ASN Wikibase Occurrence # 209346
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Date: | Friday 26 May 2017 |
Time: | 10:30 UTC |
Type: | de Havilland Canada DHC-8-402Q Dash 8 |
Owner/operator: | Flybe |
Registration: | G-PRPH |
MSN: | 4323 |
Year of manufacture: | 2001 |
Engine model: | Rotax 912 ULS |
Fatalities: | Fatalities: 0 / Occupants: 57 |
Aircraft damage: | Minor |
Category: | Serious incident |
Location: | near Manchester Airport (MAN/EGCC) -
United Kingdom
|
Phase: | En route |
Nature: | Passenger - Scheduled |
Departure airport: | Edinburgh-Turnhouse Airport (EDI/EGPH) |
Destination airport: | Manchester Airport (MAN/EGCC) |
Investigating agency: | AAIB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:Towards the end of flight BE292, the Central Warning System indicated an oil pressure loss on the No 2 engine. The engine was shut down and an uneventful single engine landing was carried out at Manchester Airport.
It was found that a cap locating the propeller overspeed governor test solenoid had detached, allowing most of the oil from the No 2 engine lubrication system to be lost. Investigation of the component revealed that the four cap securing bolts had failed, predominantly in fatigue. Extensive investigation failed to identify conclusively the root cause of the bolt fatigue damage. Although three similar in-service failures of these bolts have occurred on other aircraft types utilising this design of governor, no others have been recorded on DHC-8-400 types and all those that have occurred have been on units of an earlier modification state.
Accident investigation:
|
| |
Investigating agency: | AAIB |
Report number: | EW/C2017/09/06 |
Status: | Investigation completed |
Duration: | 10 months |
Download report: | Final report |
|
Sources:
https://assets.publishing.service.gov.uk/media/5aa7dea7e5274a3e3603aaa8/DHC-8-402_G-PRPH_04-18.pdf Revision history:
Date/time | Contributor | Updates |
15-Apr-2018 17:14 |
harro |
Added |
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