Loss of control Accident Zenair CH 601 Zodiac 59-ABO,
ASN logo
ASN Wikibase Occurrence # 23837
 
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 17 August 2003
Time:19:00
Type:Silhouette image of generic CH60 model; specific model in this crash may look slightly different    
Zenair CH 601 Zodiac
Owner/operator:private
Registration: 59-ABO
MSN:
Fatalities:Fatalities: 2 / Occupants: 2
Aircraft damage: Destroyed
Category:Accident
Location:Egletons Airfield (LFDE) -   France
Phase: Approach
Nature:Private
Departure airport:Caudecoste Airfield
Destination airport:Egletons Airfield (LFDE)
Investigating agency: BEA
Confidence Rating: Accident investigation report completed and information captured
Narrative:
During a gathering of microlights at Egletons airfield, the participants were navigating to Caudecoste (47) and then returned to Egletons at the end of the day.
Witnesses on the ground indicate that they observed the ultralight integrate into the right hand airfield circuit and arrive on final for runway 25 on a normal glide path. They then saw it, at a height of about 60 meters, "stall on the right wing and go into a spin" before disappearing behind some trees.
Examination of the wreckage and the site showed that the ultralight had hit the ground while in a right-hand rotation and with a nose-down attitude of about 45°.
On arrival of the rescue team, the wreckage was soaked and still contained fuel. Examination of the engine shows that it was not delivering power but was operating at low rpm at the time of impact (this observation is consistent with a reduced engine approach).
Witnesses mention the passage of showers, brief and heavy at the time of the occurrence, which made the paved runway glare when landing into the sun. However, none of the pilots indicated that they had flown through any of these in the airfield circuit.
This ultralight was not equipped with a stall warning device.
The attitude of the ultralight during its fall was characteristic of a low speed stall. The deteriorating weather conditions and the glare may have confused the pilot to the point that he did not monitor his approach speed. The low height did not allow him to regain control of the ultralight before the collision with the ground.

Accident investigation:
cover
  
Investigating agency: BEA
Report number: 
Status: Investigation completed
Duration:
Download report: Final report

Sources:

https://www.bea.aero/docspa/2003/59-o030817/htm/59-o030817.html
http://www.bea.aero/docspa/2003/59-o030817/pdf/59-o030817.pdf

Revision history:

Date/timeContributorUpdates
27-Sep-2008 01:00 ASN archive Added
15-Apr-2009 10:35 harro Updated
21-Nov-2022 20:34 Ron Averes Updated [Location]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org