No fatalities

1953-03-27: De Havilland DH.114 Heron (PP-SLG) — Transportes Aéreos Salvador — Itapebi, Brazil

Itapebi, BrazilTakeoff (climb)

On March 27, 1953, a De Havilland DH.114 Heron (registration PP-SLG) operated by Transportes Aéreos Salvador was involved in an aviation accident near Itapebi, Brazil during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The exact cause of the loss of power on engine number two could not be determined with certainty. However, it was reported that the decision of the captain to abandon the takeoff was against the published procedures as the loss of power occurred after the… 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 1781253447Data APIEditorial standards

During takeoff, the captain noted a loss of power on engine two and aborted, initiating emergency braking. The aircraft overran the runway, lost its undercarriage, and sustained beyond-repair damage. All 14 occupants evacuated safely.

Incident Overview

A four-engine aircraft overran the runway and sustained substantial damage after the captain aborted the takeoff due to a loss of power on engine number two. The incident occurred during the takeoff roll, and the aircraft came to rest a few dozen yards beyond the runway. All 14 occupants evacuated safely, but the aircraft was damaged beyond repair.

Sequence of Events

During the takeoff roll, the pilot-in-command observed a loss of power on engine number two. The captain decided to abandon the takeoff procedure and initiated an emergency braking maneuver. The aircraft was unable to stop within the remaining runway distance, overran the runway, lost its undercarriage, and came to rest a short distance beyond.

Probable Cause

The official investigation was unable to determine the exact cause of the loss of power on engine number two. However, it was noted that the captain's decision to abort the takeoff was contrary to published procedures, as the loss of power occurred after the aircraft had reached rotation speed (VR). According to those procedures, the takeoff should have been continued with three engines operating.