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: | Friday 7 April 2023 |
Time: | 08:27 UTC |
Type: | Piper PA-28-180 Cherokee Archer II |
Owner/operator: | Cambourne Insurance Services Ltd |
Registration: | G-AXSG |
MSN: | 28-5605 |
Year of manufacture: | 1970 |
Engine model: | Lycoming O-360-A4A |
Fatalities: | Fatalities: 0 / Occupants: 3 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | St Marys Airport, Hugh Town, Isle of Scilly -
United Kingdom
|
Phase: | Landing |
Nature: | Private |
Departure airport: | Henstridge Airport (EGHS) |
Destination airport: | Isles Of Scilly-St. Mary's Airport (ISC/EGHE) |
Investigating agency: | AAIB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The Piper PA-28-180 (G-AXSG) experienced a runway excursion after landing due to the landing gear collapsing at St Mary’s Airport, Isles of Scilly.
On touchdown the left main landing gear collapsed. The cause of the collapse was failure of both upper torque link attachment lugs on the landing gear cylinder due to fatigue cracking. There is a known history of fatigue cracking on cast landing gear cylinders and a manufacturer’s Service Bulletin exists to regularly inspect the area around the attachment lugs. There is currently no Airworthiness Directive to mandate the Service Bulletin.
One Safety Recommendation is made to the CAA to ensure that the level of safety of cast main landing gear cylinders fitted to PA-28 and PA-32 aircraft is acceptable."
=Safety Recommendation 2024-001=
It is recommended that the Civil Aviation Authority undertakes an unsafe condition assessment, in accordance with the requirements of UK Regulation (EU) No 748/2012 Annex I Part 21.A.3, for the cast main landing gear cylinder cracking affecting PA-28 and PA-32 aircraft, and take appropriate action based on the outcome of the assessment.
=AAIB Conclusion=
The left main landing gear torque link attachment lugs failed due to fatigue cracking, causing the wheel assembly and oleo to come out of the landing gear cylinder on landing.
While a Servicing Bulletin exists to inspect the landing gear for fatigue cracking, the EASA Airworthiness Directive mandating the inspection was cancelled in 2020 due to the perceived low number of cast aluminium
cylinders in service and the level of risk of failure.
The Servicing Bulletin was carried out on G-AXSG, with the landing leg still fitted to the aircraft. It is possible that the fatigue cracks were present but were not detected using the dye penetrant inspection technique.
Accident investigation:
|
| |
Investigating agency: | AAIB |
Report number: | AAIB-29086 |
Status: | Investigation completed |
Duration: | 10 months |
Download report: | Final report |
|
Sources:
1. AAIB Final Report:
https://assets.publishing.service.gov.uk/media/65ba505fc75d30000dca0fb4/Piper_PA-28-180_G-AXSG_03-24.pdf 2. G-AXSG history 1969-1973:
https://cwsprduksumbraco.blob.core.windows.net/g-info/HistoricalLedger/G-AXSG-1.pdf 3. G-AXSG history 1973-1975:
https://cwsprduksumbraco.blob.core.windows.net/g-info/HistoricalLedger/G-AXSG-2.pdf 4.
https://www.flightradar24.com/data/aircraft/g-axsg 5.
https://www.planelogger.com/Aircraft/Registration/G-AXSG/ 6.
https://en.wikipedia.org/wiki/St_Mary%27s_Airport,_Isles_of_Scilly#
History of this aircraft
G-AXSG was built in 1969 (first registered 17.11.69) and was with its 15th owner from new at the time of the above incident.
Location
Media:
Revision history:
Date/time | Contributor | Updates |
01-Feb-2024 15:31 |
Dr. John Smith |
Added |
01-Feb-2024 15:33 |
harro |
Updated [Other fatalities, Departure airport, Embed code, Narrative, Accident report] |