Crash of a Cessna 402B in Cajicá: 3 killed

Date & Time: Aug 8, 2015 at 1003 LT
Type of aircraft:
Operator:
Registration:
HK-4990
Flight Type:
Survivors:
No
Schedule:
Guaymaral - Guaymaral
MSN:
402B-1219
YOM:
1977
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5539
Captain / Total hours on type:
0.00
Copilot / Total flying hours:
2594
Copilot / Total hours on type:
59
Aircraft flight hours:
8985
Circumstances:
The twin engine airplane departed Bogotá-Guaymaral Airport on a local training flight, carrying one passenger, one instructor and one pilot who was following his initial training. While descending to the airport from the north for an approach to runway 11, the crew encountered technical problems with the engine and declared an emergency. While trying to make an emergency landing, the aircraft collided with power cables and crashed in a garden located about 12 km north of Bogotá-Guaymaral Airport. The aircraft was destroyed by impact forces and all three occupants were killed. There was no fire.
Probable cause:
Double engine failure on approach due to fuel exhaustion. The following contributing factors were identified:
- Poor Crew Resources Management in decision making, team work and communications in the cockpit,
- Low level of alert of the crew while completing a training mission,
- The crew failed to follow the emergency procedures,
- Limited experience of the instructor to proceed with an initial training,
- Poor flight planning.
Final Report:

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

Date & Time: Aug 1, 2015 at 0805 LT
Type of aircraft:
Operator:
Registration:
YR-PEG
Flight Phase:
Survivors:
Yes
MSN:
1G197-44
YOM:
1982
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
6577
Circumstances:
The history of occurrence was established based on the witnesses’ statements. On 31.07.2015, the aircraft AN-2 registered YR-PEG was positioned on a flight field in the vicinity of the farm in Stӑncuţa commune, Brăila County, being prepared in order to perform several aviochemical flights in Giurgeni area on the following day. In the morning of 01.08.2015, the pilot and the aeronautical technical staff from his team were informed by the beneficiary of aviochemical works that, because it was raining in Giurgeni area, they will perform some aviochemical flights in Stӑncuţa area, in the vicinity of the flight field. Consequently, the aircraft was prepared for the flight in the area as follows: 200 l of gasoline were defueled from the aircraft tanks, the engine was started and the operating parameters were checked according to the specific diagram. The aircraft was supplied with chemical substances for the aerial work and after only a few minutes, the engine was started again, in order to take-off. Onboard there were the pilot and an aeronautical technician (hereinafter referred to as passenger) who occupied the pilot's seat on the right. The take-off on the S-N direction was normal in the first part. The take-off run was short – approximately 100 m, in the witnesses’ opinion – under the conditions of a gusty wind from the E direction, whose speed was gradually increasing. During the initial climb, at a height of about 15-20 m, the aircraft began to lean to the left and descend slightly. During this turn in descent, bank angle continued to increase, the aircraft flying with the left wing at very low height above the aircrafts parked towards the northern end of the flight field. Considering the aircraft evolution and observing that the pilot was not acting for correction, the passenger onboard on the right-hand pilot seat, tried instinctively to turn the aircraft control yoke to the right. According to his statement, he failed to operate the control yoke, considering that this was in a blocking state of which nature he could not specify. With the engine still running in take-off mode, the aircraft continued to descend, and after passing the parked aircrafts, it hit the ground with the propeller and the left wing tip. The impact of the wing tip determined the aircraft to pivot to the left and make a hard contact with the ground. The engine stopped because of the shock. An early fire was extinguished by witnesses arrived at the accident site. Amid the destruction of the cockpit and fuselage, the pilot was thrown out of the aircraft suffering serious injuries. The passenger, who occupied the right-hand seat, managed (after recovering from the shock) to exit the aircraft wreckage. The pilot and passenger were transported to the hospital. Later on, the pilot died due to multiple traumatic injuries, and the passenger required a long hospitalization period due to the injuries suffered. The aircraft was totally destroyed. There was no other damage in the area.
Probable cause:
The probable causes of this accident are the following:
- Temporary incapacitation of the pilot,
- Use of flaps upon take-off in the conditions of deterioration/modification of weather conditions during take-off (wind direction and speed),
- Aircraft operation with incomplete crew.
Final Report:

Crash of a Casa CN-235M-100 in Agustín Codazzi: 11 killed

Date & Time: Jul 31, 2015 at 1430 LT
Operator:
Registration:
FAC1261
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Palanquero – Valledupar – Barranquilla
MSN:
C-118
YOM:
1997
Country:
Crew on board:
11
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
The aircraft departed Palanquero AFB on a flight to Barranquilla with an intermediate stop in Valledupar. While cruising in poor weather conditions, the crew informed ATC about an engine failure when radio contact was lost. The aircraft entered an uncontrolled descent and crashed in a field located near Agustín Codazzi, some 50 km south of Valledupar. The aircraft was totally destroyed by impact forces and there was no fire. All 11 crew members were killed. The airplane was completing a special mission on behalf of the Colombian Intelligence Forces.
Crew:
Maj Adalberto Ramírez,
Lt Sergio Bojacá,
2nd Lt Luisa Salazar,
2nd Lt Andrés Rojas,
1st Tec Juan Carlos Correa,
Tec Jorge Iván Angulo,
Tec Giovany Roa,
Tec Tercero Juan Camilo Rivera,
Tec Tercero Hawer Moreno,
Tec Elkin Sierra,
Tec Édgar Contreras.

Crash of a Tupolev TU-95MS near Litovko: 2 killed

Date & Time: Jul 14, 2015 at 1650 LT
Type of aircraft:
Operator:
Registration:
RF-94204
Flight Phase:
Survivors:
Yes
Schedule:
Ukrainka - Ukrainka
MSN:
00854
YOM:
1984
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was performing a training/reconnaissance mission out from Ukrainka AFB. While cruising at an altitude of 5,000 metres in clouds and icing conditions, three of the four engines failed. At an altitude of 3,500 metres, all seven crew members bailed out and the aircraft crashed in a tundra located some 30 km from Litovko, Amur district of the Khabarovsk region. Five crew members survived while two others were killed. The registration of the 'Bear' was dual RF-94204 and 77 Red.
Probable cause:
Triple engine failure while flying icing conditions.

Crash of a PZL-Mielec AN-2R near Kezhma

Date & Time: Jun 19, 2015 at 1653 LT
Type of aircraft:
Operator:
Registration:
RA-40646
Flight Phase:
Survivors:
Yes
Schedule:
Kodinsk - Kezhma
MSN:
1G213-53
YOM:
1985
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12732
Captain / Total hours on type:
5074.00
Copilot / Total flying hours:
4747
Copilot / Total hours on type:
3538
Aircraft flight hours:
5824
Aircraft flight cycles:
9346
Circumstances:
The single engine aircraft departed Kodinsk at 1400LT on a survey flight, carrying five fire bombers and four crew members (two pilots and two observers). About two hours into the flight, the occupant spotted a fire. All five fire bombers were dropped with their materials in two groups. Then the crew increased engine power and continued at an altitude of about 150-200 metres. The engine oil temperature started to increase and reached 150°. Five minutes later, the engine failed. The crew attempted an emergency landing when the aircraft impacted 20 metres tall trees, stalled and crashed in a wooded area. The wreckage was found south of Kezhma, some 126 km east of Kodinsk. All four occupants evacuated safely and the aircraft was destroyed.
Probable cause:
The accident with An-2 RA-40646 aircraft occurred during the emergency landing on a forest. The landing was due to inadvertent in-flight engine shutdown caused by destruction of bronze filling of hub 62.06.02 of master rod big end of crank mechanism. Most probably the destruction of hub bronze filling was caused by manufactured flaw consisting in a lack of bronze adhesion with steel base on the part of a surface.
Final Report:

Crash of a PZL-Mielec AN-2R near Rostov

Date & Time: Jun 15, 2015 at 0754 LT
Type of aircraft:
Operator:
Registration:
RA-84553
Flight Phase:
Survivors:
Yes
MSN:
1G189-20
YOM:
1980
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10541
Aircraft flight hours:
9645
Circumstances:
The single engine aircraft was engaged in a crop spraying mission on behalf of the Mikhail Farm located in the Tatsinsky District of the Rostov Region. The aircraft was carrying 400 kilos of fuel, 1,200 liters of pesticides, one pilot and one boy aged 13, the son of the farmer. Few minutes after takeoff, while approaching the area to be treated at a height of about 20-25 metres and at a speed of 130 km/h, the engine failed. The aircraft lost height, collided with power cables and crashed in a field, bursting into flames. The wreckage was found 2 km from the Mikhail farmhouse. The pilot escaped unhurt while the boy was injured. The aircraft was totally destroyed by a post crash fire.
Probable cause:
The reason for the accident with An-2 RA-84553 was performing a flight in a known defective aircraft, leading to engine failure and the need for in-flight forced landing, during which there was a collision with power lines, followed by a rough landing that led to the structural failure and fire. Investigation to determine the cause of the engine failure was not possible due to the failure to ensure the safety of the aircraft after the accident and the absence of operational and technical documentation. The adoption of the decision by the pilot to reject takeoff after detecting a loss engine power on the takeoff could have prevented the accident. The aircraft did not have a valid Certificate of Airworthiness and the time between overhauls had been exceeded on 10 April 2015.
Final Report:

Crash of a Swearingen SA226TC Metro II in Querétaro: 5 killed

Date & Time: Jun 2, 2015 at 1425 LT
Type of aircraft:
Operator:
Registration:
XA-UKP
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Santiago de Querétaro - Santiago de Querétaro
MSN:
TC-376
YOM:
1980
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
19172
Captain / Total hours on type:
3731.00
Copilot / Total flying hours:
364
Copilot / Total hours on type:
117
Aircraft flight hours:
26985
Aircraft flight cycles:
37207
Circumstances:
The twin engine aircraft was engaged in a post-maintenance test flight out from Santiago de Querétaro Airport, carrying three engineers and two pilots. It departed runway 09 at 1421LT and the crew was cleared to climb to FL125. While approaching the altitude of 12,000 feet, the aircraft entered an uncontrolled descent and crashed on a motorway located 11 km southwest of the airport, bursting into flames. The aircraft was totally destroyed by impact forces and a post crash fire and all five occupants were killed.
Probable cause:
Loss of control of the aircraft in flight for undetermined reasons. No mechanical failure was found on the aircraft and its components that could affect the normal operation of the airplane.
The following findings were identified:
- Lack of coordination and effective communication between ground staff and flight crew,
- Lack of adequate supervision of operations by the operator,
- Lack of a safety culture of the operator.
Final Report:

Crash of a Embraer EMB-821 Carajá in Rochedo

Date & Time: May 24, 2015 at 0953 LT
Operator:
Registration:
PT-ENM
Flight Phase:
Survivors:
Yes
Schedule:
Miranda – Campo Grande
MSN:
820-072
YOM:
1978
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8378
Captain / Total hours on type:
470.00
Copilot / Total flying hours:
1006
Copilot / Total hours on type:
4
Circumstances:
The twin engine airplane departed Miranda-Estância Caimam Airfield at 0915LT on a charter flight to Campo Grande, carrying seven passengers and two pilots. About 35 minutes into the flight, while flying 79 km from the destination in good weather conditions, the left engine failed. The crew was unable to feather the propeller and to maintain a safe altitude, so he decided to attempt an emergency landing. The aircraft belly landed in an agriculture area, slid for few dozen metres and came to rest. All nine occupants suffered minor injuries and the aircraft was damaged beyond repair.
Probable cause:
Failure of the left engine in flight due to fuel exhaustion. The following findings were identified:
- The fuel tanks in the left wing were empty while a quantity of 320 litres of fuel was still present in the fuel tanks of the right wing,
- The crew was unable to maintain altitude because he could not feather the left propeller,
- The pilots were misled by a false indication of the fuel gauge coupled to the left wing tank which displayed a certain value while the tank was actually empty. This error was caused by the fuel sensors for the left wing tanks being installed inverted,
- The aircraft was not airworthy at the time of the accident due to several defects,
- The Minimum Equipment List (MEL) was not up to date,
- The Cockpit Voice Recorder (CVR) was unserviceable,
- The automatic propeller feathering system was out of service,
- The fuel sensors for the left wing tanks had been installed inverted,
- Bad contact with the right wing fuel sensor connector plug,
- The pilots failed to follow the published procedures related to an engine failure,
- Poor flight preparation,
- Crew complacency,
- The crew training program by the operator was inadequate,
- Lack of supervision on part of the operator.
Final Report:

Crash of a Embraer EMB-820C Navajo in Ricaurte: 2 killed

Date & Time: May 24, 2015 at 0040 LT
Operator:
Registration:
PT-RCN
Flight Phase:
Flight Type:
Survivors:
No
MSN:
820-121
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew took off from a small airfield located in the suburb of Manaus at the end of the day with a load of 616 small packages containing cocaine. After entering the Venezuelan Airspace without clearance, the crew was contacted twice by ATC but failed to answer. Authorities decided to send two fighters to establish a visual and radio contact with the crew but without success as, due to the low visibility caused by night and poor weather conditions, the crew of the Navajo was able to continue the flight without further problem. Nevertheless, three hours later, the twin engine aircraft was again localized passing over the State of Cojedes, and the decision was taken to shoot it down. Out of control, the Navajo crashed in a pasture located in the region of Ricaurte, and was totally destroyed by impact forces. Both pilots were killed and a load of narcotics was found. At the time of the accident, the aircraft was illegally registered YV1246 as a sticker has been affixed above the official Brazilian registration PT-RCN.
Probable cause:
Shot down by the pilot of a Venezuelan Air Force fighter.

Crash of a Cessna 441 Conquest II near Cañaote: 3 killed

Date & Time: Apr 1, 2015
Type of aircraft:
Operator:
Registration:
XB-KGS
Flight Phase:
Flight Type:
Survivors:
No
MSN:
441-0232
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Crashed in unknown circumstances near Cañaote, State of Cojedes. The wreckage was found the following morning. The aircraft was destroyed, all three occupants were killed and a load of 999 kilos of cocaine was found among the debris.