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Bearskin Airlines 4330: loss of control at Detour Lake

Printed page 8. PDF page 8.

winds were from 360� magnetic (M)7 at 15 knots, gusting to 20 knots. Based on a 100� crosswind and the direction of the aircraft, the captain, as the PF, briefed the area navigation approach using the global navigation satellite system
Open final report at PDF page 8Loss of control and impact with runway

Bearskin Airlines 4330: loss of control at Detour Lake

Printed page 20. PDF page 20.

1005, the time of the occurrence, the winds were from 350�M, which created a 100� left crosswind.
Open final report at PDF page 20Loss of control and impact with runway

Bearskin Airlines 4330: loss of control at Detour Lake

Printed page 41. PDF page 41.

non-standard approach while facing challenging weather conditions, including a 100� crosswind (quartering tailwind). The workload associated with managing these factors was likely exacerbated by the crew's inexperience with them. On the 2 previous occasions that the ca
Open final report at PDF page 41Loss of control and impact with runway

Bearskin Airlines 4330: loss of control at Detour Lake

Printed page 45. PDF page 45.

weather at the time, the aircraft experienced a quartering tailwind of 6 to 10 knots and a crosswind of 9 to 16 knots. Therefore, the captain's efforts were also focused on maintaining the aircraft's alignment with the runway heading during
Open final report at PDF page 45Loss of control and impact with runway

Bearskin Airlines 4330: loss of control at Detour Lake

Printed page 48. PDF page 48.

flight in sub-optimal weather conditions (ceiling at minima and significant variable crosswinds) These dimensions were known to the company and were being managed individually in a variety of ways, both formally (e.g., via training and procedures) and informally (e.g.,
Open final report at PDF page 48Loss of control and impact with runway

Bearskin Airlines 4330: loss of control at Detour Lake

Printed page xii. PDF page 14.

circumstances, (2) continuation of the approach to a landing when the company's maximum crosswind component was exceeded, and (3) use of reverse thrust greater than 1.3 engine pressure ratio after landing. The safety issues in this report focus on flight
Open official document at PDF page 14Runway Overrun During Landing: American Airlines Flight 1420, McDonnell Douglas MD-82, N215AA, Little Rock, Arkansas, June 1, 1999