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

Date & Time: May 7, 2015 at 1604 LT
Operator:
Registration:
N962DA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Spokane - Spokane
MSN:
46-36031
YOM:
1996
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5800
Captain / Total hours on type:
950.00
Circumstances:
The commercial pilot was departing on a local post-maintenance test flight in the single-engine airplane; Four aileron cables had been replaced during the maintenance. Shortly after takeoff, the airplane began to roll right. As the climb progressed, the roll became more pronounced, and the airplane entered a spiraling dive. The pilot was able to maintain partial control after losing about 700 ft of altitude; he guided the airplane away from the airport and then gradually back for a landing approach. During this period, he reported to air traffic control personnel that the airplane had a "heavy right aileron." As the airplane passed over the runway threshold, it rolled right and crashed into a river adjacent to the runway. The aircraft was destroyed and both occupants were killed.
Probable cause:
The mechanic's incorrect installation of two aileron cables and the subsequent inadequate functional checks of the aileron system before flight by both the mechanic and the pilot, which prevented proper roll control from the cockpit, resulting in the pilot's subsequent loss of control during flight. Contributing to the accident was the mechanic's and the pilot's self-induced pressure to complete the work that day.
Final Report:

Crash of a Cessna 208B Grand Caravan in Verdigris

Date & Time: Mar 24, 2015 at 1507 LT
Type of aircraft:
Operator:
Registration:
N106BZ
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Tulsa - Tulsa
MSN:
208B-0106
YOM:
1988
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6500
Captain / Total hours on type:
970.00
Aircraft flight hours:
11443
Circumstances:
The pilot reported that, during the postmaintenance test flight, the turboprop engine lost power. The airplane was unable to maintain altitude, and the pilot conducted a forced landing, during which the airplane was substantially damaged. The engine had about 9 total flight hours at the time of the accident. A teardown of the fuel pump revealed that the high-pressure drive gear teeth exhibited wear and that material was missing from them, whereas the driven gear exhibited little to no visible wear. A metallurgical examination of the gears revealed that the damaged drive gear was made of a material similar to 300-series stainless steel instead of the harder specified M50 steel, whereas the driven gear was made of a material similar to the specified M50 steel. Subsequent to these findings, the airplane manufacturer determined that the gear manufacturer allowed three set-up gears made from 300-series stainless steel to become part of the production inventory during the manufacturing process. One of those gears was installed in the fuel pump on the accident airplane, and the location of the two other gears could not be determined. Based on the evidence, it is likely that the nonconforming gear installed in the fuel pump failed because it was manufactured from a softer material than specified, which resulted in a loss of fuel flow to the engine and the subsequent loss of engine power. The manufacturer subsequently inspected its stock of gears and issued notices to customers that had engines with fuel pumps installed with the same part number gear set as the one installed on the accident airplane. The manufacturer also issued a service information letter and service bulletins regarding the fuel pump gear set for engines used in civilian and military applications. As of the date of this report, the two remaining gears have not been located.
Probable cause:
The fuel pump gear manufacturer’s allowance of set-up gears made from a nonconforming material to be put in the production inventory system, the installation of a nonconforming gear in the accident airplane’s production fuel pump, and the gear’s failure, which resulted in a loss of fuel flow to the engine and the subsequent loss of engine power.
Final Report:

Ground accident of a Dornier DO328-110 in Hamburg

Date & Time: Jan 12, 2015
Type of aircraft:
Operator:
Registration:
D-CIRD
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
3011
YOM:
1994
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was parked on the ramp and subject to engine test run with one or two engineers on board. During the test, the aircraft jumped over the chocks then collided with obstacles and came to rest. There were no injuries while the aircraft was damaged beyond repair. It was operated by Sun-Air of Scandinavia on behalf of British Airways.

Crash of an Antonov AN-2 in Sevryukovo

Date & Time: Oct 6, 2013 at 1425 LT
Type of aircraft:
Operator:
Registration:
RA-31505
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Sevryukovo - Sevryukovo
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Bought in 2000 and stored since, the airplane was under restoration since August 2013. The crew (one pilot and one engineer), decided to perform a test flight in the region of Sevryukovo (Korocha District of the Belgorod region). En route, the engine failed, forcing the crew to attempt an emergency landing. The aircraft impacted ground and crashed, coming to rest upside down and bursting into flames. Both occupants escaped uninjured while the aircraft was partially destroyed by fire.
Probable cause:
An investigation by the Interstate Aviation Committee revealed that the airplane carried a false registration and was flown without a certificate of airworthiness. Since the airplane was not officially registered, the IAC terminated their investigation.

Crash of a PZL-Mielec AN-2P in Shakhty

Date & Time: Jul 28, 2013
Type of aircraft:
Operator:
Registration:
FLA-3618K
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Shakhty - Shakhty
MSN:
1G151-37
YOM:
1973
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Shakhty Airport, Rostov oblast, the pilot encountered engine problem. He elected to make an emergency landing in an open field located 500 metres from the airport. On touchdown, the aircraft lost its undercarriage, wings and tail before coming to rest in bushes. The pilot, uninjured, fled the scene but was arrested by police few hours later. Technician by a Plant at the Shakhty Airport, he was the owner of this aircraft since seven months and was performing a local test flight despite he was not in possession of any valid pilot licence according to Russian authorities.

Crash of a Canadair CL-601-3A Challenger in Chino

Date & Time: Jun 13, 2013 at 1817 LT
Type of aircraft:
Registration:
N613SB
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
5088
YOM:
1991
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Two technicians were performing engine tests on apron at Chino Airport. While facing a hangar, the aircraft jumped over the chocks and collided with the metallic door of the hangar before coming to rest half inside. Both occupants escaped uninjured and the aircraft was damaged beyond repair.
Probable cause:
No investigation has been conducted by the NTSB about this event.

Crash of a Beechcraft A100 King Air in Saint-Mathieu-de-Beloeil

Date & Time: Jun 10, 2013 at 1725 LT
Type of aircraft:
Operator:
Registration:
C-GJSU
Flight Type:
Survivors:
Yes
Schedule:
Montreal - Montreal
MSN:
B-88
YOM:
1971
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4301
Captain / Total hours on type:
1500.00
Aircraft flight hours:
13616
Aircraft flight cycles:
10999
Circumstances:
The aircraft took off from the Montréal/St-Hubert Airport, Quebec, on a local flight under visual flight rules with 1 pilot and 3 passengers on board. The purpose of the flight was to check the rudder trim indicator and to confirm a potential synchronization problem between the autopilot and the global positioning system (GPS). As the aircraft approached Runway 24R at the Montréal/St-Hubert Airport, both engines (Pratt & Whitney Canada, PT6A-28) stopped due to fuel exhaustion. The pilot diverted to the St-Mathieu-de-Beloeil Airport, Quebec, and then attempted a forced landing in a field 0.5 nautical mile west of the St-Mathieu-de-Beloeil Airport. The aircraft struck the ground 30 feet short of the selected field, at 1725 Eastern Daylight Time. The aircraft was extensively damaged, and the 4 occupants sustained minor injuries. The emergency locator transmitter activated during the occurrence. The flight took place during daylight hours, and there was no fire.
Probable cause:
Findings as to causes and contributing factors:
- The pilot relied exclusively on the gauge readings to determine the quantity of fuel on board, without cross-checking the fuel consumption since the last fueling to validate those gauge readings.
- The pilot misread the fuel gauges and assumed that the aircraft had enough fuel on board to meet the minimum fuel requirements of the Canadian Aviation Regulations for this visual flight rules flight, rather than adding more fuel to meet the greater reserves required by the company operations manual.
- The pilot did not monitor the fuel gauges while in flight and decided to extend the flight to carry out a practice instrument approach with insufficient fuel to complete the approach.
- The right engine stopped due to fuel exhaustion.
- The pilot did not carry out the approved engine failure procedure when the first engine stopped, and the propeller was not feathered, resulting in significant drag which reduced the aircraft's gliding range after the second engine stopped.
- The pilot continued flying toward Montréal/St-Hubert Airport (CYHU), Quebec, despite having advised air traffic control of the intention to divert to the St-Mathieu-de-Beloeil Airport (CSB3), Quebec, and without communicating the emergency. The priority given to communications resulted in the aircraft moving farther away from the intended diversion airport.
- The left engine stopped due to fuel exhaustion 36 seconds after the right engine stopped, when the aircraft was 7.4 nautical miles from Runway 24R at Montréal/St-Hubert Airport (CYHU), Quebec, and 2400 feet above sea level.
- The pilot's decision to lower the landing gear while the aircraft was still at 1600 feet above sea level further increased the drag, reducing the aircraft's gliding range. As a result, the aircraft was not able to reach the runway at St-Mathieu-de-Beloeil Airport (CSB3), Quebec.
- The operations manager was unable to perform the duties and responsibilities of the position related to monitoring and supervision of flight operations. As a result, the safety of more than half of the flights was compromised.
Findings as to risk:
- If the total fuel quantity required for a flight is not calculated and clearly displayed on the operational flight plan, there is an increased risk that aircraft will depart without the fuel reserves required by the Canadian Aviation Regulations.
- If flights are planned and carried out without the fuel reserves required by the Canadian Aviation Regulations, there is an increased risk of fuel exhaustion resulting from unanticipated situations that extend the duration of the flight.
- If pilots elect to extend flight without first determining whether sufficient fuel reserves are available to do so, there is an increased risk of fuel exhaustion.
- If pilots do not regularly check the quantity of fuel on board, there is an increased risk of fuel exhaustion.
- If pilots do not rule out a fuel leak before opening the crossfeed valve, they risk losing all of the remaining fuel on board.
- If a pilot does not maintain control of an aircraft until landing, the force of an impact following an aerodynamic stall is likely to be far greater, increasing the risk of injury or death during a forced landing.
- If a pilot does not declare an emergency to air traffic control in a timely manner, the pilot may be deprived of assistance and resources that could help deal with the emergency, increasing the risk of an accident.
- If pilots do not receive training in dealing with complex emergencies that require prioritizing tasks, there is a risk that they will not react effectively to emergencies, increasing the risk of an accident.
- If companies do not establish a process to monitor the performance of their pilots during training and testing, there is a risk that those companies will inadvertently assign pilots to carry out flights for which they are not proficient.
- If a flight is planned and authorized solely by the pilot, with no cross-check for compliance with existing regulations, there is a risk that deviations will continue undetected, reducing the safety of the flight.
- If pilots operate without regular supervision to ensure compliance with regulations and company procedures, coupled with effective training, there is a risk of procedural adaptations that result in reduced safety margins.
- If companies assign inexperienced personnel to key flight operations management positions, there is a risk that deviations in performance or from regulations will not be detected, reducing the safety of flight operations.
- If the pilot proficiency check requirements for a chief pilot are not more stringent than those for other pilots, there is a risk that the chief pilot will be unable to perform the duties required to ensure the safety of company training and operations.
- If the approval process for appointment of operations management personnel by companies is reduced to a compliance checklist based on the minimum standards in the Commercial Air Service Standards and on pilot proficiency checks that may be repeated an unlimited number of times, there is a risk that candidates who are unfit to perform the duties and responsibilities of their positions will be appointed.
- If Transport Canada does not take into consideration the combined knowledge and experience of a new operator's management team, there is a risk that the operator will lack the skills necessary to ensure the safety of flight operations.
- If process inspections carried out by Transport Canada do not examine factors related to a recent occurrence, there is a risk that those hazardous conditions will go undetected and will persist.
If process inspections carried by TC on newly certificated operators do not closely examine the outcomes of company processes, there is a risk that hazardous conditions will not be identified and will persist.
- If the inability of appointed individuals to perform their duties and responsibilities does not constitute grounds for suspending or revoking the ministerial approval of such appointments, there is a risk that operations management personnel who are not competent will remain in their positions, increasing the risk to flight safety.
Other findings:
- The chief pilot did not meet the requirements of the Canadian Aviation Regulations at the time of appointment.
- There was no indication that the aircraft's fuel gauges were not functioning properly at the time of the occurrence flight, and it is unlikely that a deviation of the fuel gauge indicator was a factor in the pilot's decision to take off.
- C-GJSU had approximately 260 pounds of fuel on board when it took off from Montréal/St-Hubert Airport (CYHU), Quebec, and did not experience a fuel leak during the occurrence flight.
Final Report:

Crash of a Piper PA-31T Cheyenne II in Fort Lauderdale: 3 killed

Date & Time: Mar 15, 2013 at 1621 LT
Type of aircraft:
Registration:
N63CA
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Fort Lauderdale - Fort Lauderdale
MSN:
31-7820033
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
10000
Aircraft flight hours:
5006
Circumstances:
The multiengine airplane had not been flown for about 4 months and was being prepared for export. The pilot was attempting a local test flight after avionics upgrades had been performed. Shortly after takeoff, the pilot transmitted that he was experiencing an "emergency"; however, he did not state the nature of the emergency. The airplane was observed experiencing difficulty climbing and entered a right turn back toward the airport. It subsequently stalled, rolled right about 90 degrees, and descended. The airplane impacted several parked vehicles and came to rest inverted. A postcrash fire destroyed the airframe. Both engines were destroyed by fire and impact damage. The left propeller assembly was fire damaged, and the right propeller assembly remained attached to the gearbox, which separated from the engine. Examination of wreckage did not reveal any preimpact malfunctions. It was noted that the left engine displayed more pronounced rotational signatures than the right engine, but this difference could be attributed to the impact sequence. The left propeller assembly displayed evidence of twisting and rotational damage, and the right propeller assembly did not display any significant evidence of twisting or rotational damage indicative of operation with a difference in power. The lack of flight recorders and the condition of the wreckage precluded the gathering of additional relevant information.
Probable cause:
The pilot's failure to maintain airplane control following an emergency, the nature of which could not be determined because of crash and fire damage, which resulted in an aerodynamic stall.
Final Report:

Crash of a Rockwell Aero Commander 500B in Broomfield

Date & Time: Mar 1, 2013 at 1545 LT
Operator:
Registration:
N93AA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Broomfield - Broomfield
MSN:
500-1296-111
YOM:
1963
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15000
Captain / Total hours on type:
414.00
Aircraft flight hours:
10021
Circumstances:
The pilot stated that, during the preflight inspection of the airplane, he checked the fuel gauge, and it indicated 65 gallons. Due to the design of the fuel system, it is not possible to visually check the fuel level to confirm that the fuel gauge indication is accurate. During takeoff and as he reduced power for enroute climb, the left engine began to surge and lose power. He immediately turned left back toward the airport and contacted the control tower to advise that he was making a single-engine, straight-in approach to land. When he lowered the landing gear, the right engine began to surge and lose power. Subsequently, the pilot declared an emergency, and, realizing he had insufficient engine power and altitude to return to the airport, he retracted the landing gear and made a no-flap, gear-up landing on a nearby golf course. Postaccident application of battery power to the airplane confirmed that the fuel gauge indicated 65 gallons; however, when the airplane's fuel system was drained, only about 1/2 gallon of fuel was recovered. Thus, the engines lost power due to fuel exhaustion.
Probable cause:
Loss of engine power due to fuel exhaustion. Contributing to the accident was the failure of the fuel gauge to indicate the actual amount of fuel on board the airplane and the design of the airplane's fuel system, which precluded a visual confirmation of the fuel level.
Final Report:

Crash of a Cessna 550 Citation II in Greenwood

Date & Time: Nov 17, 2012 at 1145 LT
Type of aircraft:
Operator:
Registration:
N6763L
Flight Type:
Survivors:
Yes
Schedule:
Greenwood - Greenwood
MSN:
550-0673
YOM:
1991
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11592
Captain / Total hours on type:
903.00
Copilot / Total flying hours:
4501
Copilot / Total hours on type:
13
Aircraft flight hours:
8611
Circumstances:
The aircraft, registered to the United States Customs Service, and operated by Stevens Aviation, Inc., was substantially damaged during collision with a deer after landing on Runway 9 at Greenwood County Airport (GRD), Greenwood, South Carolina. The airplane was subsequently consumed by postcrash fire. The two certificated airline transport pilots were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the maintenance test flight, which was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. According to the pilot, the purpose of the flight was to conduct a test of the autopilot and flight director systems on board the airplane, following a "cockpit modernization" their company had performed. The airplane completed the NDB/GPS RWY 27 instrument approach procedure and then circled to land on Runway 9. About 5 seconds into the landing rollout, a deer appeared from the wood line and ran into the path of the airplane. The deer struck the airplane at the leading edge of the left wing above the left main landing gear, and ruptured an adjacent fuel cell. The pilot was able to maintain directional control, and the airplane was stopped on the runway, spilling fuel and on fire. The crew performed an emergency shutdown of the airplane and egressed without injury.Greenwood County Airport did not have a fire station co-located on the airport facility. The fixed base operator called 911 at the time of the accident, and the fire trucks arrived approximately 10 minutes after notification.
Probable cause:
Collision with a deer during the landing roll, which resulted in a compromised fuel tank and a postimpact fire. In a telephone interview, the manager of the Greenwood County Airport explained that Greenwood was not an FAR Part 139 Airport, and while there was no published Wildlife Management Program for the airport, she had been very proactive about eradicating wildlife that could pose a hazard to safety on the airport property, primarily deer and wild turkey. She contacted the United States Department of Agriculture (USDA) for guidance and advice and she attended a wildlife management course. Among the suggestions offered by the USDA, was to remove the deer habitat. The manager proposed adding the area between the runway and taxiway to an approach clearing project in order to reduce the habitat. The manager worked with a local charity and local hunters with depredation permits to take deer on the airport property, and their efforts averaged 50 deer a year. The hunts were conducted in stands away from runways and on property not aviation related. The nearest deer stand was 1 mile from the runway, and the hunters fired only shotguns. The hunts were conducted between the hours of 0700 and 1000. On the morning of the accident, the last shot was fired at 0930.When asked why the hunters were still on the property at the time of the accident, the manager said they had stayed to eat lunch, and repeated that the hunt was long over and that the last shot was fired hours before the accident. She offered that the deer struck by the airplane was probably flushed from the woods by another deer or a coyote, whose population has also grown in recent years.After the accident, the Federal Aviation Administration contacted the state and had the Greenwood County Airport added to a list of airports where funding for improvements had been allotted. A second 10-foot perimeter fence was added around the existing 6-foot fence, and since its construction only 4 deer have been taken inside the perimeter, and no wild turkeys have been sighted
Final Report: