NTSB CAROL · Event
Event LAX94LA103
Registry · N6375D
FAA Aircraft Registry record.
Make / Model
CESSNA 172N
Year of manufacture
1979 · 15 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19790522
ADS-B equipped
Yes — Mode-S A85AC8
Registrant of record
XIN HAN AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE STUDENT PILOT'S FAILURE TO MAINTAIN DIRECTIONAL AND HIS IMPROPER USE OF THE RUDDER. THE STUDENT PILOT'S FAILURE TO RAISE THE FLAPS, THE PREVAILING 90-DEGREE CROSSWIND, AND HIS LACK OF TOTAL EXPERIENCE ARE FACTORS IN THIS ACCIDENT.
Factual narrative
On January 24, 1994, at 1635 hours Pacific standard time, a Cessna 172N, N6375D, lost control and veered off runway 25R at the Livermore Municipal Airport, Livermore, California. The noncertificated student pilot was conducting a local visual flight rules solo instructional flight and was not injured. The airplane, operated by Sierra Academy of Aeronautics (herein referred to as Sierra Academy), Livermore, sustained substantial damage. Visual meteorological conditions prevailed. The flight originated at Livermore Municipal Airport at 1540 hours. Mr. James Deeton, Director of Flight Operations, Sierra Academy, submitted the Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1/2. He said that the student was dispatched at 1540 hours and departed to the practice area. The student returned to the airport at 1610 hours and was doing touch-and-go takeoffs and landings. On the last takeoff, the student attempted to take off with the flaps fully extended (30 degrees). The student failed to maintain directional control and departed the left side of the runway and entered the soft, recently plowed terrain. When the airplane's nose wheel encountered the mud, the airplane nosed over onto its back. Mr. Deeton also indicated on the accident report that the airplane did not experience any malfunctions or failures. According to the Federal Aviation Administration, the winds were reported to be from 150 degrees at 5 knots at the time of the accident. The operator reported the winds were from 160 degrees at 6 knots. THE STUDENT WAS PRACTICING TOUCH-AND GO-TAKEOFFS AND LANDINGS. ON THE LAST TAKEOFF, THE STUDENT PILOT ATTEMPTED TO TAKE OFF WITH THE FLAPS FULLY EXTENDED. HE THEN FAILED TO MAINTAIN DIRECTIONAL CONTROL BY IMPROPERLY USING THE RUDDER. THE AIRPLANE EXITED THE LEFT SIDE OF THE RUNWAY AND NOSED OVER ONTO ITS BACK. THERE WERE NO REPORTED AIRPLANE/ENGINE MALFUNCTIONS OR FAILURES. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_LAX94LA103.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 (icing). 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 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗