29 fatalities

1963-06-03: Douglas DC-3 (VT-AUL) — Indian Airlines — Pathankot, India

Pathankot, IndiaFlight

On June 3, 1963, a Douglas DC-3 (registration VT-AUL) operated by Indian Airlines was involved in an aviation accident near Pathankot, India in flight. 29 people were killed. Investigators recorded the probable cause as: The accident was caused by structural failure of the aircraft in the air following overstressing as a result of loss of control. 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 1781243876Data APIEditorial standards

A Hiper Dakota on a scheduled flight from Amritsar to Srinagar crashed near Pathankot after losing control during a left turn, killing all 29 occupants.

Accident Sequence

The aircraft departed Amritsar at 1115 LT on a scheduled domestic flight to Srinagar with 29 persons on board. Seven minutes after takeoff, the crew reported the aircraft's position 25 miles from Amritsar. No further communication was received. Shortly after 1200, a telephone report indicated that the aircraft had crashed in a field near Sarna railway station, about five miles west of Pathankot.

Eyewitness Accounts

Eyewitnesses observed the aircraft execute a left turn, after which it went out of control and rapidly lost altitude. The aircraft then assumed a climbing attitude, broke apart in the air, and crashed to the ground, catching fire upon impact. All 29 occupants were killed.

Investigation Findings

The official investigation determined that the accident resulted from structural failure of the aircraft in flight, caused by overstressing following a loss of control. The loss of control was attributed to improper rigging of the rudder bungee system, a component designed to prevent the rudder of the Hiper Dakota from reversing or locking during yawed turns or when encountering a severe side gust. The investigation equally considered that malfunctioning or improper operation of the autopilot may have initiated a yaw and exacerbated the rudder's tendency to lock.

Probable cause

The accident was caused by structural failure of the aircraft in the air following overstressing as a result of loss of control. The loss of control was caused by improper rigging of the rudder bungee system which helps to prevent the marked tendency of the rudder of the Hiper Dakota to reverse or lock under conditions of yawed turn and/or encountering a severe side gust. It is equally likely that malfunctioning or improper operation of the autopilot may have initiated a yaw and accentuated the tendency of the rudder to lock.