CEN13LA514
2013-08-28 · Emporia, Kansas, United States · Minor · 1 aircraft · Status: Completed
Aircraft involved
Probable cause & findings
The right wing’s folding up in flight for reasons that could not be determined because an examination did not reveal any abnormalities with the airframe that would have precluded normal operation.
Factual narrative
On August 28, 2013, about 1130, central daylight time, an unregistered, light sport Challenger II airplane, impacted trees and terrain near the Emporia Municipal Airport (KEMP), Emporia, Kansas. The airline transport rated pilot, sole occupant, received minor injuries and the airplane sustained substantial damage. The airplane was owned and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Day visual meteorological conditions prevailed and no flight plan was filed. The flight departed Herington Regional Airport (KHRU) at an unknown time and was en route to Joplin, Missouri. According to the pilot, he had just purchased the airplane and was in process of flying the airplane back to his home airfield. As he approached KEMP, part of the right wing folded up, and the airplane descended in a spiral. The airplane impacted trees and came to rest near a creek. The pilot reported that the engine was still running and was able to exit the airplane to get help. The airplane's experimental-amateur built data plate annotated the airplane as a Challenger II UL trainer, serial number CH2-0600-R-1983, with a date of manufacture of 06/02/2002 and listed an individual builder. The data plate also listed the empty weight as 358 lbs and an 800 lbs gross weight. There was no record of an experimental-light sport airworthiness certificate, or aircraft registration in accordance with the Light Sport Aircraft rule, that was effective January 2008. The accident pilot added that he did not have any of the airplane's previous owner records. The airplane was recovered to the Emporia airport, where inspectors from the Federal Aviation Administration, examined the airplane. The inspectors examined the fractured airframe's tubing. They reported that all of the fractured surfaced indicated static overload. The inspectors were unable to find any fatigue cracks or anomalies with the airframe that would account for the wing failure The pilot was ferrying the experimental, amateur-built airplane back to his home airport. As he approached an en route airport, part of the right wing folded up, and the airplane spiraled down. The airplane impacted trees and came to rest near a creek. The airplane did not have an airworthiness certificate or registration number. Examination of the wreckage revealed no preexisting damage that would have precluded normal operation. The pilot did not have any of the airplane's previous records; the reason for the right wing folding could not be determined. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft structures-Wing structure-(general)-Failure - C
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2013_CEN13LA514.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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