Accident Quad City Challenger II N448WM,
ASN logo
ASN Wikibase Occurrence # 80423
 
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:Monday 1 November 2010
Time:14:15
Type:Silhouette image of generic quad model; specific model in this crash may look slightly different    
Quad City Challenger II
Owner/operator:Private
Registration: N448WM
MSN: CH2-1002-2263
Engine model:Bombardier Rotax
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Sauk County, 3 miles north of Sauk Prairie Airport, Prarie du Sac, WI -   United States of America
Phase: En route
Nature:Private
Departure airport:Prairie Du Sac, WI (91C)
Destination airport:Merrill, WI (RRL)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The airplane impacted the ground following an in-flight separation of the left wing during cruise flight. The pilot, who was the sole occupant, was fatally injured. Witnesses reported seeing the airplane traveling north, about 300-500 feet above ground level, when one wing suddenly separated from the airplane. One of the witnesses stated that the other wing separated shortly after the first one. Postaccident examination confirmed that both wings were completely separated from the airplane with the exception of the right wing aft spar and aileron. Examination of the fractures in the wing attachment fittings revealed signatures consistent with overload failure with the exception of one fitting that had no perceptible damage due to deformation or fracture. The attachment bolt for the fitting that showed no perceptible overload damage was not recovered during the investigation; however, the relative lack of damage to the strut fitting indicates that the attachment bolt either failed, or its corresponding nut had loosened and separated during the flight. A portion of wing fabric retained for testing showed that the fabric met the minimum performance requirements as set forth in regulations. No preaccident defects were found with regard to the components examined.
Probable Cause: The separation of the fuselage-mounted wing strut attachment fitting for an undetermined reason, which resulted in the separation of the left wing of the airplane.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN11LA050
Status: Investigation completed
Duration: 1 year and 9 months
Download report: Final report

Sources:

NTSB
FAA register: http://www.wiscnews.com/news/article_73e0f122-e62f-11df-8b49-001cc4c03286.html
http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N448WM
http://www.airnav.com/airport/91C

Location

Media:

Revision history:

Date/timeContributorUpdates
02-Nov-2010 08:52 gerard57 Added
02-Nov-2010 15:21 Anon. Updated [Aircraft type, Registration, Cn, Operator, Other fatalities, Location, Departure airport, Destination airport, Source]
03-Nov-2010 14:22 harro Updated [Embed code]
21-Dec-2016 19:25 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
26-Nov-2017 18:37 ASN Update Bot Updated [Cn, Other fatalities, Departure airport, Destination airport, Source, Narrative]

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