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Printed page 31. PDF page 45.
vertical acceleration of about 1.42 Gs during the initial pitch-up maneuver after the aft control column movement. Thus, the actual airplane performance was slightly better than the clean wing (no ice accretion) performance assumed in the AFM. 1.16.2 Aircraft PerformanceOpen final report at PDF page 45NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 82. PDF page 96.
resulted in an airplane-nose-up elevator deflection, and adding power. In response to the aft control column movement, the AOA increased to 13�, pitch attitude increased to about 18�, load factor increased from 1.0 to about 1.4 Gs, and airspeed slowedOpen final report at PDF page 96NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 86. PDF page 100.
the load factor was 1 G. However, as stated previously, the captain's inappropriate aft control column inputs in response to the stick shaker led to an aerodynamic stall. CVR and FDR data showed that the captain made an initial aftOpen final report at PDF page 100NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 87. PDF page 101.
NTSB Aircraft Accident Report abrupt and inappropriate.197 The aft control column input occurred within 1 second of the stick shaker activation, which suggested that the captain's hands were close to or resting on the control column. However, it waOpen final report at PDF page 101NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 151. PDF page 165.
with the flight. 5. This accident was not survivable. 6. The captain's 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 didOpen final report at PDF page 165NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407
Printed page 5. PDF page 19.
NTSB Aircraft Accident Report when the autopilot disengaged, the airplane was at an airspeed of 131 knots. FDR data showed that the control columns moved aft at 2216:27.8 and that the engine poweOpen final report at PDF page 19NTSB AAR-10/01: Loss of control on approach, Colgan Air 3407