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GAA15CA004

2015-03-09 · Hurricane, Utah, United States · None · 1 aircraft · Status: Completed

Airport 1L8

Current FAA registration · N949WB

Make / Model
CIRRUS DESIGN SR22
Year of manufacture
2003 · 12 years old at event
Engine
CONT MOTOR IO-550 SERIES (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20030109
ADS-B equipped
Yes — Mode-S AD308D

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's failure to maintain directional control during the landing roll.

Factual narrative

The pilot reported that he entered a right traffic pattern for runway 19; on his first approach he noted that he was going to overshoot the runway and executed a go-around procedure. On his second attempt after he touched down on the runway, he reported a "radical" right quartering tail wind that pushed the airplane to the left of the runway. The airplane's left main tire departed the asphalt surface, the pilot then attempted a go-around by advancing the throttle to full and decreasing the flaps to 50 percent. The pilot stated that he was not gaining lift and the stall warning horn was audible. Subsequently the airplane impacted a ditch and bounced about 10 feet which resulted in substantial damage to the spar carry-through on the bottom of the fuselage. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot reported that he entered a right traffic pattern for runway 19; on his first approach he noted that he was going to overshoot the runway and executed a go-around procedure. On his second attempt after he touched down on the runway, he reported a "radical" right quartering tail wind that pushed the airplane to the left of the runway. The airplane's left main tire departed the asphalt surface, the pilot then attempted a go-around by advancing the throttle to full and decreasing the flaps to 50 percent. The pilot stated that he was not gaining lift and the stall warning horn was audible. Subsequently the airplane impacted a ditch and bounced about 10 feet which resulted in substantial damage to the spar carry-through on the bottom of the fuselage. The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. 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
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
  • — Environmental issues-Conditions/weather/phenomena-Wind-Tailwind-Effect on operation

Verbatim from NTSB's published report. Source file NTSB_2015_GAA15CA004.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 (stall, go-around). All research papers