NTSB CAROL · Event
Event FTW98LA017
Registry · N4957A
FAA Aircraft Registry record.
Make / Model
CESSNA A152
Year of manufacture
1979 · 18 years old at event
Engine
LYCOMING 0-235 SERIES (115 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19791107
ADS-B equipped
Yes — Mode-S A625F9
Registrant of record
PEA-WAYMAN FLIGHT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper recovery from a bounced landing and her failure to maintain directional control during the aborted landing. Factors were the wind gust and the turbulence.
Factual narrative
On October 2, 1997, at 1045 central daylight time, a Cessna A152 airplane, N4957A, was substantially damaged following a loss of control while landing near Rockwall, Texas. The solo student pilot was not injured. The airplane was owned and operated by a private owner under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the solo instructional flight for which a flight plan was not filed. The flight originated from the Rockwall Municipal Airport at approximately 0930. The operator reported that the 63 hour student pilot was endorsed for a solo round-robin flight (12 nautical miles each way) from the Rockwall Municipal Airport, to Mesquite, Texas, where she was cleared to practice takeoffs and landings. The student pilot completed two landings at the Mesquite Airport and departed the traffic pattern to return to Rockwall. The student pilot told the FAA inspector that during her approach to runway 16 at the Rockwall Airport, she "got too low on final as she encountered turbulence from the hangars located at the northwest corner of the airport." In her enclosed written statement, the student pilot stated that "while flaring over the numbers, the winds gusted and the airplane touched down with the right wheel to the left side of the runway and bounced." The student pilot stated that that after losing control of the airplane, she applied full power in an attempt to abort the landing. She further stated that the airplane managed to get airborne at an indicated airspeed of 40 to 50 knots; however, the main landing gear impacted the top strand of barbed wire from the airport's perimeter fence with the landing gear. The airplane nosed over after impacting the fence and the airplane came to rest in the inverted position. The operator reported that the winds at the airport at the time of the accident were from 180 degrees at 7 knots. Examination of the airplane by the FAA inspector that traveled to the accident site disclosed that the engine firewall, vertical stabilizer and the fuselage (at the right wing attaching point) sustained structural damage. The operator reported that the 63-hour student pilot was endorsed for a solo round-robin flight from the Rockwall Municipal Airport, to Mesquite, Texas, where she was cleared to practice takeoffs and landings. On her return flight to the Rockwall Airport, the student pilot lost control of the airplane during her landing roll on runway 16 after she 'got too low on final approach and she encountered turbulence from the hangars located at the northwest corner of the airport.' After losing control, the student pilot applied full power in an attempt to abort the landing. She added that the airplane managed to get airborne at 40 to 50 knots; however, the main landing gear impacted the airport's perimeter fence with the landing gear and the airplane nosed over coming to rest in the inverted position. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW98LA017.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2026 · arXiv preprint
Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
- arXiv 2025 · arXiv preprint
Explainable LiDAR 3D Point Cloud Segmentation and Clustering for Detecting Airplane-Generated Wind Turbulence
Wake vortices - strong, coherent air turbulences created by aircraft - pose a significant risk to aviation safety and therefore require accurate and reliable detection methods.
- arXiv 2024 · arXiv preprint
Does small-scale turbulence matter for ice growth in mixed-phase clouds?
Representing the glaciation of mixed-phase clouds in terms of the Wegener-Bergeron-Findeisen process is a challenge for many weather and climate models, which tend to overestimate this process because…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
Browse the full corpus — academia portal ↗