NTSB CAROL · Event
Event ERA15CA081
Registry · N430WH
FAA Aircraft Registry record.
Make / Model
BELL 430
Year of manufacture
2006 · 8 years old at event
TCDS
H9SW · BELL HELICOPTER TEXTRON
Engine
ROLLS-ROYC 250-C40B (715 hp)
Seats / Engines
10 seats · 2 engines
Last airworthiness date
20060317
ADS-B equipped
Yes — Mode-S A5251A
Registrant of record
AVIATION TRUST COMPANY LLC TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's misjudgment of his helicopter's position relative to a parked helicopter during a pedal turn.
Factual narrative
According to the pilot, he flew a "normal" approach to the helicopter pad, then hover-taxied to the parking area. Two other helicopters were parked at the far edges on opposite sides of the parking area. Following a procedure that had been developed over the previous 10 years and executed over 20 times without incident, the pilot hover-taxied into the center position and began a pedal turn to align the helicopter with the others. About 90 degrees through the pedal turn, the tail rotor of the pilot's helicopter contacted a main rotor blade tip of one of the parked helicopters, resulting in substantial damage to a tail rotor blade. The pilot completed the pedal turn and landed uneventfully. The pilot did not report any preexisting mechanical anomalies that would have precluded normal operation. According to the pilot, he made a "normal" approach to a helipad and subsequently hover-taxied to the parking area. Two other helicopters were parked on opposite sides of the parking area, and per existing procedures, the pilot hover-taxied his helicopter to the center of the parking area and commenced a pedal turn to align it with the others. About 90 degrees through the turn, a tail rotor blade from the pilot's helicopter impacted a main rotor blade tip on one of the parked helicopters, resulting in substantial damage to the tail rotor blade. The pilot subsequently completed the turn and landed without further incident. The pilot did not report any preexisting mechanical anomalies that would have precluded normal operation. 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).
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2014_ERA15CA081.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2019 · Presentation
Failure Analysis of T-38 Aircraft Burst Hydraulic Aileron Return Line
During maintenance troubleshooting for fluctuating hydraulic pressures, a technician found that a right hand aileron return line, on the flight hydraulic side, was ruptured (Fig. 1, 2).
- NASA NTRS 2019 · Contractor Report (CR)
Independent Orbiter Assessment (IOA): Analysis of the hydraulics/water spray boiler subsystem
The results of the Independent Orbiter Assessment (IOA) of the Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL) are presented.
- NASA NTRS 2019 · Contractor Report (CR)
Implications of equipping a DC-8-61 fleet with RNAV/two-segment approach avionics
Due to the costs of implementing two-segment approaches with special purpose computers, and the fact that such systems rely on special ground equipment not generally in use today, it is useful to cons…
- NASA NTRS 2018 · Other
Scale Model Icing Research Tunnel
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