Crash of a Beechcraft C90B King Air in Kiev: 5 killed

Date & Time: Dec 9, 2007 at 1759 LT
Type of aircraft:
Operator:
Registration:
D-IBDH
Survivors:
No
Schedule:
Hradec Králové – Kiev
MSN:
LJ-1307
YOM:
1992
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
18200
Captain / Total hours on type:
900.00
Aircraft flight hours:
3257
Aircraft flight cycles:
3639
Circumstances:
The twin engine aircraft departed Hradec Králové on an exec flight to Kiev with four passengers and one pilot on board. On final approach to Kiev-Zhuliany Airport, the pilot encountered poor visibility (below minimums) and descended too fast and too low. On short final, at a speed of 220 knots, the aircraft impacted ground and crashed in a wasteland located 2,590 metres short of runway 08 and 48 metres to the right of its extended centerline. The aircraft was destroyed upon impact and all five occupants were killed, among them the CEO of the Czech company Minib that bought the aircraft last 28 November. According to Czech Authorities, the aircraft was to be transferred to the Czech Republic Registry within January 2008. At the time of the accident, the horizontal visibility was 900 metres and the vertical visibility was 100 feet due to low clouds.
Probable cause:
It was determined that the aircraft impacted ground after the pilot continued the approach in below minima weather conditions.
The following findings were identified:
- The pilot continued the descent below MDA until the aircraft impacted ground,
- Few seconds prior to the accident, ATC instructed twice the pilot to initiate a go-around procedure, but this was too late,
- The pilot was approaching the airport at an excessive speed and below the glide,
- Poor visibility due to low clouds (below minimums).
Final Report:

Crash of a Cessna 208B Super Cargomaster in Columbus: 2 killed

Date & Time: Dec 5, 2007 at 0651 LT
Type of aircraft:
Operator:
Registration:
N28MG
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Columbus - Buffalo
MSN:
208B-0732
YOM:
1999
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1310
Captain / Total hours on type:
200.00
Aircraft flight hours:
9936
Aircraft flight cycles:
9033
Circumstances:
The cargo flight was departing on its fourth flight leg of a five-leg flight in night instrument conditions, which included a surface observation of light snow and a broken ceiling at 500 feet above ground level (agl). One pilot who departed just prior to the accident flight indicated that moderate snow was falling and that he entered the clouds about 200 feet agl. The accident airplane's wings and tail were de-iced prior to departure. Radar track data indicated the accident flight was about 45 seconds in duration. An aircraft performance radar study indicated that the airplane reached an altitude of about 1,130 feet mean sea level (msl), or about 400 feet above ground level, about 114 knots with a left bank angle of about 29 degrees. The airplane descended and impacted the terrain at an airspeed of about 155 knots, a pitch angle of -16 degrees, a left roll angle of 22 degrees, and a descent rate of 4,600 feet per minute. The study indicated that the engine power produced by the airplane approximately matched the engine power values represented in the pilot's operating handbook. The study indicated that the required elevator deflections were within the available elevator deflection range, and that the center-of-gravity (CG) position did not adversely affect the controllability of the airplane. The study indicated that the load factor vectors, the forces felt by the pilot, could have produced the illusion of a climb, even when the airplane was in a descent. The inspection of the airframe and engine revealed no anomalies that would have precluded normal operation.
Probable cause:
The pilot's failure to maintain aircraft control and collision avoidance with terrain due to spatial disorientation. Contributing to the accident were the low cloud ceiling and night conditions.
Final Report:

Crash of a Beechcraft 60 Duke in Wilmington: 1 killed

Date & Time: Dec 4, 2007 at 0722 LT
Type of aircraft:
Operator:
Registration:
N105PP
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wilmington – Allentown
MSN:
P-105
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1080
Circumstances:
According to a witness, prior to arriving in the run-up area the pilot lowered the airplane's flaps. After the right flap fully extended, the flap key on the drive shaft inside the 90-degree drive assembly adapter fractured, in overload, in the direction of flap extension. Before takeoff, the pilot raised the flaps; however, with the fractured key, the right flap would have remained fully extended. The pilot could have identified this condition prior to takeoff, either visually or by means of the flap indicator, which received its input from the right flap actuator. The pilot subsequently took off, and the airplane turned left, but it is unknown at what point the pilot would have noted a control problem. The pilot climbed the airplane to 250 to 300 feet and allowed the airspeed to bleed off to where the airplane stalled and subsequently spun into the ground. Airplane manufacturer calculations revealed that the pilot should have been able to maintain control of the airplane at airspeeds over 70 knots. According to the pilot's operating handbook, the best two-engine angle of climb airspeed was 99 knots and the best two-engine rate of climb airspeed was 120 knots.
Probable cause:
The pilot's failure to maintain adequate airspeed during a split flap takeoff, which resulted in an aerodynamic stall. Contributing to the accident were the failure of the right flap drive mechanism and the pilot's failure to verify that both flaps were retracted prior to takeoff.
Final Report:

Crash of a Cessna 208B Grand Caravan in Corozal

Date & Time: Dec 4, 2007
Type of aircraft:
Operator:
Registration:
V3-HFS
Flight Phase:
Survivors:
Yes
Schedule:
Corozal – San Pedro
MSN:
208B-0579
YOM:
1996
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll on runway 25 at Corozal Airport, the pilot decided to abandon the takeoff procedure. Unable to stop within the remaining distance, the single engine aircraft overran, went through a fence and came to rest against trees. All 12 occupants escaped uninjured while the aircraft was damaged beyond repair.

Ground accident of an Airbus A340-642X in Toulouse

Date & Time: Nov 15, 2007 at 1710 LT
Type of aircraft:
Operator:
Registration:
F-WWCJ
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
856
YOM:
2007
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
24
Circumstances:
The aircraft registered F-WWCJ was tested at a fixed point at Toulouse-Blagnac Airport. The current mission consisted of various test' systems with airline technicians who had ordered the plane. It unfolded engines in operation without chocks wheel. At the end of these tests, after having stopped and inspected the engines, the technicians restarted them for a new fixed point at high power, to find the source of oil seeps. About three minutes after power-up, the aircraft began to moving forward. The technician in the left seat noticed the movement and informed the test technician in the right seat. The latter acted on the brakes located rudder pedals then released the parking brake. The DFDR then shows a release of the brake command with the rudder bar. As the plane continues to advance, he tried to deviate from his course using the steering wheel. The nose gear quickly got in the way as the plane accelerated. The plane struck an inclined blast wall. Its front part broke and flipped over to the other side. Thirteen seconds elapsed between the start of the aircraft's movement and the shock with the wall. The aircraft was destroyed and all nine occupants were injured, four seriously.
Probable cause:
The accident was due to completion without chocks and on all four engines at the same time of a test during which the thrust was close to the capacity of the parking brake. The lack of a system for detecting and correcting drifts while carrying ground tests, in a context of industrial pressure and permanent sales force, encouraged a test to be carried out outside of the established procedures. The surprise led the ground test technician to focus on the brakes; therefore, he did not think of reducing the engines thrust.
Final Report:

Crash of a Bombardier BD-700-1A11 Global Express 5000 in Fox Harbour

Date & Time: Nov 11, 2007 at 1434 LT
Operator:
Registration:
C-GXPR
Survivors:
Yes
Schedule:
Hamilton – Fox Harbour
MSN:
9211
YOM:
2006
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9188
Captain / Total hours on type:
64.00
Copilot / Total flying hours:
6426
Copilot / Total hours on type:
9
Aircraft flight hours:
92
Aircraft flight cycles:
26
Circumstances:
The aircraft, operated by Jetport Inc., departed Hamilton, Ontario, for Fox Harbour, Nova Scotia, with two crew members and eight passengers on board. At approximately 1434 Atlantic standard time, the aircraft touched down seven feet short of Runway 33 at the Fox Harbour aerodrome. The main landing gear was damaged when it struck the edge of the runway, and directional control was lost when the right main landing gear collapsed. The aircraft departed the right side of the runway and came to a stop 1000 feet from the initial touchdown point. All occupants evacuated the aircraft. One crew member and one passenger suffered serious injuries; the other eight occupants suffered minor injuries. The aircraft sustained major structural damage.
Probable cause:
Findings as to Risk:
1. Because aircraft EWH information is not readily available to pilots, crews may continue to conduct approaches with an aircraft mismatched to the visual glide slope indicator (VGSI) system, increasing the risk of a reduced TCH safety margin.
2. Due to limited knowledge of the various VGSI systems in operation and their limitations, flight crews will continue to follow visual guidance that might not provide for safe TCH.
3. Jetport did not develop an accurate company risk profile. This precluded identification of systemic safety deficiencies and development of appropriate mitigation strategies.
4. If adequate safety oversight of POC operators is not maintained by the regulator, or the delegated organization, especially during SMS implementation, there is an increased risk that safety deficiencies will not be identified.
5. The fact that the Canadian Business Aviation Association (CBAA) did not insist that milestones for SMS implementation and development be followed may result in some POC operators never reaching full SMS compliance.
6. If Transport Canada does not ensure that the CBAA fulfills its responsibilities for adequate oversight of the Canadian Aviation Regulations (CARs) subpart 604 community, safety deficiencies will not be identified and addressed.
7. The audit of Jetport’s SMS, conducted by the CBAA–accredited auditor, did not identify the deficiencies in the program or make any suggestions for improvement. Without a comprehensive audit of an operator’s SMS, deficiencies could exist resulting in the operator’s inability to implement an effective mitigation strategy.
8. Contrary to the recommendations made in the Transport Canada/CBAA feasibility studies, the CBAA did not have a quality assurance program for its audit process. As a result, there is a risk that the CBAA will fail to identify weaknesses in the POC audit program.
9. At the time of the accident, no one at Fox Harbour (CFH4) had been assigned responsibility for regular maintenance of the APAPI, therefore preventing timely identification of APAPI equipment misalignment.
10. Jetport’s risk analysis before the introduction of the Global 5000 did not identify the incompatibility between the EWH of the aircraft and the APAPI at CFH4.
11. Not wearing shoulder harnesses during landings and take-offs increases the potential risk of passenger injuries.
12. Passengers not wearing footwear could impede evacuation, increase the risk of injury, and reduce post-crash mobility and (potentially) survival.
Other Findings:
1. A SMS integrates sound risk management policies, practices, and procedures into day-to-day operations and, properly implemented, offers great potential to reduce accidents.
2. Contrary to its own assessment protocol, Transport Canada did not document its decision to close off the CBAA assessment even though the CBAA had not submitted an acceptable corrective action plan.
3. Depiction of the different types of VGSIs differs, depending on the publication.
Final Report:

Crash of an Airbus A340-642 in Quito

Date & Time: Nov 9, 2007 at 1706 LT
Type of aircraft:
Operator:
Registration:
EC-JOH
Survivors:
Yes
Schedule:
Madrid - Quito
MSN:
731
YOM:
2006
Flight number:
IB6463
Country:
Crew on board:
14
Crew fatalities:
Pax on board:
345
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14024
Captain / Total hours on type:
2375.00
Copilot / Total flying hours:
10095
Copilot / Total hours on type:
1742
Aircraft flight hours:
8704
Aircraft flight cycles:
965
Circumstances:
Following an uneventful flight from Madrid, the crew contacted Quito Approach at 1650LT and received descent instructions in preparation for an instrument approach no. 4 (VOR QIT DME/ILS) for runway 35. During the descent the crew were notified that preceding flights had reported braking action medium to poor. The flight crew selected auto braking to 'High'. At 17:05, the crew reported the runway in sight, after which the controller stated that the wind was 170° at 4 knots, the runway was wet and reported braking action was poor. The flight was cleared to land. The pilot in command, following the procedures established by Iberia, decided to leave the ILS glide path and captured the path of the PAPI lights. The aircraft touched down 200 metres past the threshold at a 3.09g side load. The spoilers deployed automatically and main gear tyres 3 and 8 blew. The flap lever was moved involuntarily by the copilot, from the full position to position 2. The crew applied full manual braking and select reverse thrust. The Auto Brake function failed, after which the crew disconnected the antiskid braking system and continued to apply manual braking. The aircraft passed the end of runway 35, with a ground speed of 90 knots, hit the ILS localizer and stopped 232 meters further. Passengers and crew were evacuated using the slide at door 2R, thirty minutes after the aircraft stopped. All occupants escaped uninjured while the aircraft was considered as damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the crew who decided to continue the approach to Quito Airport, knowing the poor runway conditions, poor weather conditions and the aircraft weight, and his failure to initiate a go-around procedure while forcing the aircraft to intercept the PAPI, causing the aircraft to be unstabilized.
Contributing factors:
- On the date of the incident, the crew did not have specific regulations and operating procedures (the briefing of the operator for the airport in Quito was inappropriate to the existent conditions).
- The fact that the crew still being experienced similar airports in Quito and had not experienced similar weather situations, circumstances that would have allowed a strategy of approximation consistent with the terms of this operation, in particular as regards:
- Calculations in flight for landing runway length,
- Minimum altitude to start the maneuver of changing the path of ILS to PAPI,
- Carrying out a very detailed briefing that allowed unwanted deviations on approach,
- The weather conditions existing at the time of landing (visibility, tail wind and moderate rain).

Crash of an Antonov AN-12TB in Khartoum: 2 killed

Date & Time: Nov 8, 2007 at 0807 LT
Type of aircraft:
Operator:
Registration:
ST-JUA
Flight Type:
Survivors:
Yes
Schedule:
Khartoum - Juba
MSN:
3 3 411 10
YOM:
1963
Flight number:
JUC700
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Aircraft flight hours:
11787
Aircraft flight cycles:
7220
Circumstances:
The four engine aircraft departed Khartoum-Haj Yusuf Airport at 0759LT on a cargo flight to Juba, carrying four crew members and a load of 11 tons of various goods. After takeoff, while climbing, the crew reported the failure of the engine n°3 and was cleared to return for an emergency landing. After touchdown, the aircraft went out of control, veered off runway and came to rest in the military area of the airport, bursting into flames. All four crew members were injured while two people on the ground were killed. The aircraft was destroyed by a post crash fire.
Probable cause:
Failure of the engine n°3 during initial climb following a bird strike.

Crash of a Beechcraft A100 King Air in Chino: 2 killed

Date & Time: Nov 6, 2007 at 0918 LT
Type of aircraft:
Operator:
Registration:
N30GC
Flight Phase:
Survivors:
No
Schedule:
Chino - Visalia
MSN:
B-177
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3136
Aircraft flight hours:
11849
Circumstances:
The reported weather at the time of the accident was calm winds, a 1/4-mile visibility in fog and a vertical visibility of 100 feet. Shortly after takeoff for the instrument-flight-rules flight, the airplane made a slight turn to the left and impacted the tops of 25-foot trees about a 1/2 mile from the runway. An enhanced ground proximity warning system was installed on the airplane and data extraction from the system indicated that the airplane achieved an initial positive climb profile with a slight turn to the left and then a descent. A witness reported hearing the crash and observed the right wing impact the ground and burst into flames. The airplane then cartwheeled for several hundred feet before coming to rest inverted. The airframe, engines, and propeller assemblies were inspected with no mechanical anomalies noted that would have precluded normal flight.
Probable cause:
The pilot's failure to maintain a positive climb rate during an instrument takeoff. Contributing to the accident was the low visibility.
Final Report:

Crash of a Cessna 340 in Garberville: 3 killed

Date & Time: Nov 6, 2007 at 0855 LT
Type of aircraft:
Operator:
Registration:
N5049Q
Survivors:
No
Schedule:
Redding – Garberville
MSN:
340-0016
YOM:
1971
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
18500
Aircraft flight hours:
7691
Circumstances:
The pilot arrived in the vicinity of his destination airport, which was located in a narrow river valley. The airport was located within a large area of Visual Flight Rules (VFR) conditions with clear skies and almost unlimited visibility, but the pilot discovered that the airport was covered by a localized dense layer of fog about 200 to 250 feet thick. There were no instrument approaches to the non-controlled airport. Witnesses reported that the pilot flew at low-level up the valley, and eventually entered the fog as the flight approached the airport. About one mile prior to reaching the airport, the pilot attempted to climb out of the valley, but the airplane began impacting trees on the rising terrain. The airplane eventually sustained sufficient damage from impacting the trees that it descended into the terrain. Post-accident inspection of the airframe and engines found no evidence of a mechanical failure or malfunction.
Probable cause:
The pilot's intentional visual flight rules (VFR) flight into instrument meteorological conditions (IMC), and his failure to maintain clearance from the trees and terrain during climb. Contributing to the accident were the weather conditions of fog and a low ceiling, and the mountainous/hilly terrain.
Final Report: