MOYES DRAGONFLY near Ridgely, MD — 2011-07-23
- Date
- 2011-07-23
- Location
- Ridgely, MD, USA
- Airport
- RJD
- Aircraft
- MOYES DRAGONFLY
- Registration
- N402HA
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Initial climb
Probable cause
An in-flight loss of control for reasons that could not be determined during postaccident examinations.
NTSB narrative
The flight instructor who was towed aloft by the tow airplane with his student in a tandem hang glider reported that the airplane did not lift off until it was near the end of the grass runway. A witness reported that, after the airplane released the glider, it began to turn left while climbing until it completed a 270-degree turn, reached a peak altitude of about 270 feet above ground level, then entered a spin, rotated one to two times, and subsequently impacted the ground. Postaccident examination of the engine revealed no evidence of any preimpact failures or malfunctions that would have precluded normal operation. Further, no evidence was found indicating that a flight control malfunction occurred or that the tow rope became entangled. During examinations, one of the airplane's bracing cables, which strengthened and stiffened the airplane's structure and normally extended from the upper surface of the right wing to a plate above the tailwheel, was found on the ground beneath the right wing with both of its ends broken from the airplane structure attachment points. The cable had fractured in overload in the eye splice sleeves at both ends. Although failure of this cable might have distorted the airplane's structure in flight and resulted in controllability challenges, it could not be determined if the cable failed in flight or during the impact sequence. It is also possible that the pilot became distracted during the climb while watching the hang glider after the release and allowed the airspeed to degrade, which resulted in an aerodynamic stall and subsequent spin.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have aborted the flight after towline release.
NTSB coding
Evidence available
- FDR / data
- Photos
- 34 docket documents
Docket documents34
- Aircraft Performance Informationform
- Parametric Performance Studyform
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Additional Witness Statements and Interview Summariesinterview
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statements and Interview Summariesinterview
- Airplane Three view Drawing as Provided by LiteFliteother
- Cable Measurementsother
- Excerpts From AC 43.13-1Bother
- Excerpts From Flight and Operations Manual - Preflight and Disassembly (Pre Accident)other
- Excerpts From LiteFlite Dragonfly C Model Assemby Instructions (Pre Accident)other
- Excerpts From Pitman Air SLSA Maintenance Manual (Post Accident)other
- Flytec 4500 Recorded Dataother
- Receipt of Aircraft Partsother
- Transport Canada TP7317 Aviation Safety Ultralight and Balloon 1/1999other
- Weather Observations and Records (KESN METARs)other
- Photo 10: Photograph of Exemplar Dragonfly(Showing Thimble Wear)photos
- Photo 11: Photograph of Exemplar Dragonfly (Showing Broken Wire)photos
- Photo 12: Photograph of Exemplar Dragonfly (Showing Unrepaired Tear in Fabric)photos
- Photo 1: Photograph of Main Wreckagephotos
- Photo 2: Close Up Photograph of Main Wreckage (Front View)photos
- Photo 3: Right Upper Wing Cable Attach Point (Showing Missing Bracing Cable)photos
- Photo 4: Close Up Photograph of Right Upper Wing Cable Attach Point (Showing Missing Bracing Cable and Cracked Thimble on Adjacent Cablephotos
- Photo 5: Photograph of Right Lower Aft Boom Cable Attach Point (Showing Missing Cable)photos
- Photo 6: Photograph of Elongated Bolt Hole in Structural Tubingphotos
- Photo 7: Photograph of Wear Around Bolt Hole in Boom Tube (Showing Evidence of Movement)photos
- Photo 8: Photograph of Exemplar Dragonfly (Showing Elongated Bolt Hole and Thimble Wear)photos
- Photo 9: Photograph of Exemplar Dragonfly (Showing Elongated Bolt Hole in Tang)photos
- Satellite Image of Accident Sitephotos
- Excerpts From Pitman Air SLSA POH and FTS - Preflight, Disassembly, and Safety Reporting (Post Accident)report
- Materials Laboratory 15 - Factual Report 12-044.report
- Pilot Toxicological Reportreport
- Wreckage Diagramwreckage
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