ASN Wikibase Occurrence # 154328
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Sunday 6 June 1999 |
Time: | 18:05 LT |
Type: | Aces High Cuby II |
Owner/operator: | Private |
Registration: | G-BVNA |
MSN: | PFA 257-1258 |
Fatalities: | Fatalities: 2 / Occupants: 2 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | near the Giant's Causeway, North Antrim coast, Northern Ireland -
United Kingdom
|
Phase: | En route |
Nature: | Private |
Departure airport: | Mullaghmore Airfield, County Antrim |
Destination airport: | Mullaghmore Airfield, County Antrim |
Investigating agency: | AAIB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:G-BVNA was flying near the Giant's Causeway in Northern Ireland with a strong on-shore breeze & was seen to cross the coastline. Witnesses saw G-BVNA at approx 800 feet agl with one of its wings "Folded up about 1/2 to 1/3 along its length" & then saw the aircraft in a descending spiral to the ground.
Both occupants were killed in the impact. Two accompanying microlights experienced severe turbulence & could not land nearby. Weather aftercasts indicated surface wind at 010 degrees/20 knots & 2,000 feet wind at 020 degrees/28 knots.
G-BVNA was the only Cuby II kit imported into the UK. The Canadian manufacturer was later dissolved but production of a derivative aircraft, the Eurocub, continued in Hungary. There had been a static structural test in Hungary but not including torsional loadings.
The wing rib structure was of lightweight construction. Upward failure of the RH outer wing panel resulted from a failure of both spars just inboard of the wing strut, main spar failing first. In the L/H wing, there was incipient buckling damage, putting the left wing close to a similar collapse.
This loading probably included extra load factor applied by rearward stick movement.
CAA Closure: The hazard is adequately controlled by existing requirements, procedures and documentation. Registration G-BVNA cancelled by the CAA on 22 September 1999 ass "destroyed" and owner's "Addressee Status: Deceased"
Accident investigation:
|
| |
Investigating agency: | AAIB |
Report number: | |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
1. AAIB:
http://www.aaib.gov.uk/cms_resources.cfm?file=/dft_avsafety_pdf_501463.pdf 2. CAA:
http://www.caa.co.uk/aircraft-registration/ Revision history:
Date/time | Contributor | Updates |
21-Mar-2013 07:33 |
ryan |
Added |
25-May-2013 02:38 |
Dr. John Smith |
Updated [Time, Cn, Other fatalities, Location, Source, Narrative] |
15-Mar-2015 18:59 |
Dr. John Smith |
Updated [Operator, Departure airport, Destination airport, Source, Narrative] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation