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Atlas / NTSB / ERA15CA081

NTSB CAROL · Event

Event ERA15CA081

2014-12-21 Miami Gardens, Florida, United States Airport · 0FD2 None 1 aircraft Status: Completed

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 ↗.