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GAA17CA123

2017-01-24 · Wichita, Kansas, United States · None · 1 aircraft · Status: Completed

Airport ICT

Current FAA registration · N4792T

Make / Model
PIPER PA-28R-200
Year of manufacture
1972 · 45 years old at event
Engine
LYCOMING I0360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19720302
ADS-B equipped
Yes — Mode-S A5E539

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain directional control while landing in gusting crosswind conditions.

Factual narrative

The pilot reported that during the landing roll in a gusting crosswind, the airplane veered off the runway to the left into the grass. During the runway excursion, the right wing impacted an airport sign, which resulted in substantial damage. After the airplane had stopped, the pilot taxied to the ramp without further incident. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. A review of recorded data from the automated weather observation station located on the airport, revealed that, about 2 minutes before the accident the wind was 310° at 22 knots, wind gusts at 27 knots. The airplane landed on runway 1R. According to the pilot operating handbook for the accident airplane, the maximum demonstrated crosswind component for the airplane is 20 miles per hour/17.3 knots. The pilot reported that, during the landing roll in gusting crosswind conditions, the airplane veered off the runway to the left into the grass. During the runway excursion, the right wing impacted an airport sign, which resulted in substantial damage. After the airplane had stopped, the pilot taxied to the ramp without further incident. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. A review of recorded data from the automated weather observation station located on the airport revealed that, about 2 minutes before the accident, the wind was from 310° at 22 knots, gusting to 27 knots. The airplane landed on runway 1R. According to the Pilot's Operating Handbook for the accident airplane, the maximum demonstrated crosswind component for the airplane is 20 miles per hour/17.3 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft oper/perf/capability-Aircraft capability-Maximum crosswind component-Capability exceeded - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • — Environmental issues-Physical environment-Object/animal/substance-Sign/marker-Effect on equipment
  • — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Ability to respond/compensate
  • — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Ability to respond/compensate

Verbatim from NTSB's published report. Source file NTSB_2017_GAA17CA123.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 (runway excursion). All research papers