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.

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

Date & Time: Mar 25, 2015 at 0046 LT
Type of aircraft:
Registration:
UR-62681
Flight Type:
Survivors:
No
MSN:
1G179-11
YOM:
1978
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was performing an illegal flight, most probably from Belarus, with a load of cigarettes on board. By night, he was attempting to land in a field located in Promin when the single engine aircraft impacted the roof of a house and crashed on a small road, bursting into flames. The aircraft was destroyed by a post crash fire and both occupants were killed.

Crash of a Cessna 208B Grand Caravan in Verdigris

Date & Time: Mar 24, 2015 at 1507 LT
Type of aircraft:
Operator:
Registration:
N106BZ
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Tulsa - Tulsa
MSN:
208B-0106
YOM:
1988
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6500
Captain / Total hours on type:
970.00
Aircraft flight hours:
11443
Circumstances:
The pilot reported that, during the postmaintenance test flight, the turboprop engine lost power. The airplane was unable to maintain altitude, and the pilot conducted a forced landing, during which the airplane was substantially damaged. The engine had about 9 total flight hours at the time of the accident. A teardown of the fuel pump revealed that the high-pressure drive gear teeth exhibited wear and that material was missing from them, whereas the driven gear exhibited little to no visible wear. A metallurgical examination of the gears revealed that the damaged drive gear was made of a material similar to 300-series stainless steel instead of the harder specified M50 steel, whereas the driven gear was made of a material similar to the specified M50 steel. Subsequent to these findings, the airplane manufacturer determined that the gear manufacturer allowed three set-up gears made from 300-series stainless steel to become part of the production inventory during the manufacturing process. One of those gears was installed in the fuel pump on the accident airplane, and the location of the two other gears could not be determined. Based on the evidence, it is likely that the nonconforming gear installed in the fuel pump failed because it was manufactured from a softer material than specified, which resulted in a loss of fuel flow to the engine and the subsequent loss of engine power. The manufacturer subsequently inspected its stock of gears and issued notices to customers that had engines with fuel pumps installed with the same part number gear set as the one installed on the accident airplane. The manufacturer also issued a service information letter and service bulletins regarding the fuel pump gear set for engines used in civilian and military applications. As of the date of this report, the two remaining gears have not been located.
Probable cause:
The fuel pump gear manufacturer’s allowance of set-up gears made from a nonconforming material to be put in the production inventory system, the installation of a nonconforming gear in the accident airplane’s production fuel pump, and the gear’s failure, which resulted in a loss of fuel flow to the engine and the subsequent loss of engine power.
Final Report: