45 fatalities

Military transport crash during initial climb due to overweight condition (43-47228)

Zhijiang, ChinaTakeoff (climb)

On October 30, 1945, a Curtiss C-46 Commando (registration 43-47228) operated by United States Army Air Forces - USAAF (1941-1947) was involved in an aviation accident near Zhijiang, China during takeoff. 45 people were killed. Investigators recorded the probable cause as: The aircraft exceeded its maximum takeoff weight, preventing it from gaining sufficient altitude after rotation and leading to a stall during initial climb. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-08-05Data APIEditorial standards

A military aircraft crashed shortly after takeoff while carrying 46 soldiers and crew. The accident resulted in 45 fatalities and five serious injuries, attributed primarily to the aircraft exceeding its maximum takeoff weight.

What happened

The incident occurred during the initial climb phase immediately following departure. While ascending, the aircraft executed a right bank before stalling and descending rapidly into the ground. The impact triggered a massive explosion at the crash site. Weather conditions were reported as good at the time of the accident.

Prior to the flight, the copilot noted that the magneto check for the right engine was unsatisfactory. However, the captain assessed the check as acceptable and proceeded with the takeoff procedure. The aircraft was carrying a full complement of 46 soldiers, each equipped with their complete personal packages and ammunition, in addition to the three crew members.

Findings

Investigation into the event indicated that the aircraft failed to gain sufficient altitude after rotation. A primary contributing factor was that the total weight of the aircraft was significantly above the admissible Maximum Takeoff Weight (MTOW). This excess weight compromised the climb performance, leading to the stall and subsequent crash. The accident resulted in 45 fatalities and five serious injuries.

Probable cause

The aircraft exceeded its maximum takeoff weight, preventing it from gaining sufficient altitude after rotation and leading to a stall during initial climb.