to zero. The aircraft entered an uncontrolled descent, struck the snow covered ground and crashed 250 meters past the runway end. All three crew members escaped with minor injuries while the aircraft was damaged beyond repair.
Probable cause:
It was determined that the flaps retracted prematurely and accidentally following a short-circuit by the flaps button where electrical resistances were corroded by condensation.

Crash of a PZL-Mielec AN-2 off Tiksi: 5 killed

Date & Time: Sep 26, 1969 at 2027 LT
Type of aircraft:
Operator:
Registration:
CCCP-44984
Survivors:
Yes
Schedule:
Borogon – Tiksi
MSN:
1G27-06
YOM:
1963
Flight number:
T-2
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Aircraft flight hours:
5515
Aircraft flight cycles:
3918
Circumstances:
On final approach to Tiksi by night and poor weather conditions, while at an altitude of 300 meters and a speed of 150 km/h, the engine failed. The airplane stalled and crashed into the Tiksi bay, some 2.5 km from the runway threshold. A passenger was rescued while five other occupants were killed.
Probable cause:
The engine failed on approach to Tiksi Airport due to the failure of exhaust valves, pistons and cylinders. It was also determined that the cylinder head temperature decreased on final approach and that the carburetor was iced, causing the engine to lose power and the aircraft to suffer a reduction of aerodynamic performances.