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Atlas / NTSB / ERA16CA294

NTSB CAROL · Event

Event ERA16CA294

2016-08-17 Newnan, Georgia, United States Airport · CCO None 1 aircraft Status: Completed

Aircraft involved

Probable cause & findings

The student pilot's improper decision to land long and maintain excessive speed during the landing roll. Contributing to the accident was the student pilot's decision to maintain full flaps and aft yoke inputs at a higher speed, reducing his ability to stop the airplane on the runway.

Factual narrative

The solo student pilot reported that he was on final approach for a full stop landing when he observed another airplane waiting for the active runway. He intentionally landed long to accommodate the traffic and then "made [the] decision to keep up speed" in order to exit the runway quickly. He misjudged his speed and the airplane departed the right side of the runway, continued across a taxiway, and then down an embankment before nosing over. He later reported that the wheel brakes were less effective because he had full flaps selected. Also, he had applied aft yoke inputs, which minimized the effectiveness of the nose wheel steering system.A Federal Aviation Administration inspector examined the wreckage and reported that the airplane sustained substantial damage to the fuselage, empennage, and both wings. The pilot reported there were no preimpact mechanical malfunctions or anomalies that would have precluded normal operation of the airplane. The solo student pilot reported that he was on final approach for a full stop landing when he observed another airplane waiting for the active runway. He intentionally landed long to accommodate the traffic and then "made [the] decision to keep up speed" in order to exit the runway quickly. He misjudged his speed and the airplane departed the right side of the runway, continued across a taxiway, and then down an embankment before nosing over. He later reported that the wheel brakes were less effective because he had full flaps selected. Also, he had applied aft yoke inputs, which minimized the effectiveness of the nose wheel steering system. A Federal Aviation Administration inspector examined the wreckage and reported that the airplane sustained substantial damage to the fuselage, empennage, and both wings. The pilot reported there were no preimpact mechanical malfunctions or anomalies that would have precluded normal operation of the airplane. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Not attained/maintained - C
  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Surface speed/braking-Incorrect use/operation - C
  • C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Student/instructed pilot - C
  • F Personnel issues-Task performance-Use of equip/info-Use of equip/system-Student/instructed pilot - F
  • Environmental issues-Physical environment-Terrain-(general)-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2016_ERA16CA294.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.