Incident Overview

Date: Tuesday 19 November 2002
Aircraft Type: Boeing 727-230F
Owner/operator: DHL European Air Transport
Registration Number: OO-DHY
Location: East Midlands Airport (EMA/EGNX) – ÿ United Kingdom
Phase of Flight: Take off
Status: Substantial
Casualties: Fatalities: 0 / Occupants: 3
Component Affected: No 1 engineNo 1 engine
Investigating Agency: AAIBAAIB
Category: Accident
A significant damage occurred to No 1 engine during a takeoff from East Midlands Airport, Castle Donington, Leicestershire. The crew reported a loud grinding sound and subsequent engine failure light, leading to an immediate abort of takeoff at approximately 30 kt. Subsequent examination revealed significant fire damage to the underside of the engine, evidence of penetration from inside the engine casing, and a fracture of a low-pressure compressor fan blade. No cowl penetration was observed.A significant damage occurred to No 1 engine during a takeoff from East Midlands Airport, Castle Donington, Leicestershire. The crew reported a loud grinding sound and subsequent engine failure light, leading to an immediate abort of takeoff at approximately 30 kt. Subsequent examination revealed significant fire damage to the underside of the engine, evidence of penetration from inside the engine casing, and a fracture of a low-pressure compressor fan blade. No cowl penetration was observed.

Description

Substantial Damage to No 1 engine on take off run from East Midlands Airport, Castle Donington, Leicestershire. According to the following excerpt from the official AAIB report into the accident: “The crew reported a loud grinding sound immediately followed by illumination of the ‘engine failure’ light. They aborted the takeoff at approximately 30 kt and as the thrust levers were closed the commander was aware of resistance within the No 1 thrust lever system. Subsequent examination revealed significant fire damage centred around the underside of No 1 engine, evidence of penetration from inside the engine casing and a fracture of a second stage low pressure (LP) compressor fan blade at the root attachment. There was no evidence of cowl penetration.”

Source of Information

https://assets.publishing.service.gov.uk/media/5422ff6440f0b61342000927/dft_avsafety_pdf_026142.pdf, https://publicapps.caa.co.uk/docs/33/factor200403.pdf, http://www.skystef.be/regi/OO-DHY.htm, https://commons.wikimedia.org/wiki/File%3ABoeing_727-230-Adv(F)%2C_DHL_(European_Air_Transport_-_EAT)_AN0219187.jpghttps://assets.publishing.service.gov.uk/media/5422ff6440f0b61342000927/dft_avsafety_pdf_026142.pdf, https://publicapps.caa.co.uk/docs/33/factor200403.pdf, http://www.skystef.be/regi/OO-DHY.htm, https://commons.wikimedia.org/wiki/File%3ABoeing_727-230-Adv(F)%2C_DHL_(European_Air_Transport_-_EAT)_AN0219187.jpg

Primary Cause

Engine failure due to a penetrating fire.Engine failure due to a penetrating fire.

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