Crash of an Antonov AN-26B-100 in Balad: 34 killed

Date & Time: Jan 9, 2007 at 0702 LT
Type of aircraft:
Operator:
Registration:
ER-26068
Survivors:
Yes
Schedule:
Adana – Balad
MSN:
113 08
YOM:
1981
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
34
Circumstances:
The aircraft was performing a charter flight from Adana, Turkey, to Balad AFB (located 70 km north of Baghdad), carrying 30 workers coming from Moldova, Russia, Turkey and Ukraine, on behalf of the Turkish Company Kulak specialized in reconstruction projects. The aircraft departed Adana Airport at 0600LT for a 90 minutes flight. On approach, the crew encountered poor visibility due to foggy conditions. Unable to locate the runway, the captain decided to initiate a go-around procedure. Few minutes later, while attempting a second approach, the aircraft descended too low and crashed 2,5 km short of runway, bursting into flames. A passenger was seriously injured while 34 other occupants were killed.
Probable cause:
The cause of the accident and the exact position of the aircraft during the last segment could not be determined with certainty as the FDR was not in the aircraft at the time of the accident.

Crash of a Piper PA-61 Aerostar (Ted Smith 601) in Jamestown: 1 killed

Date & Time: Jan 8, 2007 at 0950 LT
Operator:
Registration:
N720Z
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Jamestown – Buffalo
MSN:
61-0592-7963262
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5531
Captain / Total hours on type:
753.00
Aircraft flight hours:
2783
Circumstances:
During the initial climb, a "throbbing or surging" sound was heard as the airplane departed in gusting wind conditions with a 600-foot ceiling and 1/2 mile visibility in snow. Moments later the airplane came "straight down" and impacted the ground. During examination of the wreckage, it was discovered that that the fuel selector switch for the right engine had been in the "X-FEED" position during the accident. Examination of documents discovered in the wreckage revealed, three documents pertaining to operation of an Aerostar. These documents consisted of two airplane flight manuals (AFMs) from two different manufacturers, and a checklist. Examination of the first of the AFMs revealed, that it had the name of both the pilot and the operator on the cover of the document. Further examination revealed that it had been published 4 years prior to the manufacture of the accident airplane, and contained information for a Ted Smith Aerostar Model 601P, which the operator had previously owned. This document contained no warnings regarding the use of the crossfeed system during takeoff. Examination of the second of the two AFMs found in the wreckage revealed that it was the Federal Aviation Administration (FAA) approved AFM for the accident airplane. Unlike the first AFM, the second AFM advised that the fuel selector "X-FEED" position should be used in "level coordinated flight only." It also advised that each engine fuel selector "must be in the ON position for takeoff, climb, descent, approach, and landing." It also warned that, if the airplane was not in a level coordinated flight attitude, "engine power interruptions may occur on one or both engines" when "X-FEED" is selected "due to unporting of the respective engine's fuel supply intake port." Review of the checklist contained in the FAA approved AFM for the Piper Aircraft Model 601P under "STARTING ENGINES," required a check of the crossfeed system prior to engine start by selecting each fuel selector to "ON," then selecting "X-FEED," and after verifying valve actuation and annunciator light illumination, returning the fuel selector to "ON." Additionally, under "BEFORE TAKEOFF" It also required that the fuel selectors be checked in the "ON" position, and that the "X-FEED" annunciator light was out, prior to takeoff. Examination of the pilot's checklist revealed that, it consisted of multiple pages inserted into plastic protective sleeves and included both typed, and hand written information. A review of the section titled "BEFORE TAKEOFF" revealed that the checklist item "Fuel Selectors - ON Position," which was listed in the AFM, had been omitted.
Probable cause:
The pilot's incorrect selection of the right engine fuel selector position, which resulted in fuel starvation of the right engine, a loss of the right engine's power, and a loss of control during initial climb. Contributing to the accident were the pilot's inadequate preflight planning and preparation, and his improper use of the manufacturer's published normal operating procedures.
Final Report:

Crash of a Beechcraft A100 King Air in Sandy Bay: 1 killed

Date & Time: Jan 7, 2007 at 2002 LT
Type of aircraft:
Operator:
Registration:
C-GFFN
Flight Type:
Survivors:
Yes
Schedule:
La Ronge – Sandy Bay
MSN:
B-190
YOM:
1974
Flight number:
TW350
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8814
Captain / Total hours on type:
449.00
Copilot / Total flying hours:
672
Copilot / Total hours on type:
439
Aircraft flight hours:
17066
Circumstances:
The aircraft departed La Ronge, Saskatchewan, at 1930 central standard time under instrument flight rules to Sandy Bay, with two flight crew members and two emergency medical technicians aboard. TW350 was operating under Part VII, Subpart 3, Air Taxi Operations, of the Canadian Aviation Regulations. At 1948, air traffic control cleared TW350 out of controlled airspace via the Sandy Bay Runway 05 non-directional beacon approach. The crew flew the approach straight-in to Runway 05 and initiated a go-around from the landing flare. The aircraft did not maintain a positive rate of climb during the go-around and collided with trees just beyond the departure end of the runway. All four occupants survived the impact and evacuated the aircraft. The captain died of his injuries before rescuers arrived. Both emergency medical technicians were seriously injured, and the first officer received minor injuries. The aircraft sustained substantial damage from impact forces and was subsequently destroyed by a post-impact fire. The accident occurred at 2002 during the hours of darkness.
Probable cause:
Findings as to Risk:
1. Some Canadian Air Regulations (CARs) subpart 703 air taxi and subpart 704 commuter operators are unlikely to provide initial or recurrent CRM training to pilots in the absence of a regulatory requirement to do so. Consequently, these commercial pilots may be unprepared to avoid, trap, or mitigate crew errors encountered during flight.
2. Transport Canada (TC) Prairie and Northern Region (PNR) management practices regarding the June 2006 replacement of the regional combined audit program, in order to manage safety management system (SMS) workload, did not conform to TC’s risk management decision-making policies. Reallocation of resources without assessment of risk could result in undetected regulatory non-compliance.
3. Although TC safety oversight processes identified the existence of supervisory deficiencies within TWA, the extent of the deficiencies was not fully appreciated by the PNR managers because of the limitations of the oversight system in place at that time.
4. It is likely that the National Aviation Company Information System (NACIS) records for other audits include inaccurate information resulting from data entry errors and wide use of the problematic audit tracking form, reducing the effectiveness of the NACIS as a management tracking system.
5. Self-dispatch systems rely on correct assessment of operational hazards by pilots, particularly in the case of unscheduled commercial service into uncertified aerodromes. Unless pilots are provided with adequate decision support tools, flights may be dispatched with defences that are less than adequate.
6. TWA King Air crews did not use any standard practice in applying cold temperature altitude corrections. Inconsistent application of temperature corrections by flight crews can result in reduction of obstacle clearance to less than the minimum required and reduced safety margins.
7. The practice of not visually verifying wind/runway conditions at aerodromes where this information is otherwise unavailable increases the risk of post-touchdown problems.
8. The company dispatched flights to Sandy Bay without a standard means for crews to deal with non-current altimeter settings. Use of non-current or inappropriate altimeter settings can reduce minimum obstacle clearance and safety margins.
9. The crew was likely unaware of their ¼ nautical mile (nm) error in the aircraft position in relation to the runway threshold resulting from use of the global positioning system (GPS). Unauthorized and informal use of the GPS by untrained crews during instrument flight rules (IFR) approaches can introduce rather than mitigate risk.
10. Widespread adaptations by the King Air pilots resulted in significant deviations from the company’s SOPs, notwithstanding the company’s disciplinary policy.
11. In a SMS environment, inappropriate use of punitive actions can result in a decrease in the number of hazards and occurrences reported, thereby reducing effectiveness of the SMS.
12. Pilot workload is increased and decision making becomes more complicated where limited visual cues are available for assessing aircraft orientation relative to runway and surrounding terrain.
13. Aerodromes with limited visual cues and navigational aids are not explicitly identified in flight information publications as hazardous for night/IFR approaches. Passengers and crews will continue to be exposed to this hazard unless aircraft and aerodrome operators carry out risk assessments to identify them and take mitigating action.
14. To properly assess applicants for pilot positions, operators need access to information on experience and performance that is factual, objective, and (preferably) standardized. Because some employers are unprepared to provide this information—fearing legal action—this may lead to the appointment of pilots to positions for which they are unsuited, thereby compromising safety.
Other Findings:
1. TWA’s safety management system was not yet capable or expected to be capable of detecting, analyzing, and mitigating the risks presented by the hazards underlying this occurrence.
2. The first officer and captain met competency standards on the completion of their initial flight training before they began employment as line pilots.
3. It is very likely that the captain became the pilot flying for the remaining 20 seconds of the flight. The scenario that neither pilot was controlling the aircraft at that time is considered very unlikely.
Final Report:

Crash of a Piper PA-31-310 Navajo in Matambwe: 1 killed

Date & Time: Jan 5, 2007 at 0902 LT
Type of aircraft:
Registration:
5H-MUX
Survivors:
Yes
Schedule:
Dar es Salaam – Matambwe
MSN:
31-627
YOM:
1970
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1700
Circumstances:
The aircraft was carrying tourists, including the organizer of the trip to Matambwe. These passengers included five adults, a boy of sixteen, three girls of eleven, five and four years. There was also an infant of 11 months. This trip was arranged by a company called Tent with a View Safaris, which owns a camp at Matambwe in the Selous Game Reserve. According to the company, initially two aircraft were organized to transport the passengers to Matambwe. The booking was made through a telephone call to an operator called Wings of Zanzibar, who advised them to go to Terminal I of Julius Nyerere International Airport in Dar es Salaam. However, when the passengers arrived at the Wings of Zanzibar office at the airport, they found it closed. When Wings of Zanzibar was contacted on the telephone, a pilot employed by another company, DJB Ltd, was alerted to meet them. The pilot initially took them to the offices of DJB for payment. He also recommended that one aircraft would suffice for the trip. According to the pilot, he believed that the three children were small enough to sit on their parents’ laps. The passengers had little baggage. The aircraft, a Piper PA31-310 Navajo, took off from Dar es Salaam at 0825 hours and cruised at FL 65. The flight to Matambwe was uneventful and the aircraft was overhead the airstrip at 0902 hours. The pilot over flew the airstrip to alert the camp staff and check for wind and animals, a common procedure for landing in the Game Reserve airstrips. He also made another low run over the runway to ascertain its condition. Eye witnesses and passengers confirmed that the pilot made an overshoot, having flown very low attempting to land. The pilot was not sure of the runway condition because he had not flown into this airfield for a long time. In addition, before embarking on this trip, he had requested information on the runway condition from another pilot who had recently flown into the airstrip. He was told that the runway was usable. Finally, the pilot decided to land. He chose to land on runway 28 with full flaps. He touched down about two hundred and fifty meters beyond the beginning of the usable part of the runway and braked normally. After rolling for some time, he realized that the aircraft would not be able to stop before the end of the remaining length of the runway. With about another two hundred and fifty meters ahead, the pilot initiated a go round believing he had sufficient runway length remaining to gather enough speed for takeoff and climb out. He immediately increased power and initiated the go around. It is at this moment that the aircraft became airborne with no speed increase. The aircraft flew straight and level at full power without gaining height. It subsequently started chopping small tree tops for about two hundred meters beyond the end of the runway and then started to lose height. As it did so, the starboard wing collided with a large tree and the aircraft rotated through 180 degrees before coming to rest. The main wreckage settled below the impact tree and the passengers evacuated immediately. The wreckage caught fire immediately after the last passenger was evacuated. It burned completely, leaving only the tail fin and parts of the engine nacelle. When staff members from Tent with a View Camp located at Matambwe arrived, the aircraft was burning fiercely. They assisted in moving the occupants to a safer location, far from the burning wreckage and in administering first aid. The aircraft occupants were later treated at a local dispensary before being transported to a hospital in Dar es Salaam. One passenger died in the hospital four hours after the accident. Two passengers were treated for serious injuries. The injuries to the rest of the occupants were minor.
Probable cause:
The accident was caused by the aircraft colliding with trees just beyond the end of the runway. The failure to select the correct flap position for the take off, the lack of proficiency training, insufficient flight preparation and lack of real time information on the runway at Matambwe were contributory factors.
Final Report:

Crash of a De Havilland DHC-5 Buffalo in Nairobi

Date & Time: Dec 30, 2006 at 0632 LT
Type of aircraft:
Operator:
Registration:
5Y-SRK
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Nairobi - Baidoa
MSN:
003
YOM:
1965
Flight number:
UNO448A
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft departed Nairobi-Jomo Kenyatta Airport on a cargo flight to Baidoa, Somalia, carrying 3 crew members and a load consisting of 20 drums of fuel for the Somali interim Government in place in Baidoa, on behalf of the International Red Cross. Shortly after takeoff from runway 06, at a height of about 100 feet, the left engine lost power. The captain contacted ATC, declared an emergency and was cleared for an immediate return. After the engine was secured and the propeller was feathered, the crew initiated a turn when the aircraft lost height, collided with a power line and crashed onto a house, 3 minutes after takeoff. All three crew members were injured while no one was injured on ground.
Probable cause:
Failure of the left engine during initial climb for undetermined reasons. Marginal weather conditions were considered as a contributing factor.

Crash of a Britten-Norman BN-2A-20 Islander in Long Layu

Date & Time: Dec 30, 2006
Type of aircraft:
Operator:
Registration:
PK-VIN
Flight Phase:
Survivors:
Yes
MSN:
351
YOM:
1973
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While taking off from the grassy runway 01/19 which is 550 metres long, control was lost. The aircraft veered off runway and came to rest in a pond. There were no injuries but the aircraft was damaged beyond repair.

Crash of a Cessna 414 Chancellor in Johnstown: 2 killed

Date & Time: Dec 26, 2006 at 1555 LT
Type of aircraft:
Operator:
Registration:
N400CS
Flight Type:
Survivors:
No
Schedule:
Morgantown - Teterboro
MSN:
414-0613
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3547
Aircraft flight hours:
5904
Circumstances:
The airplane encountered in-flight icing, and the pilot diverted to an airport to attempt to knock the ice off at a lower altitude. During the instrument approach, the pilot advised the tower controller of the ice, and that it depended on whether or not the ice came off the airplane if she would land. As the airplane broke out of the clouds, it appeared to tower personnel to be executing a missed approach; however, it suddenly "dove" for the runway. The tower supervisor noticed that the landing gear were not down, and at 75 to 100 feet above the runway, advised the pilot to go around. The airplane continued to descend, and by the time it impacted the runway, the landing gear were only partially extended, and the propellers and airframe impacted the pavement. The pilot then attempted to abort the landing. The damaged airplane became airborne, climbed to the right, stalled, and nosed straight down into the ground.
Probable cause:
The pilot's improper decision to abort the landing with a damaged airplane. Contributing to the accident were the damage from the airplane's impact with the runway, the pilot's failure to lower the landing gear prior to the landing attempt, and the in-flight icing conditions.
Final Report:

Crash of a Cessna 414A Chancellor in Lawrenceville: 3 killed

Date & Time: Dec 25, 2006 at 2030 LT
Type of aircraft:
Operator:
Registration:
N62950
Flight Type:
Survivors:
No
Schedule:
Pahokee - Lawrenceville
MSN:
414-0086
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
631
Captain / Total hours on type:
406.00
Aircraft flight hours:
4313
Circumstances:
According to Atlanta Air Route Traffic Control Center (ARTCC) personnel, the pilot was given the current weather information before attempting his first instrument approach into Gwinnett County Airport-Briscoe Field (LZU), Lawrenceville, Georgia, which included: winds calm, visibility 1/2-mile in fog, and ceiling 100 feet. The pilot acknowledged the current weather information and elected to continue for the instrument landing system (ILS) runway-25 approach. During the first landing attempt, the pilot reported that he was going to execute a missed approach, but that he saw the airport below and wanted to attempt another approach. The ARTCC controller provided the pilot with radar vectors back to the ILS runway-25 approach and again updated the pilot with current weather conditions. During the second approach the tower controller advised the pilot that he was left of the runway-25 centerline. Shortly after the pilot acknowledged that he was left of the centerline, the tower controller saw a bright "orange glow" off of the left side of the approach end of runway 25. Although the weather conditions were below approach minimums for the runway 25-approach, the pilot elected to attempt the landing. A flight inspection of the ILS was completed on December 26, 2006, and the results of the inspection revealed that the ILS runway-25 approach system was satisfactory. Examination of the airframe, flight control system components, engines and system components revealed no evidence of preimpact mechanical malfunction.
Probable cause:
The pilot's failure to follow the instrument approach procedure. Contributing to the accident was the pilot's descent below the prescribed decision height altitude.
Final Report:

Crash of a Boeing 737-4Y0 in Ujung Pandang

Date & Time: Dec 24, 2006 at 2035 LT
Type of aircraft:
Operator:
Registration:
PK-LIJ
Survivors:
Yes
Schedule:
Jakarta - Ujung Pandang
MSN:
24682
YOM:
1990
Flight number:
LNI792
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
157
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Jakarta, the crew started the descent to Makassar (Ujung Pandang) Airport. On approach to runway 31, flaps were selected down from 15° to 30° when the captain observed an asymmetrical condition between both flaps and decided to set back at 15° and to continue the approach in such conditions. The aircraft landed hard to the left of the runway centerline and bounced twice. Out of control, it veered off runway, lost its right main gear and came to rest few dozen metres further. All 164 occupants evacuated safely while the aircraft was damaged beyond repair as the left main gear punctured the fuel tank and the fuselage was deformed.
Probable cause:
The exact cause of the asymmetrical flaps condition on approach is undetermined. Since all the conditions were clearly not met, the pilots should have made the decision to initiate a go-around procedure.

Crash of a Cessna 340A in Charleston: 4 killed

Date & Time: Dec 22, 2006 at 1335 LT
Type of aircraft:
Registration:
N808RA
Flight Type:
Survivors:
No
Schedule:
Rock Hill – Charleston
MSN:
340A-0796
YOM:
1979
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1504
Captain / Total hours on type:
129.00
Aircraft flight hours:
3828
Circumstances:
According to an airport employee at the Charleston Executive Airport (JZI), Charleston, South Carolina, the pilot contacted the JZI UNICOM radio frequency to request an airport advisory. The airport employee informed the pilot that the "winds were from 180 at 12 knots gusting to 17." The pilot then responded that he would be landing on runway 18, and was advised by the employee that there was no "runway 18." The pilot then stated that he would land on runway 27, and shortly thereafter said that he would land on runway 22. The employee said that out of curiosity he stepped outside to witness the approach of the airplane. He said that the airplane was southwest of the airport moving northeast perpendicular to runway 22, at an altitude of approximately 500 feet. He watched as the airplane was on a left base for runway 22. He said that the airplane overshot the runway and began a "tight, low right turn" away from the airport. Shortly thereafter, the airplane stalled and completed two revolutions before it was lost from his sight. Examination of the airframe, flight controls, engine assemblies and accessories revealed no evidence of a pre-crash mechanical failure or malfunction. A forensic toxicology test was performed on specimens from the pilot by the FAA Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma. The specimens contained, Tramadol (also known by the trade name Ultram), which is used for the management of moderate to severe pain. The level of Tramadol found in the pilot's blood on post-mortem toxicology testing was at least twice that of maximal regular doses of the substance. Single doses have been shown to cause mild impairment of psychomotor abilities in healthy volunteers. Diphenhydramine was also found in the blood of the pilot. The pilot may have been impaired, at that time, due to the use of Tramadol or Diphenhydramine or both.
Probable cause:
The pilot's failure to maintain airspeed during a turn from base to final, resulting in an inadvertent stall/spin. Contributing to the accident was the impairment of the pilot due to the combination of drugs found in his toxicological report.
Final Report: