Incident Overview

Date: Monday 20 February 1967
Aircraft Type: Douglas DC-6
Owner/operator: SAHSA – Servicio A‚reo de Honduras SA
Registration Number: HR-SAS
Location: Tegucigalpa-Toncontin Airport (TGU) – ÿ Honduras
Phase of Flight: Landing
Status: Destroyed, written off
Casualties: Fatalities: 4 / Occupants: 55
Component Affected: Propeller reversal system.Propeller reversal system.
Category: Accident
A DC-6 aircraft, SAHSA Flight 203, experienced a catastrophic accident during a short flight to Tegucigalpa. The aircraft failed due to a malfunction of the reverse pitch control mechanism, resulting in a series of events including tire burst, ground loop, and fire. The crew were unable to maneuver the throttles into reverse, leading to the brakes being used. The aircraft’s propeller reversal system failed, and the aircraft subsequently ran off the runway.A DC-6 aircraft, SAHSA Flight 203, experienced a catastrophic accident during a short flight to Tegucigalpa. The aircraft failed due to a malfunction of the reverse pitch control mechanism, resulting in a series of events including tire burst, ground loop, and fire. The crew were unable to maneuver the throttles into reverse, leading to the brakes being used. The aircraft’s propeller reversal system failed, and the aircraft subsequently ran off the runway.

Description

SAHSA Flight 203 took off from La Mesa at 08:15 for a 32-minute flight to Tegucigalpa. The flight was uneventful and the crew were assigned runway 01 for landing. The landing was normal and smooth, but the propeller reverser system failed. The crew were unable to move the throttles into the reverse-position. The aircraft had passed the point were a go-around could be attempted, so the brakes were used. The two outermost tires from the main gear legs burst. Nearing the end of the runway, a ground-loop was attempted. The DC-6 ran off the runway and the nose gear ran into a ditch, followed by the left main gear leg. The left wing fuel tank burst and the aircraft caught fire. PROBABLE CAUSE: “According to the reports by the crew, the probable cause of the accident was the failure of the reverse pitch control mechanism. The Board was not able to confirm or deny this because the fire had obliterated all traces of any possible cause.”

Primary Cause

Failure of the reverse pitch control mechanism.Failure of the reverse pitch control mechanism.

Share on:

Leave a Reply

Your email address will not be published. Required fields are marked *