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GAA19CA299

2019-05-31 · San Antonio, Texas, United States · Minor · 1 aircraft · Status: Completed

Airport 1T8

Current FAA registration · N902ES

Make / Model
CIRRUS DESIGN SR20
Year of manufacture
2002 · 17 years old at event
Engine
CONT MOTOR IO-360 SER (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20020923
ADS-B equipped
Yes — Mode-S AC770F

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's inadequate approach, delayed decision to abort the landing, and failure to properly configure the flap setting for the initial climb during the attempted aborted landing, which resulted in impact with trees.

Factual narrative

The pilot reported that, during the approach, the airspeed was about 80 knots, but he was slightly high. The pilot stated that the airplane floated down the runway further than normal before it touched down, and when he determined that he would not have enough runway to stop, he aborted the landing. The airplane did not climb as he expected, and subsequently impacted trees. The pilot added that he believed that the reason for the lack of climb was due to his failure to retract the flaps to 50%. A witness reported that the airplane landed further down the runway than normal, departed the runway, and began the takeoff from the grass alongside the runway. The airplane sustained substantial damage to the left wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot reported that, during the approach, the airspeed was about 80 knots, but the airplane was slightly high. The airplane floated down the runway further than normal before it touched down. When the pilot determined that he would not have enough runway to stop the airplane, he aborted the landing. The airplane did not climb as he expected, and it subsequently impacted trees. The pilot added that he believed that the reason the airplane failed to climb was due to his failure to retract the flaps to 50%. The airplane sustained substantial damage to the left wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Not attained/maintained - C
  • C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Climb rate-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot - C
  • C Environmental issues-Physical environment-Object/animal/substance-Tree(s)-Effect on operation - C

Verbatim from NTSB's published report. Source file NTSB_2019_GAA19CA299.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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