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Atlas / NTSB / ANC14CA060

NTSB CAROL · Event

Event ANC14CA060

2014-08-06 Anderson, Alaska, United States None 1 aircraft Status: Completed

Registry · N3502W

FAA Aircraft Registry record.

Make / Model

PIPER PA-32-260

Year of manufacture

1966 · 48 years old at event

Engine

LYCOMING 0-540 SERIES (250 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

19660222

ADS-B equipped

Yes — Mode-S A3E780

Registrant of record

N3502W LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's inadequate compensation for wind conditions, which resulted in a hard landing.

Factual narrative

The pilot was landing the tricycle gear equipped airplane at a remote, unimproved airport, which was surrounded by mountainous terrain. Before beginning his approach, the pilot assessed the wind conditions, and then planned an approach into a 25 to 35 knot quartering headwind. On short final, approximately 20 feet above ground level, a sudden wind shift caused the airplane to descend faster than anticipated. He attempted to arrest the descent by adding engine power, but the airplane landed hard and the right main wheel axle separated from the airplane. The airplane sustained substantial damage to the right wing, aileron and stabilator. The pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation. In the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been avoided if a windsock had been present at the airport; he also stated that notes in the Alaska Supplement warning operators of wind shear hazards associated with the terrain surrounding the airport would enhance safety. The pilot was landing the tricycle gear equipped airplane at a remote, unimproved airport, which was surrounded by mountainous terrain. Before beginning his approach, the pilot assessed the wind conditions, and then planned an approach into a 25 to 35 knot quartering headwind. On short final, approximately 20 feet above ground level, a sudden wind shift caused the airplane to descend faster than anticipated. He attempted to arrest the descent by adding engine power, but the airplane landed hard and the right main wheel axle separated from the airplane. The airplane sustained substantial damage to the right wing, aileron and stabilator. The pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation. In the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been avoided if a windsock had been present at the airport; he also stated that notes in the Alaska Supplement warning operators of wind shear hazards associated with the terrain surrounding the airport would enhance safety. 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-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Environmental issues-Conditions/weather/phenomena-Wind-Windshear-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2014_ANC14CA060.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 or causal vocabulary (wind shear). 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 ↗