Loss of Control in Flight · NTSB ERA24LA185
Bailey-Moyes Dragonfly — Groveland, FL
| Date | April 19, 2024 |
| Location | Groveland, FL |
| Aircraft | Bailey-Moyes Dragonfly (amateur-built) |
| Purpose of flight | Personal |
| Conditions | Day · Visual Meteorological Cond |
| Phase / occurrence | Uncontrolled descent Collision with terr/obj (non-CFIT) |
| Pilot age | 71 |
| Pilot total time | 1,432 hrs · Experienced |
| Time in type | 1,432 hrs |
| Fatalities | 1 |
Probable cause
NTSB findings
- Aircraft-Aircraft structures-Wing structure-Main frame (on wing)-Not installed/available
- Aircraft-Aircraft structures-Wing structure-Main frame (on wing)-Incorrect service/maintenance
- Personnel issues-Task performance-Maintenance-Installation-Owner/builder
- Personnel issues-Task performance-Inspection-Preflight inspection-Pilot
- Aircraft-Fluids/misc hardware-Misc hardware-Fasteners-Inadequate inspection
What happened
According to witnesses, the airplane departed and climbed to an altitude about 200 to 300 ft above ground level and then turned before the right wing “folded upward” and the airplane descended in a spiral to the ground. Postaccident examination revealed that the right lower wing strut attachment was not properly assembled; the bolt intended to connect the wing strut block to the fuselage bulkhead was threaded through the fuselage structure and tightened, but had not passed through the hole in the strut block, resulting in no load-bearing connection between the wing strut and the fuselage. The absence of deformation or damage to the bolt and wing strut block at the attachment point was consistent with the improper installation of the bolt.
Without the structural support of the right lower wing strut, the wing was unable to sustain the aerodynamic loads encountered during the initial climb, resulting in an in-flight structural failure of the right wing. The accident flight was the airplane’s first flight since it was assembled by the pilot. The airplane was unregistered and had not been issued an airworthiness certificate or operating limitations, nor had it been inspected by a designated airworthiness representative or an FAA inspector before the flight.