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Printed page 82. PDF page 96.
inappropriate aft control column inputs in response to the stick shaker caused the airplane's wing to stall. The airplane experienced several roll oscillations during the wing aerodynamic stall. FDR data showed that, after the roll angle had reached 45� leftOpen final report at PDF page 96NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 151. PDF page 165.
inappropriate aft control column inputs in response to the stick shaker caused the airplane's wing to stall. 7. The minimal aircraft performance degradation resulting from ice accumulation did not affect the flight crew's ability to fly and control the airplane.Open final report at PDF page 165NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page v. PDF page 9.
Switch.....................................................................................18 Figure 3. Q400 Engine Display Showing Ice Detected and Increased Reference Speeds Message ...........................................................................................20 Tables Table 1. Injury Chart .....Open final report at PDF page 9NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 4. PDF page 18.
a sound similar to the stick shaker. (The stick shaker warns a pilot of an impending wing aerodynamic stall17 through vibrations on the control column, providing tactile and aural cues.) The CVR also recorded a sound similar to the autopilotOpen final report at PDF page 18NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 5. PDF page 19.
increasing, the airplane pitched up; rolled to the left, reaching a roll angle of 45� left wing down; and then rolled to the right. As the airplane rolled to the right through wings level, the stick pusher activated (about 2216:34),Open final report at PDF page 19NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 18. PDF page 32.
aerodynamically clean (that is, all ice is removed from the visible leading edges and wing tips). The Q400 AFM also cautioned that a stall warning might occur if airspeed was not increased before the ref speeds switch was selected toOpen final report at PDF page 32NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407