ZENITH AIRCRAFT CO ZODIAC 601 XL near Agnos, AR — 2009-11-06
- Date
- 2009-11-06
- Location
- Agnos, AR, USA
- Aircraft
- ZENITH AIRCRAFT CO ZODIAC 601 XL
- Registration
- N538CJ
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Climb
Probable cause
The in-flight separation of both wings due to aileron flutter. The aileron flutter was the result of inadequate wing stiffness and strength and the lack of aileron counterbalances.
NTSB narrative
The light-sport airplane experienced an in-flight break-up during a cross-country flight. Flight track data recovered from an onboard global positioning system, and a subsequent performance study, depicted the airplane was maneuvering between the altitudes of 2,500 and 3,500 feet at airspeeds between about 60 and 108 knots calibrated airspeed (KCAS). The airplane performed a number of turns and maneuvers during the hour-plus flight, including a landing approach and pass over an airport. The calculated bank angle for the entire flight never exceeded 30 degrees. At the time when the breakup occurred, the airplane was climbing at about 500 feet per minute through 2,800 feet altitude and had accelerated to 100 KCAS. The estimated angle of attack was about 3 degrees during the last minute of the flight, and the airplane wreckage was spread over 600 feet on the ground. An examination of the airplane wreckage revealed compression buckling and upward and downward bending of both wings. The upward and downward movement, twisting, and flexing of the airplane wing surface was consistent with the occurrence of aerodynamic flutter. In addition, damage was noted on the flap assemblies consistent with over travel. Ultimately both wings failed in down bending. An examination of the engine revealed no anomalies. The accident pilot was experienced in the accident airplane and had built the airplane from a kit.
Analysis
- Primary failure mode
- Controlled flight into terrain
- First missed decision gate
- Pilot could have addressed flutter concerns before the flight.
NTSB coding
Evidence available
- ADS-B / radar
- Photos
- 19 docket documents
Docket documents19
- Aircraft Performance 13 - Aircraft GPS Data Studyform
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementinterview
- 601XL FAILURE RATESother
- AMD Safety Alert-Safety Directive - Rev 1other
- FAA SAIB CE-10-08other
- GPS 17 - Attachment 1other
- STRUCTURES 7 - STRUCTURES STUDYother
- Photograph 01 - Main Wreckage - Left Sidephotos
- Photograph 02 - Main Wreckage - Forward Viewphotos
- Photograph 03 - Main Wreckage - Right Sidephotos
- Photograph 04 - Main Wreckage - Rear Viewphotos
- Photograph 05 - Left Wingphotos
- Photograph 06 - Right Wingphotos
- Photograph 07 - Aerial View of Wreckage Distribution (Provided by Insurance Company)photos
- STRUCTURES 7 - STRUCTURES PHOTOS - 31 PHOTOGRAPHSphotos
- GPS 17 - Factual Report of Group Chairmanreport
- Toxicological Reportreport
Related mishaps
- Sting Sport TL-2000
2025-06-20 · Dunavant, VA
- EUROCOPTER DEUTSCHLAND GMBH MBB-BK 117 C-1
2025-05-19 · Fort Washington, PA
- CESSNA 150J
2025-02-16 · Minersville, UT
- CESSNA 172P
2025-02-03 · Clarksville, TN
- JONES LONG-EZ
2024-07-10 · Thomasville, GA
- ROTORWAY Scorpion 133
2024-07-05 · Andale, KS · 1 fatality