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ANC14CA060

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

Current FAA registration · N3502W

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

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

FAA avdata. C = Cause, 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 ↗.