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Atlas / NTSB / GAA16CA236

NTSB CAROL · Event

Event GAA16CA236

2016-05-12 Lee's Summit, Missouri, United States Airport · LXT None 1 aircraft Status: Completed

Registry · N228NC

FAA Aircraft Registry record.

Make / Model

PIPER PA-28R-200

Year of manufacture

1969 · 47 years old at event

Engine

LYCOMING I0360 SER (180 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19691028

ADS-B equipped

Yes — Mode-S A1FFE8

Registrant of record

IAL CORP

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's improper pitch control after the landing flare, resulting in an aerodynamic stall, hard landing, and consequent substantial left wing damage.

Factual narrative

According to the pilot, during a Federal Aviation Administration commercial pilot practical examination, the pilot was asked to execute a simulated engine out emergency procedure, with a 180 degree turn. The pilot reported that when abeam the runway numbers he retarded the throttle to idle and turned to final. He reported that after the landing flare, the examiner told him to lower the nose, but the airplane stalled, and the airplane landed hard. He recalled that the left landing gear collapsed but the left wing did not impact the ground. The airplane exited the left side of the runway and came to a rest in the grass safety area. The pilot reported that he did not recall whether or not the examiner grabbed the flight controls, and he does not recall the examiner telling him to abort the landing and go around. The airplane sustained substantial damage to the left wing. According to the examiner, the pilot was asked to execute a simulated engine out emergency procedure, with a 180 degree turn, and that the pilot's approach was relatively stable. He reported that he told the pilot to keep the nose down after the flare, but the airplane stalled, and landed hard. He conveyed that the events occurred so quickly that he did not have time to grab the controls. He reported that the left main landing gear collapsed, but held enough of a load to prevent the airplane wing from striking the ground. The airplane exited the runway to the left, and came to a stop in the grass safety area without further incident. Both pilots reported that there were not any pre-accident mechanical failures or anomalies with the airplane that would have precluded normal operation prior to the accident. According to the pilot, during a Federal Aviation Administration commercial pilot practical examination, the pilot was asked to execute a simulated engine out emergency procedure, with a 180 degree turn. The pilot reported that when abeam the runway numbers he retarded the throttle to idle and turned to final. He reported that after the landing flare, the examiner told him to lower the nose, but the airplane stalled, and the airplane landed hard. He recalled that the left landing gear collapsed but the left wing did not impact the ground. The airplane exited the left side of the runway and came to a rest in the grass safety area. The pilot reported that he did not recall whether or not the examiner grabbed the flight controls, and he does not recall the examiner telling him to abort the landing and go around. The airplane sustained substantial damage to the left wing. According to the examiner, the pilot was asked to execute a simulated engine out emergency procedure, with a 180 degree turn, and that the pilot's approach was relatively stable. He reported that he told the pilot to keep the nose down after the flare, but the airplane stalled, and landed hard. He conveyed that the events occurred so quickly that he did not have time to grab the controls. He reported that the left main landing gear collapsed, but held enough of a load to prevent the airplane wing from striking the ground. The airplane exited the runway to the left, and came to a stop in the grass safety area without further incident. Both pilots reported that there were not any pre-accident mechanical failures or anomalies with the airplane that would have precluded normal operation prior to the accident. 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-Pitch control-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot

Verbatim from NTSB's published report. Source file NTSB_2016_GAA16CA236.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗