Incident Overview

Date: Thursday 9 August 2007
Aircraft Type: de Havilland Canada DHC-6 Twin Otter 300
Owner/operator: Air Moorea
Registration Number: F-OIQI
Location: 1,5 km off Moorea-Temae Airport (MOZ) – ÿ French Polynesia
Phase of Flight: Initial climb
Status: Destroyed, written off
Casualties: Fatalities: 20 / Occupants: 20
Component Affected: Elevator pitch-up control cableElevator pitch-up control cable
Investigating Agency: BEABEA
Category: Accident
A DHC-6 Twin Otter, operated by Air Moorea, experienced a catastrophic accident during flight 1121 off Moorea-Temae Airport in French Polynesia. The aircraft lost pitch control after retracting flaps at approximately 350 feet, resulting in a steep nose-down attitude and subsequent sinking. The incident was caused by a failure of the elevator pitch-up control cable, triggered by wear on a cable to the right of a rope guide, coupled with a jet blast causing the rupture of several strands, and exacerbated by strain during flight. Contributing factors included insufficient pilot training on loss of pitch control, operator negligence in inspection and risk assessment, inadequate consideration of wear phenomena, and a lack of robust risk management practices.A DHC-6 Twin Otter, operated by Air Moorea, experienced a catastrophic accident during flight 1121 off Moorea-Temae Airport in French Polynesia. The aircraft lost pitch control after retracting flaps at approximately 350 feet, resulting in a steep nose-down attitude and subsequent sinking. The incident was caused by a failure of the elevator pitch-up control cable, triggered by wear on a cable to the right of a rope guide, coupled with a jet blast causing the rupture of several strands, and exacerbated by strain during flight. Contributing factors included insufficient pilot training on loss of pitch control, operator negligence in inspection and risk assessment, inadequate consideration of wear phenomena, and a lack of robust risk management practices.

Description

A DHC-6 Twin Otter operated by Air Moorea as flight 1121, departed Moorea-Temae Airport in French Polynesia. After a normal takeoff, the flaps were retracted at around 350 feet. The pilot then lost pitch control of the aeroplane, which adopted a steep nose-down attitude. The pilot was unable to regain control of the aircraft and the Twin Otter struck the sea, broke up and sank. The accident was caused by the loss of airplane pitch control following the failure, at low height, of the elevator pitch-up control cable at the time the flaps were retracted. This failure was due to a sequence of the following: – Large wear of a cable to the right of a rope guide; – External phenomenon, probably jet blast, causing the rupture of several strands; – Failure of the last strands as a result of strain during the flight when using the elevator. The following factors contributed to the accident: – The absence of information and training for pilots on the loss of pitch control; – The operator?s omission of special inspections ; – The failure by the manufacturer and the aviation authorities to fully take into account the wear phenomenon; – The failure by the aviation authorities, airport authorities and operators risk to fully take into account the risks associated with jet blast; – The rules for replacement of stainless steel cables on a calendar basis, without taking into account the activity of the airplane in relation to its type of operation.

Primary Cause

Failure of the elevator pitch-up control cable due to wear on a cable to the right of a rope guide, exacerbated by a jet blast.Failure of the elevator pitch-up control cable due to wear on a cable to the right of a rope guide, exacerbated by a jet blast.

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