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 ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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