NTSB CAROL · Event
Event LAX98LA314
Registry · N9438V
FAA Aircraft Registry record.
Make / Model
MOONEY M20C
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19700528
ADS-B equipped
Yes — Mode-S AD1BD1
Registrant of record
PRESTRIDGE JACOB
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for the existing crosswind condition, which resulted in a hard landing.
Factual narrative
On September 17, 1998, about 1400 hours Pacific daylight time, a Mooney M20C, N9438V, sustained substantial wing and fuselage damage while landing in crosswind conditions at the Reno-Taho International Airport, Reno, Nevada. The aircraft was owned and operated by the pilot under the provisions of 14 CFR Part 91, and was on a cross-country personal flight. Visual meteorological conditions prevailed and included winds at 18 knots with gusts to 26 knots. The pilot and two passengers were not injured. The flight originated at the Fullerton, California, airport about 1200 on the day of the accident with an intended destination of Reno. The pilot did not report the accident to either the Safety Board or the Federal Aviation Administration (FAA). An FBO on the Reno airport reported to the Reno Flight Standards District Office that the aircraft had sustained significant damage in the accident and had been flown to Fullerton for repair. The damaged airplane was examined by FAA inspectors from the Long Beach, California, Flight Standards District Office at a repair facility on the Fullerton airport. The damage consisted of a deformed and bent left wing, with spar wrinkles and tears, and, damage to the empennage near the bottom of the rudder. FAA inspectors interviewed the pilot-rated passenger who occupied the right front seat. He said that the pilot experienced difficulty controlling the airplane on short final approach in the prevailing crosswind condition. The pilot reportedly asked the passenger for help and by the time he was able to get on the controls, the left wing had contacted the ground. The passenger further reported to FAA inspectors that following the accident, a loaner propeller was obtained and some sheet metal straps were installed on the damaged wing. The passenger and a mechanic from Fullerton then flew the aircraft back to Fullerton. A ferry permit was not obtained. The pilot and pilot-rated passenger who occupied the right front seat said that the pilot experienced difficulty controlling the airplane on short final approach in the prevailing crosswind condition. The pilot reportedly asked the passenger for help and by the time he was able to get on the controls, the left wing had contacted the ground. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_LAX98LA314.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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