Crash of a Let L-410UVP in Butembo

Date & Time: Oct 30, 2012 at 1500 LT
Type of aircraft:
Operator:
Registration:
9Q-CAZ
Survivors:
Yes
Schedule:
Goma - Butembo
MSN:
79 02 05
YOM:
1979
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Goma, the twin engine airplane landed on runway 14/32 which is 770 metres long. After touchdown, the aircraft was unable to stop within the remaining distance. It overran, lost its left main gear and came to rest down an embankment with its left wing damaged. All 18 occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Cessna 560 Citation V in Edmonton

Date & Time: Oct 30, 2012 at 0633 LT
Type of aircraft:
Operator:
Registration:
C-FBCW
Flight Type:
Survivors:
Yes
Schedule:
Edmonton - Edmonton
MSN:
560-0191
YOM:
1992
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft departed Edmonton-City Centre Airport in the early morning on a positioning flight to Edmonton-Intl, carrying two pilots. En route, the crew encountered IMC conditions with moderate icing and the deicing systems were activated. For unknown reasons, the aircraft landed hard on runway 02, causing the right main gear to collapse. The aircraft veered off runway to the right and came to rest in a grassy area. Both pilots escaped with minor injuries and the aircraft was damaged beyond repair.

Crash of a Beechcraft 1900D in Bir Kalait

Date & Time: Oct 28, 2012
Type of aircraft:
Registration:
TT-ABB
Flight Type:
Survivors:
Yes
Schedule:
N'Djamena - Bir Kalait
MSN:
UE-406
YOM:
2000
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft departed N'Djamena on a flight to Bir Kalait, carrying 15 passengers and two pilots, among them a delegation of the Presidency. On short final, the aircraft named 'Am Djerass' was too low and struck the ground short of runway threshold. Upon impact, the undercarriage were torn off. The aircraft slid on its belly for about 200 metres before coming to rest in a sandy area with all propeller blades separated. The aircraft was damaged beyond repair but all 17 occupants escaped uninjured, among the Idriss Déby, President of the Tchad Republic who was flying to Bir Kalait to take part to the Peace and Development Forum for the Borku-Ennedi-Tibesti Region.

Crash of a Cessna 208B Grand Caravan in Yola

Date & Time: Oct 25, 2012 at 1830 LT
Type of aircraft:
Operator:
Registration:
5N-BMJ
Flight Type:
Survivors:
Yes
Schedule:
Jalingo – Yola
MSN:
208B-2098
YOM:
2009
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
999
Circumstances:
On the 25th of October, 2012 at 17: 48 h, a Cessna Caravan 208B, 5N-BMJ, departed Jalingo for Yola on a Visual Flight Rules (VFR) flight plan with four Persons-On-Board (one crew and three passengers). At 18:00 h, the Airport Manager stationed at Jalingo by Taraba State Government, called Yola Control Tower (CT) by phone to advise that the aircraft had departed Jalingo for Yola. At 18:25 h the pilot reported field in sight. CT then advised him to “continue approach and report final, wind calm” and the pilot acknowledged “will continue approach, to report final”. At 18:27 h CT had the aircraft in sight and advised the pilot to report “final, wind calm”, the pilot acknowledged. At 18:30 h, CT lost visual contact with 5N-BMJ and tried to raise her on radio but there was no response. At 18:37 h, information was received from witnesses, regarding a possible plane crash at Yola-Numan road close to Nigerian National Petroleum Corporation (NNPC) depot. This information was subsequently passed to the fire watch room. Rescue team and other security personnel were mobilized to the location of the crash. However, before the arrival of the rescue team from the airport, the locals had rescued the occupants from the wreckage. The occupants were subsequently taken to Federal Medical Centre (FMC), Yola for medical treatment. The accident occurred at dusk. The aircraft was destroyed.
Probable cause:
The Bureau could not conclusively determine the cause of this accident; however, the investigation identified the following factors:
- The pilot was not certified, qualified and not competent to fly the aircraft.
- The decision of the pilot to operate a VFR flight after sunset.
- Inadequate oversight by the Regulatory Authority.
Final Report:

Crash of a Beechcraft B90 King Air in Sturtevant

Date & Time: Oct 22, 2012 at 1830 LT
Type of aircraft:
Registration:
N821DA
Flight Type:
Survivors:
Yes
Schedule:
Jackson - Sturtevant
MSN:
LJ-406
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2331
Captain / Total hours on type:
1425.00
Aircraft flight hours:
12637
Circumstances:
The aircraft collided with a fence and a ditch when it overran runway 8R (2,272 feet by 38 feet, asphalt) while landing at the Sylvania Airport (C89), Sturtevant, Wisconsin. The commercial pilot was not injured and his passenger received minor injuries. The airplane sustained damage to its fuselage and both wings. The airplane was registered to Direct Action Aviation LLC, and was operated by Skydive Midwest. The accident flight was conducted under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Instrument meteorological conditions prevailed for the flight, which was not operated on a flight plan. The flight originated from the Jackson County Airport-Reynolds Field (JXN), Jackson, Michigan, about 1800. The pilot reported that the landing approach was normal and when the airplane crossed the runway threshold it floated and he pulled the engine power levers to the stops. He stated that although he did not remember the airplane bouncing, his passenger told him that it had. He pulled the power levers to reverse, but there was no immediate reverse thrust. He applied brakes and felt the airplane accelerate. He recognized that he would not be able to stop the airplane on the remaining runway and attempted to steer it to the north. The airplane left the runway, impacted two ditches and came to rest on a highway. The pilot stated that he should have recognized that braking action would be significantly reduced with the possibility of hydroplaning, that pulling the power levers to the stops before touchdown induced a lag in realization of reverse thrust, and that he should have executed a go-around when the airplane floated before landing. The pilot reported no mechanical failures or malfunctions of the airplane. At 1853, weather conditions reported at the Kenosha regional Airport (ENW), located 6 miles south of the accident site, included heavy rain.
Probable cause:
The pilot's decision to continue the landing after touching down long and on a wet runway that reduced the airplane’s braking capability, which resulted in an overrun.
Final Report:

Crash of an Antonov AN-12TB in Shindand

Date & Time: Oct 19, 2012 at 1800 LT
Type of aircraft:
Operator:
Registration:
EK-12112
Flight Type:
Survivors:
Yes
MSN:
01 347 907
YOM:
1971
Location:
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The four engine aircraft was completing a cargo flight to the Shindand AFB, carrying a load of 4'700 pounds of voting documents intended to the US soldiers based at Shindand AFB. For unknown reasons, the aircraft landed hard and bounced. On the second touchdown, the left main gear was torn off. The aircraft slid for about 1,750 metres then veered off runway to the left and came to rest in a drainage ditch. While all six occupants escaped uninjured, the aircraft was destroyed by impact and a post impact fire. US Federal Voting Assistance Program published a notice on 24OCT2012, informing that mail consisted of voting documents for US soldiers covering the US Presidential Election of 06NOV2012.

Crash of a McDonnell Douglas MD-11F in Campinas

Date & Time: Oct 13, 2012 at 1852 LT
Type of aircraft:
Operator:
Registration:
N988AR
Flight Type:
Survivors:
Yes
Schedule:
Miami - Campinas
MSN:
48434/476
YOM:
1991
Flight number:
CWC425
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12900
Copilot / Total flying hours:
5198
Copilot / Total hours on type:
1368
Circumstances:
The airplane took off from Miami International Airport (KMIA), destined for Viracopos Airport (SBKP), with two pilots and a mechanic on board, on a non-regular cargo transport flight. The flight was uneventful up to the moment its landing in SBKP. On the approach for landing on runway 15, the crew performed the IFR ILS Z procedure. The weather conditions were VMC, with the wind coming from 140º at 19kt. When the aircraft was granted clearance to land, the wind strength was 20kt, gusting up to 29kt. The copilot was the Pilot Flying (PF), and the captain was the Pilot Monitoring (PM) at the moment of landing. When the aircraft touched down on the runway after the flare, the left main landing gear collapsed, causing the aircraft to skid on the runway for approximately 800 meters before stopping. There was substantial damage to the left main gear assembly, to the left wing, and left engine. The aircraft stopped within the runway limits. All three crew members were uninjured.
Probable cause:
It was determined that the “the landing gear failed due to overload in the cylinder structure”. The fracture started in the rear section of the cylinder in a connection hole which served as a tension concentration point, and ended in the front part of the cylinder with its breakage into two parts. Following a failure of the right main gear upon landing in Montevideo on 20 October 2009, the right main landing gear was replaced by VARIG Engineering & Maintenance (VEM), but the organization responsible for the research of damage, the specification of the services necessary for the restoration of airworthiness, and the provision of the services that enabled the restoration of the aircraft to an airworthy condition was not identified. The same aircraft parts were subjected to metallurgical analysis at the Boeing Long Beach Materials, Processing and Physics [MP&P] Laboratories, in Huntington Beach, California, USA; and the technical report issued by Boeing highlighted that in one of the points of origin of the failure, the analysis had identified characteristics similar to a pre-crack point, which would have begun earlier, probably due to overload. In the tasks that led to the restoration of the aircraft airworthiness after the accident in Uruguay in 2009 (Hard-Landing), and also in subsequent periodic inspections, the existence of pre-crack traces resulting from a previous overload condition may not have been identified, something that could have resulted in a point of stress concentration.
Final Report:

Crash of a Beriev Be-12PS Chayka at Kacha NAS: 3 killed

Date & Time: Oct 12, 2012 at 1740 LT
Type of aircraft:
Operator:
Registration:
18 yellow
Flight Type:
Survivors:
Yes
Schedule:
Kacha NAS - Kacha NAS
MSN:
3602903
YOM:
1969
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was performing a training mission off the Crimea coast on behalf of the Black Sea Fleet. En route, an engine failed, forcing the crew to return to Kacha NAS. On short final, the airplane descended fast and landed hard, got airborne and climbed to several meters before stalling and crashing near the runway, bursting into flames. The captain, the copilot and the navigator were killed and the radio operator was seriously injured. The aircraft was destroyed by impact forces and a post impact fire. The antisubmarine seaplane was also registered RF-12008.
Probable cause:
Engine failure for unknown reasons.

Crash of a Raytheon 390 Premier IA in New Delhi

Date & Time: Sep 22, 2012 at 1129 LT
Type of aircraft:
Operator:
Registration:
VT-UPN
Flight Type:
Survivors:
Yes
Schedule:
Lucknow - New Delhi
MSN:
RB-236
YOM:
2008
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft departed Lucknow Airport in the morning on a flight to New Delhi-Indira Gandhi Airport with a crew of three (two pilot and a cabin crew) and three passengers, among them Shivpal Yadav, Minister by the Uttar Pradesh Government. Following an uneventful flight, the crew completed the approach to runway 27. After touch down, the left main gear collapsed and the aircraft slid on runway for about one km when the right main gear collapsed as well. Out of control, the aircraft veered off runway to the right and came to rest in a grassy area. All six occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Beechcraft Beechjet 400A in Macon

Date & Time: Sep 18, 2012 at 1003 LT
Type of aircraft:
Operator:
Registration:
N428JD
Survivors:
Yes
Schedule:
Charleston - Macon
MSN:
RJ-13
YOM:
1986
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7000
Captain / Total hours on type:
4000.00
Copilot / Total flying hours:
2500
Copilot / Total hours on type:
450
Aircraft flight hours:
5416
Circumstances:
The aircraft was substantially damaged when it overran runway 28 during landing at Macon Downtown Airport (MAC), Macon, Georgia. The airplane departed from Charleston Air Force Base/International Airport (CHS), Charleston, South Carolina, about 0930. Visual meteorological conditions prevailed and an instrument flight rules (IFR) flight plan was filed. Both Airline Transport Pilots (ATP) and one passenger sustained minor injuries. The airplane was owned by Dewberry, LLC and operated by The Aviation Department. The corporate flight was conducted under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91. According to an interview with the pilots, they arrived at DeKalb-Peachtree Airport (PDK), Atlanta, Georgia, which was their home base airport, about 0400, and then drove about 4 1/2 hours to CHS for the 0930 flight. The flight departed on time, the airspeed index bug was set on the co-pilot's airspeed for a decision takeoff speed (V1) of about 102 knots and a single engine climb speed (V2) on the pilot's side of 115 knots. The flight climbed to 16,000 feet prior to beginning the descent into MAC. When the flight was about 11 miles from the airport the flight crew visually acquired the airport and cancelled their IFR clearance with the Macon Radar Approach controller and proceeded to the airport visually. The second-in-command activated the runway lights utilizing the common traffic advisory frequency for the airport. Both crew members reported that about 3 seconds following activation of the lights and the precision approach path indicator (PAPI) lights, the PAPI lights turned off and would not reactivate. During the approach, the calculated reference speed (Vref) was 108 knots and was set on both pilots' airspeed indicator utilizing the index bug that moved around the outside face of the airspeed instrument. The landing was within the first 1,000 feet of the runway and during the landing roll out the airplane began to "hydroplane" since there was visible standing water on the runway and the water was "funneling into the middle." Maximum reverse thrust, braking, and ground spoilers were deployed; however, both pilots reported a "pulsation" in the brake system. The airplane departed the end of the runway into the grass, went down an embankment, across a road, and into trees. They further added that the airplane "hit hard" at the bottom of the embankment. They also reported that there were no mechanical malfunctions with the airplane prior to the landing. According to an eyewitness statement, a few minutes prior to the airplane landing, the airport experienced a rain shower with a "heavy downpour." The witness reported observing the airplane on approach, heard the engine thrust reverse, and then observed the airplane "engulfed in a large ball of water vapor." However, he did not observe the airplane as it departed the end of the runway. Another witness was located in a hangar on the west side of the airport and heard the airplane, looked outside and then saw the airplane with the reverse thrusters deployed. He watched it depart the end of the runway and travel into the nearby woods.
Probable cause:
The pilot’s failure to maintain proper airspeed, which resulted in the airplane touching down too fast on the wet runway with inadequate runway remaining to stop and a subsequent runway overrun. Contributing to the landing overrun were the flight crew members’ failure to correctly use the appropriate performance chart to calculate the runway required to stop on a contaminated runway and their general lack of proper crew resource management.
Final Report: