Crash of a Fletcher FU-24-950 in North Rawajitu: 1 killed

Date & Time: May 11, 2013 at 1125 LT
Type of aircraft:
Operator:
Registration:
PK-PNC
Flight Phase:
Survivors:
No
Schedule:
North Rawajitu - North Rawajitu
MSN:
243
YOM:
1977
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Pilot was engaged in a spraying mission over an oil palm plantation in the region of North Rawajitu, Lampung Province. Less than three minutes after takeoff, the single engine aircraft stalled and crashed in a wooded area, bursting into flames. The aircraft was destroyed by impact forces and a post impact fire and the pilot, sole on board, was killed.

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

Date & Time: May 10, 2013 at 1020 LT
Type of aircraft:
Operator:
Registration:
YR-LRA
Flight Phase:
Survivors:
Yes
Schedule:
Balota - Balota
MSN:
1G195-09
YOM:
1982
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6100
Captain / Total hours on type:
6060.00
Copilot / Total flying hours:
400
Aircraft flight hours:
6598
Circumstances:
The single engine aircraft departed Balota (Drobeta) Aerodrome at 0930LT on a spraying mission over wooded area on behalf of the Department of Forestry, carrying one passenger and two pilots. About 50 minutes into the flight, after it completed several low passes over the area to be treated, the engine lost power. The crew decided to return to Balota Aerodrome and completed a 180 turn when the engine stopped. The crew attempted an emergency landing in an open field. After landing, the aircraft rolled for about 130 metres when the left main gear collapsed and the airplane came to rest. All three occupants escaped uninjured and the aircraft was damaged beyond repair.
Probable cause:
Engine failure in flight due to fuel exhaustion. The following contributing factors were identified:
- Poor flight preparation on part of the crew who did not follow the pre-takeoff checklist,
- The checklist document was printed in an inappropriate format for the purpose for which it was intended,
- The aircraft was damaged beyond repair due to the nature of the terrain where the emergency landing occurred.
Final Report:

Crash of a PZL-Mielec AN-2R in Vostochnaya: 1 killed

Date & Time: Mar 23, 2013 at 1503 LT
Type of aircraft:
Operator:
Registration:
RA-02203
Flight Phase:
Survivors:
Yes
Schedule:
Vostochnaya - Vostochnaya
MSN:
1G234-34
YOM:
1989
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5536
Captain / Total hours on type:
2710.00
Copilot / Total flying hours:
61
Copilot / Total hours on type:
61
Aircraft flight hours:
3612
Aircraft flight cycles:
16267
Circumstances:
The crew was engaged in a crop spraying flight on agricultural field in Vostochnaya, about 70 km northeast of Krasnodar. The day prior to the accident, the engine failed in flight and the crew made a forced landing in a field. As the carburetor was broken, it was replaced and an engine test run was performed. On 23 March, one minute after takeoff, while climbing to a height of 30 metres, the engine failed again. The crew attempted an emergency landing when the aircraft stalled and crashed in the Bakhotinski Lake, coming to rest upside down. The copilot escaped with minor injuries while the captain was killed. The wreckage was recovered three days later.
Probable cause:
The accident was caused by its nosing during the emergency landing on water surface. The emergency landing was caused by the engine power loss and flameout in the air due to the destruction of the exhaust collector can type combustor and burn through of the carburetor intake valve followed by high temperature burnt gases ingestion into the engine carburetor intake. The destruction of the exhaust collector can type combustor most probably occurred on the corrosion mechanism energized in conditions of the material heat during the engine operation using motor petrol. Power factor resulted in initial crack formation most probably was caused by residual tenses in the material of manufacture origine caused during can type combustor manufacture. In accordance with the passport the latest can type combustor overhaul was performed on January 27, 2009 in "Shakhtinsky ARZ DOSSAAF" CJSC. The commission didn't find the actual confirmation of the can type combustor overhaul as the marking at the single remained label indicates that the specified section had overhaul at the plant n° 420GA in October 1983.
Final Report:

Crash of a PAC Cresco 08-600 in Waitaanga

Date & Time: Dec 11, 2012 at 1738 LT
Type of aircraft:
Operator:
Registration:
ZK-LTR
Flight Phase:
Survivors:
Yes
Schedule:
Taumatunui - Mount Messenger
MSN:
003
YOM:
1980
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft crashed in unknown circumstances in Waitaanga while completing a spraying mission between Taumatunui and Mount Messenger. The aircraft was destroyed and the pilot, sole on board, was seriously injured.

Crash of a Fletcher FU-24A-954 near Rotorua: 1 killed

Date & Time: Dec 8, 2012 at 1315 LT
Type of aircraft:
Operator:
Registration:
ZK-EMX
Flight Phase:
Survivors:
No
MSN:
278
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
430
Captain / Total hours on type:
95.00
Aircraft flight hours:
11300
Circumstances:
The pilot, who was undertaking training toward a Grade 2 Agricultural Pilot Rating, began work at approximately 0625 hours on the day of the accident. The pilot and his instructor, who was in another topdressing aircraft, flew to a block of land to the south east of Rotorua where the pilot completed 15 sowing runs, while his instructor worked in the local vicinity in the second aircraft. The pilot and instructor completed the work on this block, had a break and then transited to the Waikite Valley, arriving at approximately 0945 hours. At 1045 hours, after refuelling his aircraft, the pilot commenced sowing a ‘special mix’ fertiliser, in an alternating pattern between the instructor and pilot, with two aircraft operating from the airstrip. The alternating pattern allowed the instructor to observe and supervise the pilot during the take off and landing phases, while allowing the operation to proceed efficiently. The pilot and instructor stopped for lunch after an hour of flying, refuelled once more and then continued with their work. The amount of fertiliser that was loaded into the pilot’s aircraft was progressively increased as the work proceeded. The initial load of product was 900 kg, gradually increasing by 50 kg increments, when the instructor was satisfied that the pilot’s performance allowed this increase. The last five loads carried prior to the accident were each 1100 kg. Nothing untoward was noticed during the sowing runs, apart from the pilot aborting one landing attempt, due to the wake turbulence from the instructor’s aircraft during take off. At the time of the accident the pilot was performing ‘clearing runs’, sowing on remaining areas of land not already covered by previous sowing runs. Immediately prior to the accident, the pilot called the instructor on the radio to enquire of his location. The instructor responded with “directly behind you on the other side of the woolshed”. A few seconds later, as the instructor approached to land at the airstrip, he observed the pilot’s aircraft flying in a westerly direction at approximately 400 ft AGL. He then saw the pilot’s aircraft make a slight turn to the left. Describing what he had seen as: “he started to climb and turn slightly to the left, then the plane was in a left hand spin”. The instructor thought at the time that the aircraft spun for one and a half rotations to the left, prior to being obscured by the ridge adjacent to the airstrip. The accident occurred in daylight, at approximately 1315 hours, at Waikite Valley, Rotorua, at an elevation of 1460 ft. Latitude S 38° 18.5', longitude E 176° 17.42'.
Probable cause:
Conclusions
- The pilot was appropriately licensed and held a valid medical certificate.
- The aircraft had been appropriately maintained and no technical discrepancy was discovered that could have contributed to the accident.
- It is likely that, during a climbing turn, the pilot inadvertently allowed an aerodynamic stall to occur at which point the aircraft suddenly departed controlled flight.
- No emergency jettison of the hopper contents was attempted.
- The height above the ground, was insufficient for the pilot to perform a successful recovery once the departure from controlled flight had fully developed.
- The pilot’s lack of experience with agricultural operations and relative unfamiliarity with the aircraft type could not be eliminated as having a bearing on the accident.
Final Report:

Crash of a Un PZL-Mielec AN-2R in Knyazhichi

Date & Time: Apr 23, 2012 at 1335 LT
Type of aircraft:
Operator:
Registration:
UR-81515
Flight Phase:
Survivors:
Yes
Schedule:
Knyazhichi - Knyazhichi
MSN:
1G208-15
YOM:
1984
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a spraying mission in the region of Knyazhichi, Sumy Oblast, Ukraine. Following 15 successful sorties that day, the crew was ready for the 16th and started the takeoff procedure from the third of the runway which is 768 metres long. After a course of 577 metres, the single engine aircraft failed to get airborne and overran. The crew decided to abort but this was too late. The aircraft sank in muddy field and rolled for about 56 metres before coming to rest upside down. Both occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The following factors were identified:
- The crew did not use the entire runway length for the takeoff procedure (577 metres instead of the 768 metres available),
- The decision of the crew to reject takeoff was taken too late,
- The wind direction changed during the takeoff procedure and became a tailwind component.

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

Date & Time: Apr 23, 2012 at 0845 LT
Type of aircraft:
Operator:
Registration:
YR-BOR
Flight Phase:
Survivors:
Yes
Schedule:
Şirna - Şirna
MSN:
1G192-13
YOM:
1981
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4500
Copilot / Total flying hours:
5550
Aircraft flight hours:
5467
Circumstances:
The crew departed Şirna Aerodrome around 0830LT on a local spraying mission. About 15 minutes into the flight, the crew encountered engine problems and elected to make an emergency landing. He found a suitable terrain and attempted to land when the aircraft collided with a small concrete wall and some bushes before coming to rest in an open field. Both pilots escaped uninjured and the aircraft was damaged beyond repair.
Probable cause:
Failure of the crew who selected an unsuitable terrain for an emergency landing (rough terrain) and did not take into consideration the wind component.
Final Report:

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

Date & Time: Oct 9, 2011 at 1128 LT
Type of aircraft:
Operator:
Registration:
RA-81514
Flight Phase:
Survivors:
Yes
Schedule:
Zasovskaya - Zasovskaya
MSN:
1G208-14
YOM:
1984
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13000
Aircraft flight hours:
6449
Aircraft flight cycles:
30385
Circumstances:
The pilot, sole on board, was completing a spraying mission on sunflower plantations in Zasovskaya. While flying at a height of about 20 metres, preparing for a new low pass, the single engine aircraft collided with power cables, stalled and crashed upside down in an open field, bursting into flames. The aircraft was destroyed and the pilot was seriously injured.
Probable cause:
The cause of the accident without casualties to the plane An-2 RA-81514 was a violation of the established safe obstacle clearance in the performance of aviation-chemical works, which led to a collision with the lightning protection wire transmission line and the ground. A contributing factor was the performance of an incomplete flight crew. According to the An-2 Flight Manual the minimum crew for aerial chemical works is the commander of the aircraft and a copilot.
Final Report:

Crash of a PZL-Mielec AN-2R near Sasha: 1 killed

Date & Time: Sep 3, 2011 at 1200 LT
Type of aircraft:
Operator:
Registration:
UR-17739
Flight Phase:
Survivors:
No
MSN:
1G202-59
YOM:
1983
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Sole on board, the pilot was completing a crop spraying mission between the villages of Sasha and Kostyukivka. While manoeuvring at low height, the single engine aircraft hit tree tops, stalled and crashed, bursting into flames. The aircraft was destroyed by impact forces and a post impact fire and the pilot was killed.

Crash of a PZL-Mielec AN-2R in Baranikovskiy: 1 killed

Date & Time: Aug 28, 2011 at 0854 LT
Type of aircraft:
Operator:
Registration:
RA-01105
Flight Phase:
Survivors:
Yes
Schedule:
Baranikovskiy - Baranikovskiy
MSN:
1G239-50
YOM:
1991
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
1208
Aircraft flight cycles:
4247
Circumstances:
The single engine aircraft was dispatched in Baranikovskiy to perform a crop spraying mission on rice paddy field. Before flight, the tank was refueled with 250 litres of E95 fuel. The technician told the pilot the fuel was abnormally yellow but the pilot decided to proceed with the flight. Prior to take off, he asked the copilot to stay on ground and replaced him by the owner of the zone to be treated which is against the published procedures. During the takeoff roll, the aircraft did not accelerate as expected but the pilot continued. After liftoff, at a height of about 30 metres, the pilot initiated a 90° left turn when the engine lost power. He started to drop the load of chemicals then attempted an emergency landing when the aircraft impacted ground. It continued for about 134 metres then struck an irrigation drain, nosed over and came to rest, bursting into flames. The pilot was killed and the passenger was seriously injured.
Probable cause:
The accident was caused by a loss of engine power because the aircraft has been refueled with fuel dedicated to automobile.
The following contributing factors were identified:
- The pilot's lack of knowledge about the flight area and the layout of cultivated fields,
- The pilot failed to brake properly during the emergency landing,
- The absence of a copilot on board,
- The Operator certificat was revoked 3 days prior to the accident.