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Crash of a Beechcraft A100 King Air in Gods Lake Narrows

Date & Time: Nov 22, 2008 at 2140 LT
Type of aircraft:
Operator:
Registration:
C-FSNA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Gods Lake Narrows – Thompson
MSN:
B-227
YOM:
1976
Flight number:
SNA683
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3200
Captain / Total hours on type:
1850.00
Copilot / Total flying hours:
1000
Copilot / Total hours on type:
500
Circumstances:
The Sky North Air Ltd. Beechcraft A100 (registration C-FSNA, serial number B-227) operating as SN683 departed Runway 32 at Gods Lake Narrows, Manitoba, for Thompson, Manitoba with two pilots, a flight nurse, and two patients on board. Shortly after takeoff, while in a climbing left turn, smoke and then fire emanated from the pedestal area in the cockpit. The crew continued the turn, intending to return to Runway 14 at Gods Lake Narrows. The aircraft contacted trees and came to rest in a wooded area about one-half nautical mile northwest of the airport. The accident occurred at 2140 central standard time. All five persons onboard evacuated the aircraft; two received minor injuries. At approximately 0250, the accident site was located and the occupants were evacuated. The aircraft was destroyed by impact forces and a post-crash fire. The emergency locator transmitter was consumed by the fire and whether or not it transmitted a signal is unknown.
Probable cause:
Findings as to Causes and Contributing Factors:
1. An electrical short circuit in the cockpit pedestal area produced flames and smoke, which induced the crew to take emergency action.
2. The detrimental effects of aging on the wires involved may have been a factor in this electrical arc event.
3. The crew elected to return to the airport at low level in an environment with inadequate visual references. As a result, control of the aircraft was lost at an altitude from which a recovery was not possible.
Findings as to Risk:
1. The actions specified in the standard operating procedures (SOP) do not include procedures for an electrical fire encountered at low altitude at night, which could lead to a loss of control.
2. Visual inspection procedures in accordance with normal phase inspection requirements may be inadequate to detect defects progressing within wiring bundles, increasing the risk of electrical fires.
3. In the event of an in-flight cockpit pedestal fire, the first officer does not have ready access to available fire extinguishers, reducing the likelihood of successfully fighting a fire of this nature.
4. Sealed in plastic containers and stored behind each pilot seat, the oxygen masks and goggles are time consuming to access and cumbersome to apply and activate. This could increase the probability of injury or incapacitation through extended exposure to smoke or fumes, or could deter crews from using them, especially during periods of high cockpit workload.
Other Finding:
1. A failure of the hot-mic recording function of the cockpit voice recorder (CVR) had gone undetected and information that would have been helpful to the investigation was not available.
Final Report:

Crash of a Swearingen SA226TC Metro II in Shamattawa: 2 killed

Date & Time: Oct 11, 2001 at 2333 LT
Type of aircraft:
Operator:
Registration:
C-GYPA
Flight Type:
Survivors:
Yes
Schedule:
Gods Lake Narrows – Shamattawa
MSN:
TC-250
YOM:
1978
Flight number:
PAG962
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3100
Captain / Total hours on type:
1100.00
Copilot / Total flying hours:
1200
Copilot / Total hours on type:
900
Circumstances:
Perimeter Airlines Flight PAG962, a Fairchild SA226TC (Metroliner), with two pilots and a flight nurse on board, departed Gods Lake Narrows, Manitoba, at approximately 2300 central daylight time, on a MEDEVAC flight to Shamattawa. Approaching Shamattawa, the crew began a descent to the 100 nautical mile minimum safe altitude of 2300 feet above sea level (asl) and, when clear of an overcast cloud layer at about 3000 feet asl, attempted a night, visual approach to Runway 01. The aircraft was too high and too fast on final approach and the crew elected to carry out a missed approach. Approximately 30 seconds after the power was increased, at 2333, the aircraft flew into trees slightly to the left of the runway centreline and about 2600 feet from the departure end of Runway 01. The aircraft was equipped with a cockpit voice recorder (CVR) that indicated the crew were in control of the aircraft; they did not express any concern prior to impact. The aircraft broke apart along a wreckage trail of about 850 feet. Only the cabin aft of the cockpit retained some structural integrity. The captain and first officer were fatally injured on impact. The flight nurse was seriously injured but was able to exit the wreckage of the cabin. A post-crash fire was confined to the wings which had separated from the cabin and cockpit wreckage.
Probable cause:
Findings as to Causes and Contributing Factors:
1. The aircraft was flown into terrain during an overshoot because the required climb angle was not set and maintained to ensure a positive rate of climb.
2. During the go-around, conditions were present for somatogravic illusion, which most likely led to the captain losing situational awareness.
3. The first officer did not monitor the aircraft instruments during a critical stage of flight; it is possible that he was affected by somatogravic illusion and/or distracted by the non-directional
beacon to the extent that he lost situational awareness.
Other Findings:
1. The absence of approach aids likely decreased the crew=s ability to fly an approach from which a landing could be executed safely.
2. The company standard operating procedures (SOPs) did not define how positive rate is to be determined.
Final Report:

Crash of a Swearingen SA226TC Metro II in Gods River

Date & Time: Nov 1, 1996 at 1423 LT
Type of aircraft:
Operator:
Registration:
C-FHOZ
Survivors:
Yes
Schedule:
Winnipeg – Gods Lake Narrows – Gods River – Winnipeg
MSN:
TC-283
YOM:
1979
Flight number:
PAG207
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Gods River Airport runway 27, the right main gear struck a snow berm located 105 metres short of runway threshold. The crew continued the approach and the aircraft landed 99 metres past the runway threshold. On touchdown, the right main gear collapsed. The aircraft slid fore few dozen metres then veered off runway to the right and came to rest. All seven occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Cessna 441 Conquest in Fort Frances

Date & Time: Jun 18, 1994 at 0425 LT
Type of aircraft:
Operator:
Registration:
N441CA
Flight Phase:
Survivors:
Yes
Schedule:
Milwaukee – Fort Frances – God’s Lake Narrows
MSN:
441-0046
YOM:
1978
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4800
Captain / Total hours on type:
40.00
Aircraft flight hours:
2447
Circumstances:
The pilot of the Cessna 441 Conquest was conducting an international charter flight from General Mitchell International Airport in Milwaukee, Wisconsin, to Gods Lake Narrows, Manitoba. The pilot landed the aircraft at Fort Frances, Ontario, to clear customs and refuel, and then continued his visual flight rules (VFR) flight to Gods Lake Narrows. During the take-off at Fort Frances, the aircraft experienced a power loss in the left engine. The pilot elected to continue the take-off but was unable to control the aircraft after it became airborne. The aircraft veered to the left and crashed on the airfield. The accident occurred at 0425 central daylight time (CDT), at night, on the Fort Frances Municipal Airport. All seven occupants sustained minor injuries and the aircraft was damaged beyond repair.
Probable cause:
The pilot lost control of the aircraft during take-off when the left engine lost power as a result of bird ingestion. Contributing to the loss of aircraft control were a take-off weight in excess of the maximum allowable, and a centre of gravity aft of the centre of gravity limit.
Final Report: