ERA23FA078 · Rotorsport UK Ltd CAVALON
Rotorsport UK Ltd CAVALON · Accident: inflight upset during initial climb
Event
- NTSB case
- ERA23FA078
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 1 · all aircraft and ground
- Ground fatalities
- 0
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Rotorsport UK Ltd CAVALON
- Aircraft type
- Rotorsport Uk CAVALON
- Category
- Gyroplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N401GR
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From not recordedTo not recorded
- Aircraft age
- About 3 years (built 2019)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Initial climb
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Inflight upset
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft oper/perf/capability
- Personnel issues › Action/decision
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The sport pilot, who was also the owner of the gyroplane, had about 120 total hours of flight experience, all of which was in the accident gyroplane. During the three months before the accident flight, the gyroplane was in maintenance and the pilot had not flown. Surveillance video captured the accident sequence, and showed the aircraft in the initial climb. It leveled off briefly before resuming its climb while displaying a significant left yaw. Shortly thereafter, the aircraft rolled to the right about 360° and impacted the runway. Recorded data from onboard avionics, as well as postaccident examination of the aircraft, did not reveal any evidence of mechanical malfunction or anomalies that would have precluded normal operation. The rudder trim tab was found undamaged by impact and bent about 30° to the right (left rudder force). The aircraft manufacturer cautioned that extreme sideslip could result in a loss of control. With the aircraft flying sideways, the side of the aircraft faces the oncoming airflow, creating increased drag that tends to swing the fuselage away from the direction of flight. The rotor disc is subsequently pitched down on the side of the aircraft headed into the oncoming airflow. With the airflow above rather than below the rotor disc, the aircraft can rapidly roll over toward the side of the aircraft facing the direction of flight unless urgent corrective action is taken. The reason that the pilot did not take appropriate recovery action could not be determined. Toxicological testing indicated that the pilot had used cannabis, but the timing of his last cannabis use or whether he was impaired by cannabis effects at the time of the accident could not be determined. It is plausible that the pilot’s overcorrection of the aircraft’s yaw may have resulted, in some part, from impairing effects of delta-9-THC; however, the pilot also had not flown in the three months before the accident. Thus, whether the pilot’s use of cannabis contributed to the accident cannot be determined. Additionally, the pilot’s autopsy findings were consistent with high blood pressure’s effect on the heart muscle. The pilot’s disease put him at some increased risk for a sudden impairing or incapacitating cardiovascular event such as heart rhythm abnormality. Such an event cannot be ruled out; however, witness accounts and airport video were not consistent with a sudden medical event. Thus, it is unlikely that the pilot’s heart disease contributed to the accident.
Probable cause
The pilot’s improper yaw control during the takeoff initial climb, which resulted in an excessive sideslip and a subsequent loss of aircraft control.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA23FA078
- Event ID
- 20221204106407
- Case number
- ERA23FA078
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates, cause areas. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 6a2e66131d8c94016b8d5f119a0839f26ea25a85b6b92a23119668ba8769b790; retrieved 2026-09-15T07:54:50.667Z.