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Atlas / NTSB / ERA23LA289

NTSB CAROL · Event

Event ERA23LA289

2023-06-27 Anderson, South Carolina, United States Airport · AND None 1 aircraft Status: Completed

Registry · N90270

FAA Aircraft Registry record.

Make / Model

HUGHES 269A

Year of manufacture

1966 · 57 years old at event

TCDS

4H12 · SCHWEIZER RSG LLC

Engine

LYCOMING HIO-360 SER (205 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

19790405

ADS-B equipped

Yes — Mode-S AC7A00

Registrant of record

DUNN LARRY W

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The mechanics’ improper torquing of the main rotor blade dampers, which resulted in a ground resonance event during landing.

Factual narrative

Prior to the accident flight, the pilot reported experiencing vibrations in the helicopter. The pilot (who was also a mechanic) and another mechanic adjusted the main rotor dampers to address the issue. Following this adjustment, a 10-minute ground run was performed without any observed problems. The pilot then conducted a test flight during, which no issues were detected. Upon landing and while reducing the rotor rpm, the helicopter began to shake violently. The pilot attempted to perform the ground resonance recovery procedure and climbed the helicopter, but the vibration worsened, and he subsequently landed. After contacting the ground, the helicopter shook and spun uncontrollably before coming to a stop. The airframe and main rotor were substantially damaged during the accident sequence. Federal Aviation Administration inspectors examined the helicopter after the accident and found that the yellow main rotor blade’s damper had significantly higher torque than the red and blue blades, and that none of the dampers were torqued to the specification in the helicopter’s maintenance manual. The manual also described that incorrect torque adjustments of the dampers could result in “…conditions that may result in ground resonance and destruction of the helicopter. During a subsequent discussion with the assisting mechanic, he stated that he, “may have unintentionally over-torqued the blade [damper].” Based on this information, it is likely that the mechanics’ improper maintenance of the helicopter’s main rotor dampers resulted in the ground resonance event experienced at the conclusion of the post maintenance test flight test flight. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • Personnel issues-Task performance-Maintenance-(general)-Maintenance personnel
  • Aircraft-Aircraft propeller/rotor-Main rotor system-Main rotor blade system-Incorrect service/maintenance

Verbatim from NTSB's published report. Source file NTSB_2023_ERA23LA289.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗