No fatalities

Aircraft Crash-Lands After Takeoff from Bacolod, Minor Injuries Reported (PI-C626)

Bacolod, PhilippinesTakeoff (climb)

On March 22, 1958, a Douglas DC-3 (registration PI-C626) operated by Fleming Airways System Transport was involved in an aviation accident near Bacolod, Philippines during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The captain prematurely 'lifted' the aircraft before attaining the V2 speed. A contributing factor could have been the presence of the 25 to 30 mph crosswind. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

A non-scheduled flight from Manila crash-landed shortly after takeoff from Bacolod when the aircraft banked left at low altitude. The pilot attempted correction but failed. No fatalities; pilot and some passengers suffered minor injuries. Fire destroyed the main front section.

Incident Overview

A non-scheduled flight operating between Manila and Cebu with intermediate stops at Marinduque, Iloilo, and Bacolod experienced an accident shortly after departing Bacolod. The aircraft had completed the earlier segments of the flight without incident.

Sequence of Events

The aircraft took off from Bacolod at 1210 local time. Immediately after departure, while climbing to a height of approximately 5 to 8 feet above the ground, the aircraft banked sharply to the left. The pilot attempted to correct the aircraft's attitude but was unable to regain control. In response, the pilot elected to execute a crash landing.

Injuries and Damage

No fatalities occurred during the incident. The pilot and several passengers sustained minor injuries. Upon impact, a fire ignited and destroyed the main forward section of the aircraft.

Probable Cause

According to the official investigation, the captain prematurely lifted the aircraft before attaining V2 speed. A contributing factor was the presence of a crosswind of 25 to 30 miles per hour.