Incident Overview

Date: Monday 3 June 1963
Aircraft Type: Douglas DC-3 Hiper
Owner/operator: Indian Airlines
Registration Number: VT-AUL
Location: Sarna – ÿ India
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 29 / Occupants: 29
Component Affected: Rudder bungee system.Rudder bungee system.
Category: Accident
A Hyper DC-3 aircraft, operating from Amritsar, Srinagar, took off at 11:15 and lost contact with the flight at 11:23. No further communication was received. Investigation indicates a probable cause of structural failure resulting from overstressing due to loss of control, exacerbated by improper rudder bungee rigging.A Hyper DC-3 aircraft, operating from Amritsar, Srinagar, took off at 11:15 and lost contact with the flight at 11:23. No further communication was received. Investigation indicates a probable cause of structural failure resulting from overstressing due to loss of control, exacerbated by improper rudder bungee rigging.

Description

The Hiper DC-3 took off from Amritsar at 11:15 for a flight to Srinagar. Last radio contact with the flight was at 11:23 when the crew reported 25 miles from Amritsar. Nothing more was heard from the flight. 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 mal-functioning or improper operation of the autopilot may have initiated a yaw and accentuated the tendency of the rudder to lock.”

Primary Cause

Structural failure of the aircraft due to overstressing resulting from loss of control.Structural failure of the aircraft due to overstressing resulting from loss of control.

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