Incident Overview

Date: Sunday 13 June 1999
Aircraft Type: de Havilland Canada DHC-3 Otter
Owner/operator: Air Wilga Inc.
Registration Number: C-FEYY
Location: Riviere Des Prairies, QC – ÿ Canada
Phase of Flight: Taxi
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 2
Component Affected: Fuel pressure sensor fittingFuel pressure sensor fitting
Category: Accident
A DHC-3 float-equipped aircraft experienced a fire during an experimental flight following installation of the Orenda OE-600 V-8 engine. Flames were observed from the cowl flap and ahead of the windshield, leading to immediate engine shutdown. The pilot attempted extinguishing the fire with a portable extinguisher, requiring significant time to reach the shore. Municipal firefighters quickly contained the fire, resulting in damage to the firewall and engine installation. A fuel pressure sensor fitting was found to be broken, causing overheating.A DHC-3 float-equipped aircraft experienced a fire during an experimental flight following installation of the Orenda OE-600 V-8 engine. Flames were observed from the cowl flap and ahead of the windshield, leading to immediate engine shutdown. The pilot attempted extinguishing the fire with a portable extinguisher, requiring significant time to reach the shore. Municipal firefighters quickly contained the fire, resulting in damage to the firewall and engine installation. A fuel pressure sensor fitting was found to be broken, causing overheating.

Description

The float-equipped DHC-3 was to make an experimental flight following installation of the Orenda OE-600 V-8 engine. The aircraft was taxiing toward the wharf when flames were observed coming from the cowl flap and ahead of the windshield. The engine was immediately shut down. The pilot then exited the aircraft and tried to extinguish the fire using a portable fire extinguisher. It took the crew a number of minutes to reach the shore and obtain more fire extinguishers to fight the fire. The municipal firefighters arrived approximately 9 minutes later, and quickly brought the fire under control. The aircraft sustained damage to the forward part of the firewall and behind the Orenda engine installation. Examination of the aircraft showed that the fuel pressure sensor fitting (an aluminum part) was broken and that it had overheated.

Primary Cause

Fuel pressure sensor fitting failure leading to overheating.Fuel pressure sensor fitting failure leading to overheating.

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