Crash of an Ilyushin II-76TD near Bagram AFB: 9 killed

Date & Time: Jul 6, 2011 at 0010 LT
Type of aircraft:
Operator:
Registration:
4K-AZ55
Flight Type:
Survivors:
No
Site:
Schedule:
Baku - Bagram AFB
MSN:
20534 20680
YOM:
2005
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The four engine aircraft departed Baku-Bina Airport at 2126LT on a cargo flight to Bagram AFB, carrying 9 crew members and a load of 18 tons of various goods destined to the NATO forces deployed in Afghanistan. While approaching Bagram AFB by night, at an altitude of 12,500 feet, the aircraft impacted the slope of a mountain located 25 km from the airport. The wreckage was found at the first light of day. The aircraft was destroyed and all 9 occupants were killed.

Crash of a De Havilland DHC-3 Otter in Mayo: 1 killed

Date & Time: Mar 31, 2011 at 1507 LT
Type of aircraft:
Operator:
Registration:
C-GMCW
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Mayo - Rackla
MSN:
108
YOM:
1956
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5000
Captain / Total hours on type:
3000.00
Aircraft flight hours:
16431
Circumstances:
The aircraft was being utilized in support of mineral exploration activities, to transport building materials, fuel, and winter camp supplies from Mayo, Yukon, to winter airstrips located at Withers Lake and Rackla River, Yukon. Withers Lake is located 113 statute miles (sm) east of Mayo, and Rackla Airstrip is located 94 sm northeast of Mayo (Appendix B). On the accident flight, the aircraft was transporting a load of twelve 6-inch by 6-inch wood timbers, each 16 feet long, and 2 barrels of jet fuel. The pilot had arrived at the Mayo Airport at about 0630 1 on the morning of the accident. The pilot’s first trip of the day was to Withers Lake, departing Mayo at 0834. The pilot completed 2 trips to Withers Lake and 1 trip to Rackla prior to the accident flight. The accident flight departed Mayo at 1448 under visual flight rules (VFR) on a company itinerary. At 1507 the Canadian Mission Control Centre (CMCC) received a 406-MHz emergency locater transmitter (ELT) alert. Joint Rescue Co-ordination Centre Victoria (JRCC Victoria) was notified at 1522. Aircraft operating in the area were alerted, and a commercial helicopter was dispatched from Ross River, Yukon, approximately 1 hour later to search for the aircraft. The helicopter crew located the aircraft wreckage at 1833 at about 4300 feet above sea level (asl), on a remote, snow-covered hillside 38 nautical miles (nm) northeast of Mayo.
Probable cause:
The aircraft departed controlled flight for reasons which could not be determined, and broke up due to high speed.
Final Report:

Crash of a Cessna 550 Citation II in Manas: 3 killed

Date & Time: Mar 28, 2011 at 1945 LT
Type of aircraft:
Operator:
Registration:
B-7026
Flight Phase:
Survivors:
No
Site:
Schedule:
Korla - Korla
MSN:
550-0305
YOM:
1982
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Owned by the Zhongfei General Aviation Company (CFGAC), the airplane was engaged in a survey flight over the north China province of Xinjiang. It departed Korla Airport at 1600LT with a crew of three. En route, it crashed in unknown circumstances in the Manas County, Hui autonomous prefecture of Changji. SAR did not find any trace of the aircraft nor the crew. Fatal index is presumed.

Crash of a Cessna 340A near Lobatera: 6 killed

Date & Time: Feb 22, 2011 at 1510 LT
Type of aircraft:
Registration:
YV2402
Flight Phase:
Survivors:
No
Site:
Schedule:
Valera – El Vigía – San Antonio del Táchira
MSN:
340A-1502
YOM:
1982
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The twin engine aircraft departed Valera Airport on a charter flight to San Antonio del Táchira with an intermediate stop in El Vigía, carrying five passengers and one pilot. All flight was completed under VFR mode but while descending to San Antonio del Táchira, weather conditions worsened and the pilot switched to IFR mode. Shortly later, control was lost and the aircraft crashed on the slope of Mt Laja, near Lobatera. The wreckage was found about 25 km northeast of San Antonio del Táchira Airport. The aircraft disintegrated on impact and all six occupants were killed.
Probable cause:
The most probable cause for the occurrence of this accident was the loss of situational awareness, caused mainly by the change of flight conditions under visual rules to flight under instrumental flight rules, due to the adverse weather conditions in which the descent phase began, so it is possible to establish the Human Factor as the cause of the accident and the Physical Factor as a contributor.

Crash of a Let L-410UVP near Bukavu: 2 killed

Date & Time: Feb 14, 2011 at 1615 LT
Type of aircraft:
Registration:
9Q-CIF
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Bukavu – Lusenge
MSN:
83 09 22
YOM:
1983
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Eight minutes after takeoff from Bukavu-Kavumu Airport, while climbing, the twin engine aircraft crashed in unknown circumstances on the slope of Mt Biega, some 25 km north of Bukavu. The aircraft was destroyed and both pilots were killed. They were completing a cargo flight to Lusenge.

Crash of a Beechcraft B200 Super King Air in Goiânia: 6 killed

Date & Time: Jan 14, 2011 at 1810 LT
Registration:
PR-ART
Survivors:
No
Site:
Schedule:
Brasília – Goiânia
MSN:
BB-806
YOM:
1981
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
2500
Captain / Total hours on type:
550.00
Circumstances:
Following an uneventful flight from Brasília, the pilot started the descent to Goiânia-Santa Genoveva Airport in poor weather visibility with heavy rain falls and turbulences. On final approach, the twin engine aircraft descended below the glide until it impact the slope of Mt Santo Antônio located 10,7 km short of runway 32. The aircraft was destroyed by impact forces and a post crash fire and all six occupants were killed.
Probable cause:
The following findings were identified:
- Factors, such as obesity and sedentariness, associated with the high workload in the moments preceding the collision with the hill, may have contributed for the task demand to exceed the margins of safety, resulting in wrong decision-making by the pilot.
- Upon facing adverse meteorological conditions and being aware that aircraft which landed before him had reached better visibility in altitudes below 3,500 ft. on the final approach of the VOR procedure, the pilot may have increased his level of confidence in the situation, to the point of descending even further, without considering the risks involved.
- The weather conditions encountered in the final phase of the flight may have aggravated the level of tension in the aircraft cabin to the point of compromising the management of the situation by the pilot, who delegated responsibility for radiotelephony communication to a passenger.
- If one considers that the pilot may have decided to descend below the minimum safe altitude in order to achieve visual conditions, one may suppose that his decision, probably influenced by the experience of the preceding aircraft, was made without adequate evaluation of the risks involved, and without considering the option of flying IFR, in face of the local meteorological conditions. In addition, the pilot’s decision-making process may have been compromised by lack of information on Mount Santo Antonio in the approach chart.
- The primary radar images obtained by Anápolis Control (APP-AN) indicated the presence of thick nebulosity associated with heavy cloud build-ups on the final approach of the VOR procedure. Such meteorological conditions influenced the occurrence, which culminated in the collision of the aircraft with Mount Santo Antônio, independently of the hypotheses raised during the investigation.
- The final approach on the course 320º, instead of 325º, made the aircraft align with the hill with which it collided.
- Mount Santo Antonio, a control obstacle on the final approach in which the collision occurred, was not depicted in the runway 32 VOR procedure approach chart, in discordance with the prescriptions of the CIRTRAF 100-30, a fact that may have contributed to a possible decrease of the situational awareness.
Final Report:

Crash of a Piper PA-46-350P Malibu Mirage near Westcliffe: 2 killed

Date & Time: Jan 9, 2011 at 1340 LT
Registration:
N727MC
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Phoenix – Pueblo
MSN:
46-36085
YOM:
1997
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3030
Captain / Total hours on type:
467.00
Aircraft flight hours:
3734
Circumstances:
While en route to the destination airport, the pilot was issued a clearance to descend. As the airplane descended to the assigned altitude, radar plots depicted the airplane entering a right turn, climbing rapidly, and then descending rapidly in a spiral-like pattern. The airplane wreckage was found the following day in mountainous terrain. Several tall trees surrounded the perimeter of the wreckage. Many of the trees showed scuff marks down the trunks consistent with the airplane impacting the terrain in a near-vertical descent. All airplane components were accounted for at the accident site. A postaccident examination of the airplane showed no preimpact failures of the airframe or the engine. A weather analysis revealed that the airplane was descending in the immediate vicinity of a stationary front. The weather conditions in the area were conducive to the production of moderate to severe turbulence, mountain wave activity with updraft/downdrafts in excess of 750 feet per minute, and moderate icing. The radar data confirmed that the airplane began its rapid descent shortly after entering cumuliform clouds. The radar information along with the wreckage at the accident site was consistent with the pilot losing control while trying to maneuver the airplane in an area of turbulent weather.
Probable cause:
The pilot's loss of control following an encounter with moderate to severe weather.
Final Report:

Crash of a Piper PA-46-350P Malibu Mirage in Kumamoto: 2 killed

Date & Time: Jan 3, 2011 at 1714 LT
Operator:
Registration:
JA701M
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Kumamoto – Kitakyūshū
MSN:
46-36188
YOM:
1999
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1537
Captain / Total hours on type:
119.00
Aircraft flight hours:
1497
Circumstances:
The single engine aircraft departed Kumamoto Airport runway 07 at 1711LT on a private flight to Kitakyūshū, with two persons on board: a PIC in the left seat and a passenger in the right seat. At 17:12:11, the radar of the Kumamoto aerodrome station C captured the aircraft. The pilot made a position report at 6 nm north of the airport at 2,300 feet. While climbing to the altitude of 6,500 feet, the pilot was instructed to change the frequency. About three minutes after takeoff, the aircraft collided with trees and crashed in a wooded area located on the southeast slope of Mt Yago, about 14 km northeast of Kumamoto Airport. The wreckage was found in the afternoon of the following day at an altitude of 850 metres. The aircraft was destroyed and both occupants were killed, Mr. & Mrs. Hiroshi and Hiromi Kanda.
Probable cause:
It is highly probable that the aircraft collided with the mountain slope during its in-cloud post-takeoff climb with low climb rate on its VFR flight to Kitakyushu Airport from Kumamoto Airport, resulting in the aircraft destruction and fatal injuries of two persons on board–the PIC and the passenger. It is somewhat likely that the contributing factor to in-cloud flight toward mountain slope with low climb rate is the PIC’s lack of familiarization with terrain features near Kumamoto Airport; however, the JTSB was unable to clarify the reason.
Final Report:

Crash of a Rockwell Grand Commander 680FL near Perris: 1 killed

Date & Time: Dec 20, 2010 at 1000 LT
Registration:
N316KW
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Palm Springs - Chino
MSN:
680-1753-146
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
33000
Aircraft flight hours:
2278
Circumstances:
The pilot departed the airport mid-morning to fly to his home airport, 63 miles to the northwest. Weather conditions at the departureb airport were visual flight rules (VFR), the weather at the destination airport was not reported, and the weather conditions en-route were marginal VFR. The global positioning system (GPS) track for the flight indicated that the airplane departed from the airport and headed west along a highway corridor flying approximately 1,000 feet above ground level (agl) through a mountain pass. For the majority of the flight, the airplane maintained altitudes between 900 feet and 1,200 feet agl. Twenty-nine minutes after takeoff, the airplane’s GPS track turned southwest away from an area of concentrated precipitation and directly towards an isolated mountain peak that rose approximately 1,000 feet above the surrounding terrain. The pilot contacted the local air traffic control facility, reported his position and requested traffic advisories through the local airspace to his destination airport. About 6 minutes later, the pilot stated that he was having difficulty maintaining VFR and asked for an instrument flight rules (IFR)clearance. At the same time, the GPS track showed that the airplane came within 50 feet of the mountainous terrain. No further transmissions from the pilot were received. The final GPS position was recorded 1 minute later, at 500 feet agl and approximately half a mile from the crash site. The terrain rapidly ascended in this area and intersected the airplane's flight path over the remaining 1/2 mile. An airport located about 4 miles from the accident site and in an area of flat terrain 1,000 feet below the isolated mountain top, recorded weather at the time of the accident as few clouds at 900 feet agl, overcast clouds at 1,500 feet agl, and a variable ceiling between 1,200 and 1,800 feet agl, in drizzle. Weather radar images at the time of the accident depicted precipitation at the elevation and location of the accident site, indicating probable mountain obscuration.
Probable cause:
The pilot’s decision to continue visual flight into instrument meteorological conditions, which resulted in an in-flight collision with mountainous terrain.
Final Report:

Crash of a Beechcraft B60 Duke in Edwards: 2 killed

Date & Time: Dec 15, 2010 at 1602 LT
Type of aircraft:
Registration:
N571M
Flight Type:
Survivors:
No
Site:
Schedule:
Pueblo - Eagle
MSN:
P-534
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1300
Aircraft flight hours:
2456
Circumstances:
The air traffic controller had cleared the flight for the instrument approach and the pilot acknowledged the clearance. Radar data depicted the airplane turning toward the final approach course and then continuing the turn 180 degrees before disappearing from radar at 11,200 feet. The wreckage was located at an elevation of 10,725 feet. Examination of the terrain and ground scars indicated the airplane impacted terrain in a nose down, right turn. Impact forces and a postimpact fire resulted in substantial damage to the airplane. Examination of the airplane, engines, and de-icing systems revealed no mechanical anomalies. Weather at the time of the accident was depicted as overcast skies, reduced visibility, with snow showers in the area. An icing probability chart depicted a probability of moderate rime and mixed icing. Both AIRMETs and SIGMENTs advised of moderate icing between the freezing level and flight level 220 and occasional severe rime and mixed icing below 16,000 feet. During his weather briefing, the pilot stated that he was aware of the adverse weather conditions.
Probable cause:
Controlled flight into terrain, while on an instrument approach in instrument meteorological conditions, for undetermined reasons.
Final Report: