Aviation Accident Summaries

Aviation Accident Summary FTW89LA041

LAREDO, TX, USA

Aircraft #1

XBDYP

DOUGLAS DC-3

Analysis

THE PILOT STATED THAT DURING TAKEOFF FROM RUNWAY 35L, THE CO-PILOT ON THE FLIGHT CONTROLS REDUCED LEFT PROPELLER AND RIGHT ENGINE POWER AT AN ALTITUDE OF LESS THAN 100 FEET AGL. HE ATTEMPTED TO RESTORE TAKEOFF POWER WHILE APPLYING FORWARD PRESSURE ON THE CONTROL YOKE, BUT LOST CONTROL OF THE AIRCRAFT AND IMPACTED THE TERRAIN ADJACENT TO THE DEPARTURE RUNWAY. HE FURTHER STATED THAT THE CARGO MAY HAVE SHIFTED TO THE REAR OF THE AIRCRAFT DURING TAKEOFF.

Probable Cause and Findings

THE PIC'S DISREGARD FOR THE SECURITY OF THE CARGO THAT PERMITTED ITS SHIFT DURING THE TAKOEFF ROLL. THIS RESULTED IN AN AFT CG SITUATION AND A SUBSEQUENT STALL AND LOSS OF AIRCRAFT CONTROL. A CONTRIBUTING FACTOR IN THE ACCIDENT WAS THE MISMANAGEMENT OF THE ENGINE POWER BY THE CREW AND THE LACK OF EXPERIENCE OF THE CO-PILOT.

 

Source: NTSB Aviation Accident Database

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