NTSB CAROL · Event
Event LAX03LA186
Registry · N519ER
FAA Aircraft Registry record.
Make / Model
CESSNA 172S
Year of manufacture
2002 · 1 years old at event
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20020813
ADS-B equipped
Yes — Mode-S A68352
Registrant of record
STICK & RUDDER CLUB INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's inadequate compensation for the wind conditions and failure to maintain directional control. Also causal was the flight instructor's inadequate supervision of the flight in allowing the student to perform a solo flight with a strong, gusting crosswind near the factory demonstrated crosswind component limit. Factors to the accident were the gusty crosswind conditions, and a lack of flight school standards pertaining to student pilot supervised solo flights in challenging weather conditions.
Factual narrative
On June 8, 2003, at 1442 mountain standard time, a Cessna 172S, N519ER, veered off the runway, collapsing the right main and nose landing gear at Ernest A. Love Field (PRC), Prescott, Arizona. Embry-Riddle Aeronautical University (ERAU) was operating the airplane under the provisions of 14 CFR Part 91. The student pilot, the sole occupant, was not injured; the airplane sustained substantial damage. The local solo instructional flight departed Prescott about 1410. Day visual meteorological conditions prevailed, and no flight plan had been filed. The student had logged about 36 hours and was on his second supervised solo, practicing touch-and-go landings on runway 21R. Immediately prior to the accident, a dual flight with his instructor went uneventfully. The winds were from 250 degrees at 13 knots, gusting to 18 knots. On the solo flight that followed, three successful takeoffs and landings were accomplished. Like the landings before it, the fourth was performed using a forward slip to compensate for the crosswind condition. Believing that the wind was coming from the left side of the runway, the student lowered the left wing into the wind and applied right ruder. Ground contact was first made with the left main landing gear followed by the right main, and nose gear. Upon adding power to takeoff again, the left wing lifted and the aircraft pivoted around the right main gear. The aircraft then veered off the left side of the runway before the student was able to regain control. The left main gear and nose gear collapsed as a result, and damage was sustained to the left wing tip, aileron, and horizontal stabilizer. The student stated that he believed he departed the runway because he did not compensate for the crosswind with enough right rudder. The student's instructor was standing near the end of runway 21L. He had a handheld transceiver and was monitoring the student's progress throughout the flight. Having just flown with the student prior to the solo, the instructor was satisfied with the student's performance under the conditions present. As he recalled, there was a left quartering head wind of approximately 6 to 10 knots with no gusts at the approach end of the runway. However, at the departure end the winds suddenly shifted and were from the right side. In the instructor's opinion, the student simply "went back to his old habit of not maintaining a crosswind correction after touching down" and thus lost control of the airplane. The student's flight training records and ERAU's curriculum were reviewed. Throughout his training and leading up to his first solo flight 1 day prior to the accident, his instructor had noted that the student was having trouble with certain flight maneuvers, including forward slips. The ERAU curriculum sets no crosswind limits for students on their initial supervised solo flights. In a METAR weather report generated by an ASOS about 10 minutes after the accident, winds were reported to be out of 250 degrees magnetic heading at 13, gusting to 18 knots. Measurements from the hours preceding the accident and hours after the accident show differing angles of crosswind direction but similar speeds and gusts. As reported by an airport operations supervisor, the equipment that measures this data is found on the south side of the airport, about 100 yards southeast of the runway 12-30 and 21L-3R intersection. According to a Cessna 172S Skyhawk Information Manual, the maximum demonstrated crosswind is 15 knots. Using the reported METAR winds immediately after the accident, the crosswind experienced would be approximately 13 knots. In an unofficial weather report conducted by ERAU, it is stated that "employees of Embry-Riddle Aeronautical University reported very strong wind gusts in the Prescott Valley area earlier that afternoon in association with shower and microburst activity." When asked what he believed to be an appropriate crosswind for a student pilot to safely solo in, the Chief Flight Instructor stated that he would solo a student in a maximum of "7 to 10 knots of crosswind or 10 to 15 knots of head wind" depending on the student's skill level. However, it would be unusual to allow a student on their initial solo flights to fly under such conditions unless the student has been performing "exceptionally well." In his belief, 30 percent of the time students might find themselves having to fly in the less than favorable conditions of the afternoon due to schedule conflicts and availability of aircraft. Having flown earlier on the day of the accident, the Chief Instructor had noticed virga, but did not experience any microbursts. While practicing touch-and-go landings on his second supervised solo, the student pilot lost control of the airplane and veered off the left side of the runway. He had been compensating for a crosswind estimated by himself and his instructor to be around 10 knots, and from the left side of the runway, 21R. This compensation was accomplished using a forward slip, with the left wing down into the wind and right rudder. In the past his instructor had noted problems with the student's execution of forward slips, and attributes the accident to the student not maintaining adequate wind correction. At the time of the accident, winds at the airport were from 250 degrees at 13, gusting to 18 knots. Measurements from in the hours preceding the accident and hours after the accident show differing angles of crosswind direction but similar speeds and gusts. The airplane's performance charts indicate that a 13-knot crosswind would have been experienced under such conditions, and states that maximum demonstrated crosswind to be 15 knots. The Chief Flight Instructor stated that he would solo a student in a maximum of "7 to 10 knots of crosswind," but only if the student had been performing exceptionally well. The school's curriculum sets no crosswind limits for students on their initial supervised solo flights. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_LAX03LA186.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, microburst). 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 ↗