NTSB CAROL · Event
Event LAX98LA301
Registry · N8761U
FAA Aircraft Registry record.
Make / Model
CESSNA 172F
Year of manufacture
1965 · 33 years old at event
Engine
CONT MOTOR 0-300 SER (145 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19650225
ADS-B equipped
Yes — Mode-S AC0F2E
Registrant of record
SMITH DUSTIN T
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's misjudging the flare point and failure to maintain an adequate airspeed margin, which resulted in a stall/mush and hard landing. A contributing factor was the dark night conditions.
Factual narrative
On September 20, 1998, at 2130 hours Pacific daylight time, a Cessna 172F, N8761U, sustained substantial damage during a hard landing at Long Beach, California. The commercial pilot and his two passengers were not injured. The local flight was operated by the pilot under 14 CFR Part 91, and visual meteorological conditions prevailed. The pilot and his wife departed Fullerton, California, and stopped in Torrance, California, to pickup a passenger. No flight plan was filed. After departing Torrance and flying over the Long Beach harbor area, the pilot decided to land at Long Beach airport. The pilot stated he flared high; the airplane slowed so he added power to help control his descent. He then reduced power and the nose dropped. The propeller, nose wheel, left main landing gear, and left wing tip struck the ground simultaneously. The airplane bounced and the right wing struck the ground. Both propeller blades were bent, the firewall was buckled, the nose and left wheel pants were damaged, and the fuselage was buckled aft of the cowling. Both wing tips were scraped and skin panels on both wings were wrinkled. The right aileron and left horizontal stabilizer were also damaged. The pilot entered the landing pattern under night conditions and everything was normal until he flared for touchdown. He believed he had flared high and added power to help control the descent rate. He then reduced power. The nose dropped and the propeller, nose gear, left main landing gear, and left wing tip struck the pavement almost simultaneously. The aircraft bounced and struck the ground with the right wing tip before coming to rest on the runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_LAX98LA301.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 (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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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