NTSB CAROL · Event
Event LAX07LA175
Aircraft involved
Probable cause & findings
The pilot's failure to maintain an adequate airspeed that resulted in an inadvertent stall.
Factual narrative
HISTORY OF FLIGHT
On May 25, 2007, about 1325 Pacific daylight time, an experimental Light Sport Airplane (E-LSA) Skygear, N51291, experienced a loss of control and impacted terrain at Chino Airport, Chino, California. The owner/pilot was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The private pilot, the sole occupant was killed. The airplane sustained substantial damage. The local personal flight departed Chino about 1320. Visual meteorological conditions prevailed, and no flight plan had been filed. Examination of the airplane records revealed that the airplane had been issued a special airworthiness certificate on May 22, 2007. The pilot was reported to be conducting a test flight for further certification.
PERSONNEL INFORMATION
A review of Federal Aviation Administration (FAA) airman records revealed that the 57-year-old pilot held a private pilot certificate with ratings for airplane single and multiengine land. The pilot held a third-class medical certificate issued on April 24, 2007. It had no limitations or waivers. No personal flight records were located for the pilot. The National Transportation Safety Board investigator-in-charge (IIC) obtained the aeronautical experience listed in this report from a review of the FAA airmen medical records on file in the Airman and Medical Records Center located in Oklahoma City, Oklahoma. The pilot reported on his medical application that he had a total flight time of 12,000 hours, with 30 hours logged in the last 6 months.
AIRCRAFT INFORMATION
The airplane was an experimental Light Sport Airplane (E-LSA) Skygear, N51291, serial number SKG-9003010606. A review of the airplane's logbooks revealed that the airplane had a total airframe time of 8 hours at the last inspection. The logbooks contained an entry for the inspection dated May 22, 2007. The engine was a Rotax model 912. Total time since new recorded on the engine at the last inspection was 8 hours. Examination of the maintenance and flight records revealed no unresolved maintenance discrepancies against the airplane prior to departure.
METEOROLOGICAL INFORMATION
The closest official weather observation station was Chino Airport (CNO), which was .5 nautical miles (nm) south of the accident site. The elevation of the weather observation station was 650 feet mean sea level (msl). An aviation routine weather report (METAR) for CNO was issued at 1353 PDT. It stated: winds from 250 degrees at 13 knots gusting to 18 knots; visibility 5 miles; skies clear; temperature 28 degrees Celsius; dew point 11 degrees Celsius; altimeter 29.90 inches of mercury.
COMMUNICATIONS
The airplane was in contact with Chino airport traffic control tower (ATCT) on frequency 118.5. The pilot had requested to takeoff using runway 26R and advised he intended on remaining in the pattern for touch-and-go practice. The local controller cleared the pilot for right closed traffic, which the pilot then acknowledged. No further communications were received from the pilot.
WRECKAGE AND IMPACT INFORMATION
The airplane impacted the ground in a steep nose down attitude in the front yard of the airport manager's residence, which is located on the north side of the airport. During the on-site inspection of the airplane, investigators discovered numerous items that appeared to be used as ballast. The items were a large cardboard box of construction staples, a red metal toolbox, and a cardboard box with a metal workbench vise.
MEDICAL AND PATHOLOGICAL INFORMATION
The San Bernardino County Coroner completed an autopsy on May 29, 2007. The coroner listed the cause of death as "Multiple blunt force trauma, instant." The FAA Civil Aerospace Medical Institute (CAMI), Oklahoma City, performed toxicological testing of specimens of the pilot. Analysis of the specimens contained no findings for carbon monoxide, cyanide, volatiles, and tested drugs.
TESTS AND RESEARCH
Investigators examined the wreckage at Aircraft Recovery Service, Littlerock, California, on September 17, 2009. The airframe and engine were examined with no mechanical anomalies identified. The IIC interviewed an individual who was assisting the pilot with certification of the airplane. He stated that the accident airplane was about 100 pounds too heavy and most of the weight was located in the tail section. He stated that they were trying to move the center of gravity (CG) as far forward as possible. This is why the pilot may have been using so much ballast weight in the front seat area of the airplane. He stated that the original concept airframe was built in Korea and consisted of a metal frame covered with cloth. The pilot had the accident airplane built in China and the construction was the same metal frame, but was covered in hand laid fiberglass.
ADDITIONAL INFORMATION
According to FAA Advisory Circular AC 20-27F, Certification and Operation of Amateur-Built Aircraft, "Amateur builders are free to develop their own designs or build from existing designs. We do not approve these designs and it would be impractical to develop design standards for the wide variety of design configurations, created by designers, kit manufacturers, and amateur builders." The recently constructed amateur-built experimental airplane was in its initial flight test phase and was in the traffic pattern at the airport. Witnesses said it stalled and collided with terrain in a nose down attitude. The airplane had accumulated approximately 8 hours total flight time. An individual who was assisting the pilot with the certification of the airplane reported that it was about 100 pounds heavier than the original design specified due to intentional modifications that were made during construction. Most of the additional weight was located in the tail section. On the day of the accident, the pilot had loaded into the front seat numerous heavy items in an attempt to move the CG forward. The items included a metal workbench vise, a metal toolbox, and a large box of construction staples. Examination of the airplane and engine revealed no abnormalities, which would have precluded normal operation. The person assisting with certification stated that the original concept airframe was built in Korea and consisted of a metal frame covered with cloth. The pilot had the accident airplane built in China but with the metal frame covered in hand laid fiberglass. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_LAX07LA175.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, loss of control, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
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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 …
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