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SEA02LA094

2002-06-02 · Payette, Idaho, United States · None · 1 aircraft · Status: Completed

Airport S75

Current FAA registration · N9967Q

Make / Model
PIPER PA-18-135
Year of manufacture
1954 · 48 years old at event
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19850808
ADS-B equipped
Yes — Mode-S ADEC49

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to adequately compensate for the wind conditions during landing resulting in a ground loop/swerve. Wind gusts were a contributing factor.

Factual narrative

On June 2, 2002, approximately 0950 mountain daylight time, a Piper PA-18-135 airplane, N9967Q, registered to Taildragon LLC of Eagle, Idaho, and being flown by a private pilot, was substantially damaged when it ground looped during landing at Payette Municipal Airport, Payette, Idaho. The pilot and one passenger were not injured in the accident. Visual meteorological conditions prevailed and the flight was on a round-robin visual flight rules (VFR) flight plan from Boise, Idaho, to Weiser, Idaho, to Payette, to Boise at the time of the accident. The flight was conducted under the provisions of 14 CFR 91. In a written statement, the pilot reported that on downwind for landing on runway 31, he noted that the wind sock was hanging limp. Turbulence was noted on the approach and a crosswind correction was applied to maintain runway centerline. The pilot reported that during the flare for a three point landing, he noted an increased descent rate beginning about six feet above ground level. The pilot applied power to arrest the descent rate, however, when the aircraft touched down it bounced. When the aircraft settled to the surface again, the right wing was lifted by a sudden gust of wind. The aircraft weathervaned to the right and the pilot added power in an attempt to regain rudder authority. The pilot was unable to maintain directional control and the aircraft ground looped. The right wing contacted the surface, substantially damaging the wing spar and several ribs. The pilot reported no mechanical failures or malfunctions with the aircraft at the time. After the accident, the pilot noted that the wind was blowing from about 330 degrees at three to five knots, with intermittent gusts from 10 to 12 knots. The pilot reported that while on final approach for landing, he encountered turbulence and a crosswind correction was applied to maintain runway centerline. The pilot stated that during the flare for a three point landing, he noted an increased descent rate beginning about six feet above ground level. The pilot applied power to arrest the descent rate, however, when the aircraft touched down it bounced. When the aircraft settled to the surface again, the right wing was lifted by a sudden gust of wind. The aircraft weathervaned to the right and the pilot added power in an attempt to regain rudder authority. The pilot was unable to maintain directional control and the aircraft ground looped. The right wing contacted the surface, substantially damaging the wing spar and several ribs. The pilot reported no mechanical failures or malfunctions with the aircraft at the time. After the accident, the pilot noted intermittent gusts of wind from 10 to 12 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2002_SEA02LA094.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (turbulence). All research papers