NTSB CAROL · Event
Event LAX93LA265
Registry · N29396
FAA Aircraft Registry record.
Make / Model
CULVER LCA
Year of manufacture
1940 · 53 years old at event
Engine
CONT MOTOR IO-200 (115 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19890301
ADS-B equipped
Yes — Mode-S A30451
Registrant of record
JILEK DOMINIC A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO MAINTAIN CONTROL OF THE AIRCRAFT DURING TAKEOFF. A FACTOR IN THE ACCIDENT WAS THE PILOT'S LACK OF RECENT FLIGHT EXPERIENCE IN TAIL WHEEL AIRCRAFT.
Factual narrative
On June 21, 1993, at 1522 hours Pacfic daylight time, a Culver LCA, N29396, collided with the ground following a loss of control just after lift off from runway 29 at the San Luis Obispo, California, airport. Visual meteorological conditions prevailed at the time and no flight plan was filed for the operation. The aircraft incurred substantial damage. The certificated airline transport pilot, the sole occupant, was not injured. The flight was originating as a local traffic pattern practice flight at the time of the mishap. The pilot was interviewed by an inspector from the San Jose, California, Flight Standards District Office. In both his verbal and written statements, the pilot said he was picking up the aircraft which his father-in-law had just purchased, and was going to fly it to Washington state. The pilot noted that he intended to stay in the traffic pattern to do several takeoffs and landings prior to proceeding on the delivery flight. The responding FAA inspector reported that the pilot's last tail wheel aircraft experience was in 1985, and, at that time, his total tail wheel experience was 250 hours. Ground witnesses to the accident reported that the aircraft became airborne after a ground roll of about 600 feet and immediately yawed and rolled to the left. The aircraft collided with the ground adjacent to the runway. The pilot reported that during the takeoff ground roll on runway 29 he looked down at the airspeed indicator, and, when he looked up again, the aircraft had lifted off and was rolling to the left. The pilot stated that he could not correct the roll in time to prevent a nose down collision with the ground. The winds at the time were reported by the control tower at 300 degrees at 18 knots. The aircraft was examined by the responding FAA inspector. He reported that control system continuity was established throughout the aircraft, to include the tail wheel steering mechanism. The pilot did not claim any mechanical malfunction at the time of his interview with the FAA inspector. THE PILOT SAID HE WAS PICKING UP THE AIRCRAFT, WHICH HIS FATHER IN LAW HAD JUST PURCHASED, AND WAS GOING TO FLY IT TO WASHINGTON STATE. THE PILOT NOTED THAT HE INTENDED TO STAY IN THE TRAFFIC PATTERN TO DO SEVERAL TAKEOFFS AND LANDINGS PRIOR TO PROCEEDING ON THE DELIVERY FLIGHT. THE RESPONDING FAA INSPECTOR REPORTED THAT THE PILOT'S LAST TAIL WHEEL AIRCRAFT EXPERIENCE WAS IN 1985, AND, AT THAT TIME, HIS TOTAL TAIL WHEEL EXPERIENCE WAS 250 HOURS. GROUND WITNESSES TO THE ACCIDENT REPORTED THAT THE AIRCRAFT BECAME AIRBORNE AFTER A GROUND ROLL OF ABOUT 600 FEET AND IMMEDIATELY YAWED AND ROLLED TO THE LEFT. THE AIRCRAFT COLLIDED WITH THE GROUND ADJACENT TO THE RUNWAY. THE PILOT REPORTED THAT DURING THE TAKEOFF GROUND ROLL ON RUNWAY 29 HE LOOKED DOWN AT THE AIRSPEED INDICATOR, AND, WHEN HE LOOKED UP AGAIN, THE AIRCRAFT HAD LIFTED OFF AND WAS ROLLING TO THE LEFT. THE PILOT STATED THAT HE COULD NOT CORRECT THE ROLL IN TIME TO PREVENT A NOSE DOWN COLLISION WITH THE GROUND. THE WINDS AT THE TIME WERE REPORTED BY THE CONTROL TOWER AT 300 DEGREES AT 18 KTS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_LAX93LA265.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 (loss of control). 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 2024 · Accepted Manuscript (Version with final changes)
Inverse Modeling of the Initial Stage of the 1991 Pinatubo Volcanic Cloud Accounting for Radiative Feedback of Volcanic Ash
The way volcanic clouds evolve is very sensitive to the initial spatial 3D distributions of volcanic materials, which are often unknown. In this study, we conducted inverse modeling of the Mt.
- NASA NTRS 2023 · Accepted Manuscript (Version with final changes)
Observing Ocean Ecosystem Responses to Volcanic Ash
Volcanic eruptions can be catastrophic events, particularly when they occur in inhabited coastal environments. They also play important roles in climate and biogeochemical cycles, including through nu…
- arXiv 2021 · arXiv preprint
Flight Control System Design for Autonomous Aerial Surveys of Volcanoes
The controller for a quadrotor working in severe environment is developed in this study. Here, the severe environment indicates the temperature-varying air near the volcano.
- NASA NTRS 2019 · Conference Paper
Automatic Estimation of Volcanic Ash Plume Height using WorldView-2 Imagery
We explore the use of machine learning, computer vision, and pattern recognition techniques to automatically identify volcanic ash plumes and plume shadows, in WorldView-2 imagery.
- NASA NTRS 2019 · Presentation
The Hazard of Volcanic Ash Ingestion
A research team of U.S. Government agencies and engine manufacturers conducted an experiment to test volcanic-ash ingestion by a NASA owned engine in the same family as the PW 2000 that was donated by…
- NASA NTRS 2019 · Presentation
Multi-Partner Experiment to Test Volcanic-Ash Ingestion by a Jet Engine
A research team of U.S. Government agencies and engine manufacturers are designing an experiment to test volcanic-ash ingestion by a NASA owned F117 engine that was donated by the U.S. Air Force.
Browse the full corpus — academia portal ↗