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Atlas / NTSB / WPR12CA307

NTSB CAROL · Event

Event WPR12CA307

2012-07-16 Bountiful, Utah, United States Airport · BTF None 1 aircraft Status: Completed

Registry · N47WH

FAA Aircraft Registry record.

Make / Model

EUROCOPTER AS 350 B3

Year of manufacture

2003 · 9 years old at event

TCDS

H9EU · AIRBUS HELICOPTERS

Engine

TURBOMECA ARRIEL 2B (747 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

20250508

ADS-B equipped

Yes — Mode-S A5C0BD

Registrant of record

INTERNATIONAL AIR SERVICES INC TRUSTEE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The student’s failure to maintain adequate rotor rpm and the flight instructor’s delayed remedial action, which resulted in a hard landing.

Factual narrative

While performing simulated power-off autorotations with a power recovery, the certified flight instructor (CFI) and student noted that the main rotor rpm was decaying. About 150 to 200 feet above ground level (agl), the CFI took the flight controls and executed a flare about 50 feet agl, and realized the helicopter was going to settle. The CFI then attempted a run on landing, but the helicopter landed hard, spreading the skid landing gear. The helicopter then slid about 75 feet down the runway, departed the runway surface, and rolled four times before coming to rest on its left side. The CFI stated that there were no mechanical problems with the helicopter. While performing a simulated power-off autorotation with a power recovery, the certified flight instructor (CFI) and student noted that the main rotor rpm was decaying. About 150 to 200 feet above ground level (agl), the instructor took the flight controls, executed a flare about 50 feet agl, and realized that the helicopter was going to settle. The instructor then attempted a run-on landing, but the helicopter landed hard, spreading the skid landing gear and damaging the rotors, frame, engine and transmission. The helicopter then slid about 75 feet down the runway, departed the runway surface, and rolled four times before coming to rest on its left side. The CFI stated that there were no mechanical problems with the helicopter prior to the accident. 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Not attained/maintained - C
  • C Personnel issues-Action/decision-Action-(general)-Pilot - C
  • C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Prop/rotor parameters-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2012_WPR12CA307.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. 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 ↗