Crash of a Cessna 207A Skywagon in Tuluksak

Date & Time: Sep 3, 2010 at 1830 LT
Operator:
Registration:
N9942M
Flight Phase:
Survivors:
Yes
Schedule:
Tuluksak - Bethel
MSN:
207-0756
YOM:
1983
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4545
Captain / Total hours on type:
245.00
Aircraft flight hours:
29550
Circumstances:
Shortly after take off from runway 20, aircraft hit tree tops, stalled and crashed in a wooded area near the airport. Both passenger were slightly injured while the pilot was seriously injured. Aircraft was damaged beyond repair. The director of operations for the operator stated that soft field conditions and standing water on the runway slowed the airplane during the takeoff roll. The airplane did not lift off in time to clear trees at the end of the runway and sustained substantial damage to both wings and the fuselage when it collided with the trees. The pilot reported that he used partial power at the beginning of the takeoff roll to avoid hitting standing water on the runway with full power. After passing most of the water, he applied full power, but the airplane did not accelerate like he thought it would. He recalled the airplane being in a nose-high attitude and the main wheels bouncing several times before the airplane impacted the trees at the end of the runway.
Probable cause:
The pilot's delayed application of full power during a soft/wet field takeoff, resulting in a collision with trees during takeoff.
Final Report:

Crash of a Cessna 550 Citation II in Bwagaoia: 4 killed

Date & Time: Aug 31, 2010 at 1615 LT
Type of aircraft:
Registration:
P2-TAA
Survivors:
Yes
Schedule:
Port Moresby – Bwagaoia
MSN:
550-0145
YOM:
1980
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
14591
Copilot / Total flying hours:
872
Aircraft flight hours:
14268
Circumstances:
The aircraft was conducting a charter flight from Jackson’s International Airport, Port Moresby, National Capital District, Papua New Guinea (PNG), to Bwagaoia Aerodrome, Misima Island, Milne Bay Province, PNG (Misima). There were two pilots and three passengers on board for the flight. The approach and landing was undertaken during a heavy rain storm over Bwagaoia Aerodrome at the time, which resulted in standing water on the runway. This water, combined with the aircraft’s speed caused the aircraft to aquaplane. There was also a tailwind, which contributed the aircraft to landing further along the runway than normal. The pilot in command (PIC) initiated a baulked landing procedure. The aircraft was not able to gain flying speed by the end of the runway and did not climb. The aircraft descended into terrain 100 m beyond the end of the runway. The aircraft impacted terrain at the end of runway 26 at 1615:30 PNG local time and the aircraft was destroyed by a post-impact, fuel-fed fire. The copilot was the only survivor. Other persons who came to assist were unable to rescue the remaining occupants because of fire and explosions in the aircraft. The on-site evidence and reports from the surviving copilot indicated that the aircraft was serviceable and producing significant power at the time of impact. Further investigation found that the same aircraft and PIC were involved in a previous landing overrun at Misima Island in February 2009.
Probable cause:
Contributing safety factors:
• The operator’s processes for determining the aircraft’s required landing distance did not appropriately consider all of the relevant performance factors.
• The operator’s processes for learning and implementing change from the previous runway overrun incident were ineffective.
• The flight crew did not use effective crew resource management techniques to manage the approach and landing.
• The crew landed long on a runway that was too short, affected by a tailwind, had a degraded surface and was water contaminated.
• The crew did not carry out a go-around during the approach when the visibility was less than the minimum requirements for a visual approach.
• The baulked landing that was initiated too late to assure a safe takeoff.
Other safety factors:
• The aircraft aquaplaned during the landing roll, limiting its deceleration.
• The runway surface was described as gravel, but had degraded over time.
• The weather station anemometer was giving an incorrect wind indication.
Final Report:

Crash of a De Havilland DHC-2 Beaver in the Kaminshak Bay: 4 killed

Date & Time: Aug 21, 2010 at 1412 LT
Type of aircraft:
Operator:
Registration:
N9313Z
Flight Phase:
Survivors:
No
Schedule:
Swikshak Lagoon - King Salmon
MSN:
441
YOM:
1953
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4112
Aircraft flight hours:
4946
Circumstances:
The commercial pilot departed a remote, oceanside lagoon in a float-equipped airplane with three passengers on an on-demand air taxi flight in reduced visibility and heavy rain. When the airplane did not reach its destination, the operator reported the airplane overdue. Extensive search-and-rescue efforts along the coast and inland failed to find the wreckage. After the search ended, small portions of the fragmented airplane washed ashore about 28 miles northeast of the departure lagoon. The remainder of wreckage has not been located despite sonar searches of the ocean near where the wreckage was found. A stowed tent and duffel bag, which were reported to be aboard the airplane, were also found ashore near the wreckage location. The tent and duffel bag exhibited evidence of exposure to a high temperature environment, such as a fire. However, there was no evidence indicating that the fire occurred in flight. The lack of soot on the undamaged areas of the items, as well as the very abrupt demarcation line between the damaged portion and the undamaged material, is consistent with these items floating in the water and being exposed to a fuel fire on the surface of the water, rather than having been exposed to a fire in the airplane’s cargo compartment. Due to the fragmentation of the recovered wreckage, it is likely that the airplane collided with ocean’s surface while in flight; however, because the engine and a majority of the wreckage have not been found, the sequence of events leading to the accident could not be determined.
Probable cause:
Undetermined.
Final Report:

Crash of a De Havilland DHC-2 Beaver in La Grande: 2 killed

Date & Time: Jul 24, 2010 at 1053 LT
Type of aircraft:
Operator:
Registration:
C-FGYK
Flight Phase:
Survivors:
Yes
Schedule:
La Grande - Lac Eau Claire
MSN:
123
YOM:
1951
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3800
Captain / Total hours on type:
1000.00
Aircraft flight hours:
23808
Circumstances:
At approximately 1053 Eastern Daylight Time, de Havilland DHC-2 Mk. 1 amphibious floatplane (registration C-FGYK, serial number 123), operated by Nordair Québec 2000 Inc., took off from runway 31 at La Grande-Rivière Airport, Quebec, for a visual flight rules flight to l’Eau Claire Lake, Quebec, about 190 nautical miles to the north. The take-off run was longer than usual. The aircraft became airborne but was unable to gain altitude. At the runway end, at approximately 50 feet above ground level, the aircraft pitched up and banked left. It then nosed down and crashed in a small shallow lake. The pilot and 1 front-seat passenger were fatally injured and the 3 rear-seat passengers sustained serious injuries. The aircraft broke up on impact, and the forward part of the cockpit was partly submerged. The emergency locator transmitter activated on impact.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The aircraft was overloaded and its centre of gravity was beyond the aft limit. The aircraft pitched up and stalled at an altitude that did not allow the pilot to execute the stall recovery manoeuvre.
2. The baggage was not secured. Shifting of the baggage caused the triple seat to pivot forward, propelling the 3 rear-seat passengers against the pilot and front-seat passenger during impact.
3. Although the design of the triple seat met aviation standards, it separated from the floor at the time of impact, principally due to the fact that the heavy cargo shifted.
4. The action taken by TC did not have the desired outcomes to ensure regulatory compliance; consequently, unsafe practices persisted.
Finding as to Risk:
1. Operating an aircraft outside the limits and conditions under which a permit is issued can increase the risk of an accident
Final Report:

Crash of a De Havilland DHC-2 Beaver near Chute des Passes: 4 killed

Date & Time: Jul 16, 2010 at 1117 LT
Type of aircraft:
Operator:
Registration:
C-GAXL
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Lac des Quatre - Lac Margane
MSN:
1032
YOM:
1957
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
11500
Captain / Total hours on type:
9000.00
Aircraft flight hours:
17204
Circumstances:
The float-equipped de Havilland Beaver DHC-2 Mk.I (registration number C-GAXL, serial number 1032), operated by Air Saguenay (1980) Inc., was flying under visual flight rules from Lac des Quatre to Lac Margane, Quebec, with 1 pilot and 5 passengers on board. A few minutes after take-off, the pilot reported intentions of making a precautionary landing due to adverse weather conditions. At approximately 1117, Eastern Daylight Time, the aircraft hit a mountain, 12 nautical miles west-south-west of the southern part of Lac Péribonka. The aircraft was destroyed and partly consumed by the fire that broke out after the impact. The pilot and 3 passengers were killed; 1 passenger sustained serious injuries and 1 passenger sustained minor injuries. No ELT signal was received.
Probable cause:
Causes and Contributing Factors:
1. The pilot took off in weather conditions that were below the minimum for visual flight rules, and continued the flight in those conditions.
2. After a late decision to carry out a precautionary alighting, the pilot wound up in instrument meteorological conditions (IMC). Consequently, the visual references were reduced to the point of leading the aircraft to controlled flight into terrain (CFIT).
3. The passenger at the rear of the aircraft was not seated on a seat compliant with aeronautical standards. The passenger was ejected from the plane at the moment of impact, which diminished his chances of survival.
Findings as to Risk:
1. The lack of training on pilot decision-making (PDM) for air taxi operators exposes pilots and passengers to increased risk when flying in adverse weather conditions.
2. In view of the absence of an ELT signal and the operator’s delay in calling, search efforts were initiated more than 3 ½ hours after the accident. That additional time lag can influence the seriousness of injuries and the survival of the occupants.
Final Report:

Crash of a Cessna 550 Citation Bravo in Brač

Date & Time: Jul 15, 2010 at 1646 LT
Type of aircraft:
Operator:
Registration:
YU-BSG
Survivors:
Yes
Schedule:
Tirana – Brač
MSN:
550-1049
YOM:
2003
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
3427
Aircraft flight cycles:
2661
Circumstances:
Following an uneventful flight from Tirana, the crew started the approach to Brač Airport in good weather conditions. After landing on runway 04, the crew started the braking procedure but the aircraft was unable to stop within the remaining distance. It overran, went through a fence, lost its undercarriage and came to rest in a rocky area, bursting into flames. All five occupants escaped uninjured while the aircraft was partially destroyed by a post crash fire.
Probable cause:
Wrong approach configuration on part of the crew who landed too far down the runway, reducing the landing distance available. The following contributing factors were identified:
- Excessive speed on approach (the IAS was 143 knots upon touchdown),
- The crew completed the approach in a too steep descent,
- Incorrect flare which caused the aircraft to land too dar down the runway,
- Insufficient landing distance available,
- The crew failed to initiate a go-around procedure.
Final Report:

Crash of a De Havilland DHC-2 Beaver in Kukaklek Lake

Date & Time: Jun 27, 2010 at 1730 LT
Type of aircraft:
Operator:
Registration:
N9RW
Flight Phase:
Survivors:
Yes
Schedule:
Kukaklek Lake - Kukaklek Lake
MSN:
1095
YOM:
1957
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5000
Captain / Total hours on type:
2000.00
Circumstances:
The commercial pilot was taking off on a passenger flight in conjunction with a remote lodge operation under Title 14, CFR Part 91. The pilot said he picked up passengers in the float-equipped airplane on a beach, and water-taxied out into the lake for takeoff. He said he taxied out about 1,200 feet, reversed course into the wind, and initiated a takeoff. He said when the airplane reached his predetermined abort point, the airplane was still on the water, and might not lift off in time to avoid the terrain ahead. The pilot said rather than abort the takeoff he elected to apply full power and continue the takeoff. He said the airplane collided with the bank, and nosed over. The pilot said there were no preaccident mechanical anomalies with the airplane. The owner of the company said the lake was about 1 mile wide where the pilot elected to takeoff. He said the airplane received substantial damage to the wings and fuselage. He also said the passengers related to him that the engine sounded fine, but they did not think the pilot taxied out very far into the lake.
Probable cause:
The pilot's decision to use only a portion of the available takeoff area, which resulted in a collision with terrain during takeoff.
Final Report:

Crash of a Beechcraft A100 King Air in Québec: 7 killed

Date & Time: Jun 23, 2010 at 0559 LT
Type of aircraft:
Operator:
Registration:
C-FGIN
Flight Phase:
Survivors:
No
Schedule:
Québec - Seven Islands - Natashquan
MSN:
B-164
YOM:
1973
Flight number:
APO201
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
3046
Captain / Total hours on type:
372.00
Copilot / Total flying hours:
2335
Copilot / Total hours on type:
455
Aircraft flight hours:
19665
Aircraft flight cycles:
16800
Circumstances:
Aircraft was making an instrument flight rules flight from Québec to Sept-Îles, Quebec. At 0557 Eastern Daylight Time, the crew started its take-off run on Runway 30 at the Québec/Jean Lesage International Airport; 68 seconds later, the co-pilot informed the airport controller that there was a problem with the right engine and that they would be returning to land on Runway 30. Shortly thereafter, the co-pilot requested aircraft rescue and fire-fighting (ARFF) services and informed the tower that the aircraft could no longer climb. A few seconds later, the aircraft struck the ground 1.5 nautical miles from the end of Runway 30. The aircraft continued its travel for 115 feet before striking a berm. The aircraft broke up and caught fire, coming to rest on its back 58 feet further on. The 2 crew members and 5 passengers died in the accident. No signal was received from the emergency locator transmitter (ELT).
Probable cause:
Findings as to Causes and Contributing Factors:
1. After the take-off at reduced power, the aircraft performance during the initial climb was lower than that established at certification.
2. The right engine experienced a problem in flight that led to a substantial loss of thrust.
3. The right propeller was not feathered; therefore, the rate of climb was compromised by excessive drag.
4. The absence of written directives specifying which pilot was to perform which tasks may have led to errors in execution, omissions, and confusion in the cockpit.
5. Although the crew had the training required by regulation, they were not prepared to manage the emergency in a coordinated, effective manner.
6. The priority given to ATC communications indicates that the crew did not fully understand the situation and were not coordinating their tasks effectively.
7. The impact with the berm caused worse damage to the aircraft.
8. The aircraft’s upside-down position and the damage it sustained prevented the occupants from evacuating, causing them to succumb to the smoke and the rapid, intense fire.
9. The poor safety culture at Aéropro contributed to the acceptance of unsafe practices.
10. The significant measures taken by TC did not have the expected results to ensure compliance with the regulations, and consequently unsafe practices persisted.
Findings as to Risk:
1. Deactivating the flight low pitch stop system warning light or any other warning system contravenes the regulations and poses significant risks to flight safety.
2. The maintenance procedures and operating practices did not permit the determination of whether the engines could produce the maximum power of 1628 ft-lb required at take-off and during emergency procedures, posing major risks to flight safety.
3. Besides being a breach of regulations, a lack of rigour in documenting maintenance work makes it impossible to determine the exact condition of the aircraft and poses major risks to flight safety.
4. The non-compliant practice of not recording all defects in the aircraft journey log poses a safety risk because crews are unable to determine the actual condition of the aircraft at all times, and as a result could be deprived of information that may be critical in an emergency.
5. The lack of an in-depth review by TC of SOPs and checklists of 703 operators poses a safety risk because deviations from aircraft manuals are not detected.
6. Conditions of employment, such as flight hours–based remuneration, can influence pilots’ decisions, creating a safety risk.
7. The absence of an effective non-punitive and confidential voluntary reporting system means that hazards in the transportation system may not be identified.
8. The lack of recorded information significantly impedes the TSB’s ability to investigate accidents in a timely manner, which may prevent or delay the identification and communication of safety deficiencies intended to advance transportation safety.
Final Report:

Crash of a Douglas DC-3C in Berlin

Date & Time: Jun 19, 2010 at 1447 LT
Type of aircraft:
Operator:
Registration:
D-CXXX
Flight Phase:
Survivors:
Yes
Schedule:
Berlin - Berlin
MSN:
16124/32872
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft departed Berlin-Schönefeld Airport on a local 35-minute sightseeing flight over Berlin with 25 passengers and three crew members on board. Shortly after takeoff, while in initial climb, the pilots encountered technical problems with the right engine and elected to make an emergency landing. The aircraft struck the airport boundary fence then crash landed on its belly with its right wing partially torn off. All 28 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Loss of power on the right engine for unknown reasons.

Crash of a Casa 212 Aviocar 100 near Mintom: 11 killed

Date & Time: Jun 19, 2010 at 1000 LT
Type of aircraft:
Operator:
Registration:
TN-AFA
Flight Phase:
Survivors:
No
Schedule:
Yaoundé - Yangadou
MSN:
151
YOM:
1979
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
The aircraft departed Yaoundé-Nsimalen Airport at 0913LT on a charter flight to Yangadou, a small airstrip serving several iron mines in north Congo. At 0951LT, the crew made its last radio contact with ATC then the aircraft disappeared from radar screens. The wreckage was found around 1700LT on June 21 near Mintom. The aircraft was totally destroyed and all 11 occupants were killed, among them Ken Talbot, an Australian investor in iron business. The flight was conducted for the Cameroon company Cam Iron, a subcontractor of the Australian Sundance Resources Group.