Incident Overview

Date: Wednesday 17 March 1965
Aircraft Type: Handley Page HPR-7 Herald 202
Owner/operator: Eastern Provincial Airways
Registration Number: CF-NAF
Location: Upper Musquodoboit, NS – ÿ Canada
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 8 / Occupants: 8
Component Affected: Underfloor fuselage skinUnderfloor fuselage skin
Category: Accident
Eastern Provincial Flight 102 experienced a catastrophic structural failure during flight due to a ruptured underfloor fuselage skin. The incident occurred after climbing through FL120 and resulted in immediate separation of the nose and front fuselage, leading to control lever failures and subsequent debris dispersal in heavily wooded terrain. The probable cause was corrosion in the underfloor area, specifically along stringer No. 32, which caused structural failure.Eastern Provincial Flight 102 experienced a catastrophic structural failure during flight due to a ruptured underfloor fuselage skin. The incident occurred after climbing through FL120 and resulted in immediate separation of the nose and front fuselage, leading to control lever failures and subsequent debris dispersal in heavily wooded terrain. The probable cause was corrosion in the underfloor area, specifically along stringer No. 32, which caused structural failure.

Description

Eastern Provincial Flight 102 departed Moncton at 06:35 on a flight to Torbay with several intermediate stops. The Herald departed Halifax’s runway 33 at 09:10 and was instructed to turn right and climb to FL130. While climbing through FL120 the underfloor fuselage skin ruptured. It opened up sufficiently to be contacted by one of the propellers. Disruption of the structure and subsequent progressive separation of the nose and front fuselage resulted in failures of the control levers. Separation of the remaining empennage and the aft section of the fuselage followed instantaneously. The debris came down in heavily wooded rolling terrain. PROBABLE CAUSE: “Failure of corroded skin area along the bottom centre line of the aircraft beneath stringer No.32 which resulted in structural failure of the fuselage and aerial disintegration.”

Primary Cause

Corrosion in the underfloor area along stringer No. 32Corrosion in the underfloor area along stringer No. 32

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