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 Beechcraft A100 King Air in Sault Sainte Marie

Date & Time: Jan 2, 2006 at 0200 LT
Type of aircraft:
Operator:
Registration:
N700NC
Flight Type:
Survivors:
Yes
Schedule:
Traverse City – Sault Sainte Marie
MSN:
B-138
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7620
Captain / Total hours on type:
70.00
Aircraft flight hours:
13033
Circumstances:
The airplane, operated as an emergency medical flight, received substantial damage when it veered off the edge of runway 32 (5,235 feet long by 100 foot wide asphalt, slush and snow covered) and impacted a snow bank during landing roll at a non 14 CFR Part 139 airport. Night instrument meteorological conditions prevailed at the time of the accident. The pilot stated that during a non precision approach while two miles from the runway, he observed it to be completely covered in snow and slush. He continued the approach and upon touchdown the airplane decelerated in deep slush and veered to the left after a rollout of 1,200 feet. The pilot reported that prior to accepting the emergency medical flight, he obtained a weather briefing from a flight service station during which time no notices to airman (NOTAMs) existed that pertained to the destination airport. The pilot reported that he knew the airport was getting rain and was expecting the runway to be clear. He was surprised that the runway was covered with heavy slush. The airport manager stated that the runway was covered with wet, slushy snow as there had been periods of wet snow and rain that occurred late the previous day and evening of the accident. The airport weather observation recorded the presence of light snow in a period of approximately 24 hours before the accident. The pilot "wondered" why no NOTAM was issued relating to the runway condition. The Airport Facility Directory and the FAA's web site provides a list of 14 CFR Part 139 airports which are inherently required to issue NOTAMs. However, Advisory Circular 150/5200-28C states, the management of a public use airport is expected to make known, as soon as practical, any condition on or in the vicinity of an airport, existing or anticipated, that will prevent, restrict, or present a hazard during the arrival or departure of aircraft. Airport management is responsible for observing and reporting the condition of airport movement areas. Public notification is usually accomplished through the NOTAM system. The Aeronautical Information Manual, states that NOTAM information is information that could affect a pilot's decision to make a flight. It includes information such as airport or primary runway closures, changes in the status of navigational aids, ILS's, radar service availability, and other information essential to planned en route, terminal, or landing operations.
Probable cause:
The inadequate in-flight decision to continue the approach to land, directional control not maintained, and the contaminated runway. Contributing factors were flight to destination alternate not performed, a notice to airman not issued by airport personnel relating to snow/slush contamination of the runway, and the snow bank that the airplane impacted during the landing.
Final Report:

Crash of a Beechcraft A100 King Air in La Ronge

Date & Time: Dec 30, 2005 at 1500 LT
Type of aircraft:
Operator:
Registration:
C-GAPK
Flight Type:
Survivors:
Yes
Schedule:
Pinehouse Lake – La Ronge
MSN:
B-198
YOM:
1974
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
A Beechcraft A100 King Air, C-GAPK was inbound to La Ronge Airport, SK (YVC), from Pinehouse Lake on a medevac flight. On descent into La Ronge the crew noticed ice building on the wing leading edges. At approximately 6 miles back on final the crew operated the wing de-ice boots, however a substantial amount of residual ice remained after application of the boots. It was reported that in the landing flare at about 100 knots, the aircraft experienced an ice-induced stall from an altitude of about 20 feet followed by a hard landing. The right wing and nacelle buckled forward and downward from the landing impact forces to the extent that the right propeller struck the runway surface while the aircraft was taxiing off the runway.

Crash of a Beechcraft A100 King Air in Paparo

Date & Time: Dec 26, 2005 at 1700 LT
Type of aircraft:
Operator:
Registration:
YV1507
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Barcelona – Charallave
MSN:
B-155
YOM:
1973
Location:
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route from Barcelona to Charallave, the crew encountered engine problems and elected to divert to the nearest airport. Eventually, he attempted an emergency landing when the aircraft crash landed in a prairie and collided with trees. All three occupants escaped with minor injuries and the aircraft was damaged beyond repair.

Crash of a Beechcraft A100 King Air in Fort Vermilion

Date & Time: Jul 13, 2004 at 0001 LT
Type of aircraft:
Registration:
C-FQOV
Flight Type:
Survivors:
Yes
Schedule:
Grande Prairie – Fort Vermilion
MSN:
B-38
YOM:
1970
Flight number:
LRA913M
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crew twin engine aircraft was performing an ambulance flight from Grande Prairie to his base in Fort Vermilion with one patient, one doctor, one accompanist and two pilots on board. On final approach, the aircraft was too high and eventually landed hard. Upon touchdown, the right main gear collapsed and the aircraft veered off runway to the right and and came to rest. All five occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:

Crash of a Beechcraft A100 King Air in Chibougamau

Date & Time: Apr 19, 2004 at 1018 LT
Type of aircraft:
Operator:
Registration:
C-FMAI
Survivors:
Yes
Schedule:
Quebec - Chibougamau
MSN:
B-145
YOM:
1973
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11338
Captain / Total hours on type:
2600.00
Copilot / Total flying hours:
1176
Copilot / Total hours on type:
400
Circumstances:
The Beechcraft A100, registration C-FMAI, operated by Myrand Aviation Inc., was on a chartered instrument flight rules flight from QuÈbec/Jean Lesage International Airport, Quebec, to Chibougamau/Chapais Airport, Quebec, with two pilots and three passengers on board. The copilot was at the controls and was flying a non-precision approach for Runway 05. The pilot-in-command took the controls less than one mile from the runway threshold and saw the runway when they were over the threshold. At approximately 1018 eastern daylight time, the wheels touched down approximately 1500 feet from the end of Runway 05. The pilot-in-command realized that the remaining landing distance was insufficient. He told the co-pilot to retract the flaps and applied full power, but did not reveal his intentions. The co-pilot cut power, selected reverse pitch and applied full braking. The aircraft continued rolling through the runway end, sank into the gravel and snow, and stopped abruptly about 500 feet past the runway end. The aircraft was severely damaged. None of the occupants were injured.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The aircraft was positioned over the runway threshold at an altitude that did not allow a landing at the beginning of the runway, and this, combined with a tailwind component and the wet runway surface, resulted in a runway excursion.
2. Failure to follow standard operating procedures and a lack of crew coordination contributed to confusion on landing, which prevented the crew from aborting the landing and executing a missed approach.
3. The pilot-in-command held several management positions within the company and controlled the pilot hiring and dismissal policies. This situation, combined with the level of experience of the co-pilot compared with that of the pilot-in-command, had an impact on crew cohesiveness.
Findings as to Risk:
1. The pilot-in-command of C-FMAI decided to execute an approach for Runway 05 without first ensuring that there would be no possible risk of collision with the other aircraft.
2. The regulatory requirement to conform to or avoid the traffic pattern formed by other aircraft is not explicit as to how the traffic pattern should be avoided, in terms of either altitude or distance, which can result in risks of collision.
3. The regulations do not indicate whether the missed approach segment should be considered part of the traffic pattern; this situation can lead pilots operating in uncontrolled airspace to believe that they are avoiding another aircraft executing an instrument approach when in reality a risk of collision exists.
Final Report:

Crash of a Beechcraft A100 King Air in Terrace Bay

Date & Time: Jan 1, 2004
Type of aircraft:
Operator:
Registration:
C-GFKS
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Terrace Bay – Thunder Bay
MSN:
B-247
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On take off roll on runway 25 at dusk, left wing struck a snowbank on left side of the runway. Aircraft veered off runway and came to rest in snow with its nose gear sheared off and several damages to the fuselage. Both pilots were uninjured.
Probable cause:
A NOTAM stated that there were windrows four feet high, 10 feet inside the runway lights on both sides of the runway. This NOTAM also stated that the cleared portion of the runway was covered with ¼ inch of loose snow over 60 percent compacted snow and 40 percent ice patches and that braking action was fair to poor. The take-off was being conducted at dusk in conditions of poor lighting and contrast. Crosswind was not a factor.

Crash of a Beechcraft A100 King Air in Eveleth: 8 killed

Date & Time: Oct 25, 2002 at 1022 LT
Type of aircraft:
Operator:
Registration:
N41BE
Survivors:
No
Schedule:
Saint-Paul – Eveleth
MSN:
B-245
YOM:
1979
Flight number:
N41BE
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
5116
Captain / Total hours on type:
200.00
Copilot / Total flying hours:
701
Copilot / Total hours on type:
107
Aircraft flight hours:
12726
Circumstances:
On October 25, 2002, about 1022 central daylight time, a Raytheon (Beechcraft) King Air A100, N41BE, operated by Aviation Charter, Inc., crashed while the flight crew was attempting to execute the VOR approach to runway 27 at Eveleth-Virginia Municipal Airport, Eveleth, Minnesota. The crash site was located about 1.8 nautical miles southeast of the approach end of runway 27. The two pilots and six passengers were killed, and the airplane was destroyed by impact forces and a post crash fire. The airplane was being operated under the provisions of 14 Code of Federal Regulations Part 135 as an on-demand passenger charter flight. Instrument meteorological conditions prevailed for the flight, which operated on an instrument flight rules flight plan. Among those on board were Paul Wellstone, Senator of Minnesota, his wife Sheila and one of his three children Marcia.
Probable cause:
The flight crew's failure to maintain adequate airspeed, which led to an aerodynamic stall from which they did not recover.
Final Report:

Crash of a Beechcraft 100 King Air in Buriti Alegre

Date & Time: Nov 25, 2001 at 1205 LT
Type of aircraft:
Registration:
PT-DNP
Flight Type:
Survivors:
Yes
Schedule:
Goiânia – Buriti Alegre
MSN:
B-56
YOM:
1970
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13316
Captain / Total hours on type:
1500.00
Circumstances:
On final approach to Buriti Alegre Airfield runway 05, following an uneventful flight from Goiânia-Santa Genoveva Airport, the pilot attempted to lower the flaps twice but the circuit breakers opened. He decided to continue the approach in a flapless configuration when, on short final, the aircraft stalled and collided with a wall located 15 metres short of runway. On impact, the undercarriage were torn off and the airplane landed on its belly, slid for 500 metres and came to rest, bursting into flames. All six occupants escaped uninjured while the aircraft was destroyed by fire.
Probable cause:
The pilot decided to continue the approach in a flapless configuration and at an insufficient speed, which caused the aircraft to stall on short final.
Final Report: