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WPR13CA027

2012-10-28 · Hanapepe, Hawaii, United States · None · 1 aircraft · Status: Completed

Airport PAK

Current FAA registration · N216AB

Make / Model
ROBINSON HELICOPTER R22 BETA
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19870609
ADS-B equipped
Yes — Mode-S A1CFCE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's selection of an unsuitable landing area. Contributing to the pilot’s decision to land in an unsuitable landing area was his lack of helicopter experience, which led him to misidentify the precursor event.

Factual narrative

The pilot, who was in training to add a helicopter rating to his pilot certificate, said he had just departed for a solo flight. He accelerated the helicopter to cruise flight and noticed an “unusual vibration.” He performed an immediate precautionary landing straight ahead. During the touchdown sequence, one of the helicopter’s landing skids hit a tree branch, and the helicopter rolled onto its side. The helicopter’s main rotor impacted the tail boom, which separated from the fuselage. Several days after the accident, the pilot flew with his flight instructor in a different helicopter and attempted to replicate the vibration. As a result of this flight, the pilot believes that, during the accident flight, he encountered a tailwind and that there was nothing wrong with the helicopter. The pilot reported that he had departed for a solo training flight to add a helicopter rating to his pilot certificate. He accelerated the helicopter to cruise flight and noticed an “unusual vibration.” He performed an immediate precautionary landing. During the touchdown sequence, one of the helicopter’s landing skids hit a tree branch, and the helicopter rolled onto its side. The helicopter’s main rotor impacted the tailboom, which separated from the fuselage. Several days after the accident, the pilot flew with his flight instructor in a different helicopter and attempted to replicate the vibration. As a result of this flight, the pilot believes that he encountered a tailwind during the accident flight that caused him to feel a vibration. Subsequently, the pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • — Environmental issues-Physical environment-Object/animal/substance-Tree(s)-Effect on operation
  • C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
  • C Environmental issues-Physical environment-Runway/land/takeoff/taxi surfa-(general)-Decision related to condition - C
  • F Personnel issues-Experience/knowledge-Experience/qualifications-Total experience w/ equipment-Pilot - F

Verbatim from NTSB's published report. Source file NTSB_2012_WPR13CA027.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.