LAX98LA301
1998-09-20 · LONG BEACH, California, United States · None · 1 aircraft · Status: Completed
Airport LGB
Current FAA registration · N8761U
- 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
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 ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
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- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
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- 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…