Country
Lithuania

Crash of a PZL-Mielec AN-2R in Trollhättan

Date & Time: Aug 26, 2003 at 1730 LT
Type of aircraft:
PZL-Mielec AN-2
Operator:
Svedijos Prekes
Registration:
LY-KAE
Flight Phase:
Landing (descent or approach)
Flight Type:
Training
Survivors:
Yes
Site:
Airport (less than 10 km from airport)
Schedule:
Trollhättan - Trollhättan
MSN:
1G196-54
YOM:
1982
Location:
Trollhättan
Västergötland
Country:
Sweden
Region:
Europe
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing at Trollhättan-Målöga Airport, the aircraft nosed over and came to rest upside down. Both occupants escaped uninjured while the aircraft was damaged. It was apparently repaired.
Probable cause:
The pilot used excessive brakes after touchdown, causing the brakes to block. The landing maneuver was completed with a tailwind component.

Crash of a PZL-Mielec AN-2TP near Rocca di Mezzo: 3 killed

Date & Time: Mar 9, 2002 at 1339 LT
Type of aircraft:
PZL-Mielec AN-2
Operator:
Svedijos Prekes
Registration:
LY-AVD
Flight Phase:
Flight
Flight Type:
Ferry
Survivors:
No
Site:
Mountains
Schedule:
Budapest - Tunis
MSN:
1G137-53
YOM:
1972
Flight number:
SJK2801
Location:
Rocca di Mezzo
Abruzzo
Country:
Italy
Region:
Europe
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft departed Budapest-Ferihegy Airport at 0829LT on a VFR flight to Tunis. According to the flight plan the aircraft would fly over Split, Pescara, crossing the Apennines towards Ostia and then onwards to Tunis. Weather conditions over the central part of Italy were poor with a cold front associated with thunderstorm activity, low clouds and icing conditions. After passing over the Adriatic sea, the aircraft overflew Pescara at 1320LT where the pilot informed ATC that the aircraft was inbound Aneda (a reporting point 19 NM East of Monte Rotondo) at a cruising altitude of 5.500 feet. While in vicinity of Pescara, ATC requested and obtained confirmation from the crew that he was able to continue under VFR mode. Shortly later, at a speed of 115 knots, the single engine aircraft struck the slope of Mt Rotondo (1.880 metres high) located near Rocca di Mezzo. The aircraft disintegrated on impact and all three occupants were killed.
Probable cause:
Analysis of available evidence make it reasonable to classify the event investigated as an unintentional terrain impact, Controlled Flight Into Terrain (CFIT). At accident time, because of the reduced visibility, incompatible with VFR flying, the crew could not evaluate correctly the orography of the area along there route. It has to be noted that it was not possible to ascertain if adequate maps were available to the crew showing the exact position of ground relief and obstacles. It was not possible to determine if the pilots had flown across the same area in the past. Given the meteorological conditions over the area, the crew did not conform to the Visual Flying Rules that mandated for a track change to maintain the required flight parameters (visibility/clearance from obstacles) and/or a diversion to a suitable alternate airport (as international rules mandate).
Contributing factors:
Analysis of available evidence suggests that the following may be considered as contributory factors to the accident. The prevailing meteorological conditions existing on March 9, 2002 over the flight path of LY-AVD across the central part of Italy did not allow for the flight to be continued under VFR. The Antonov AN-2 was not fit for flying in low visibility (IMC) and was not equipped for flying in icing conditions. The pilot of the LY-AVD did not hold the required English language radio-telephony (RT) qualification to operate outside the country of licensing. The pilot of the LY-AVD did not hold an IFR qualification (for flying in IMC).
Final Report:
Subscribe to Svedijos Prekes