NTSB CAROL · Event
Event LAX99LA055
Aircraft involved
Probable cause & findings
The pilot's misjudged landing flare, which lead to an inadvertent stall/mush 10 feet above the ground.
Factual narrative
On December 18, 1998, at 1545 hours Pacific standard time, a Piper PA-28-180, N5413S, landed hard on runway 26 at the Big Bear, California, airport. The aircraft, owned and operated by Aero Haven, Inc., under 14 CFR Part 91, sustained substantial damage. The private pilot and one passenger were not injured. Visual meteorological conditions existed for the personal flight that had departed from Lake Havasu, Arizona, on the day of the accident. The flight was scheduled to terminate at Big Bear and no flight plan was filed. The pilot reported that the aircraft's approach speed was 85 miles per hour when the aircraft contacted the surface. He stated that the aircraft porpoised down the runway, and on the second contact with the surface the propeller struck the runway. The pilot stated that there was a loss of directional control after he lost use of the rudder. The aircraft veered to the right and departed the runway striking a landing light. A Federal Aviation Administration inspector from the Riverside, California, Flight Standards District Office responded to the accident site. The inspector interviewed a witness and inspected the aircraft. The witness stated that the aircraft came into land and flared approximately 10 feet above the runway and stalled. The inspector noted that the main landing gear was intact, but the structural mounting bolts in the wing were elongated. He further noted that the engine mounts were bent and the main spars had been compromised. The inspector observed an unattached rudder bellcrank. A witness at the airport reported that the aircraft flared approximately 10 feet above the runway, stalled, and hit the runway hard. Examination of the airplane revealed that the landing gear structural mounting bolts were elongated, the engine mounts and both main spars were bent. The pilot reported that there were no preimpact mechanical malfunctions. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_LAX99LA055.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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