Accident Swearingen SA226-TC Metro II C-FEPW, Friday 13 June 1997
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Date:Friday 13 June 1997
Type:Silhouette image of generic SW4 model; specific model in this crash may look slightly different    
Swearingen SA226-TC Metro II
Owner/operator:North American Airlines
Registration: C-FEPW
MSN: TC-294
Year of manufacture:1979
Engine model:Garrett TPE331-10UA-511G
Fatalities:Fatalities: 0 / Occupants: 2
Other fatalities:0
Aircraft damage: Destroyed, written off
Location:Ottawa/Macdonald-Cartier International Airport, ON (YOW) -   Canada
Phase: Landing
Departure airport:Hamilton Airport, ON (YHM/CYHM)
Destination airport:Ottawa-Macdonald-Cartier International Airport, ON (YOW/CYOW)
Investigating agency: TSB
Confidence Rating: Accident investigation report completed and information captured
The co-pilot was flying the aircraft for a radar-vectored, localizer/back-course approach to runway 25 of the Ottawa/Macdonald-Cartier airport. Air traffic control requested that the crew fly the aircraft at a speed of 180 knots or better to the Ottawa NDB, which is also the final approach fix (FAF) for the approach to runway 25. At approximately eight nautical miles from the airport the aircraft was clear of cloud and the crew could see the runway. In order to conduct some instrument approach practice, the pilot, who was also the company training pilot, placed a map against the co-pilot's windscreen to temporarily restrict his forward view outside the aircraft. The approach briefing was not amended to reflect the simulated instrument conditions for the approach. The co-pilot accurately flew the aircraft on the localizer to the FAF, at which point, he began to slow the aircraft to approximately 140 knots and requested that the pilot set ½ flap, which he did. Once past the FAF, the co-pilot's workload increased, and he had difficulty flying the simulated approach. On short final to runway 25, the pilot removed the map from the co-pilot's windscreen. The co-pilot noted that the aircraft was faster and higher than normal and he tried to regain the proper approach profile. By the time the aircraft reached the threshold of the runway 25, it was approximately 500 feet above ground, and at a relatively high speed, so the pilot took control of the aircraft for the landing. The pilot attempted to descend and slow the aircraft as it proceeded down the length of the runway and stated that he had just initiated an overshoot when he heard the first sounds of impact. The propellers struck the runway about 4,590 feet from the threshold of runway 25. The aircraft came to rest about 6,770 feet from the threshold, and a fire broke out in the area of the right engine.

CAUSES AND CONTRIBUTING FACTORS: "The aircraft was landed with the landing gear retracted because the flight crew did not follow the standard operating procedures and extend the landing gear. Contributing to the occurrence were the lack of planning, coordination, and communication on the part of the crew; and the failure of the landing gear warning system."

Accident investigation:
Investigating agency: TSB
Report number: TSB Report A97O0100
Status: Investigation completed
Duration: 11 months
Download report: Final report




photo (c) Werner Fischdick; San Diego International Airport, CA (SAN); 19 July 1988

Revision history:


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