ERA23FA070 · Robinson Helicopter R44
Robinson Helicopter R44 · Accident: system/component malfunction/failure (non-power) while maneuvering
From WBTV Heliport (NC90) to an unrecorded destination
Event
- NTSB case
- ERA23FA070
- 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
- 2 · all aircraft and ground
- Ground fatalities
- Unknown
- 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
Robinson Helicopter R44
- Aircraft type
- Robinson R44
- Category
- Helicopter
- 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
- N7094J
- Operator
- Total Traffic & Weather Network
- Onboard fatalities
- Unknown
- Route
- From WBTV Heliport (NC90), Charlotte, NCTo not recorded
- Aircraft age
- About 23 years (built 1999)
- 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
- Maneuvering
- 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
- System/component malfunction/failure (non-power)
- 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 propeller/rotor
- Personnel issues › Task performance
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The purpose of the flight was to provide video training for a local staff meteorologist over a simulated news scene. About 5 minutes into the flight, the pilot began a series of left, 360° orbits over an interstate highway. During the third orbit, helicopter control was lost and the helicopter entered a steep descent until it impacted a grassy area adjacent to the highway. The pilot made a radio call before impact stating that they were “going down.” The helicopter impacted a grassy area adjacent to an interstate highway. There was no postaccident fire. An examination of the helicopter’s flight controls after the accident revealed the forward left control rod end that should have been connected to the stationary swashplate on the main rotor was disconnected and the connecting hardware was missing. A metallurgical examination of the remaining components suggested that the connecting hardware, including a threaded bolt, nut, palnut, two washers, and two hat-shaped spacers were loose and backed out during the flight. It is unlikely that the hardware was secure before the flight and may have been loose for multiple flights before the accident. Additional examination of the remaining hardware revealed that one of the two spacers was installed backwards, most likely during the field overhaul of the helicopter about three years before the accident. The subject hardware was required to be inspected for security by the pilot during each preflight inspection and by maintenance personnel at each 100-hour/annual inspection. The pilot tested positive for quinine and the pain reliever tramadol and was under a physician’s care for arthritis and polyarthralgia that was unreported to the Federal Aviation Administration. However, based on the mechanical issues and the actions of the pilot immediately before the accident, performance impairments were not an issue. Thus, it is unlikely that the effects from the pilot’s use of quinine and tramadol were factors in this accident.
Probable cause
The inadequate inspections of the forward left control rod end attachment hardware to the stationary swashplate by the pilot and by maintenance personnel, resulting in an eventual loosening and backing out of the hardware and subsequent loss of helicopter control.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA23FA070
- Event ID
- 20221122106348
- Case number
- ERA23FA070
- 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: 47ebaf200312d2eee53efb09706eab5973ecfce6da7745b445001f216cfff84c; retrieved 2026-09-15T07:54:26.306Z.