NTSB CAROL · Event
Event LAX07CA120
Registry · N320
FAA Aircraft Registry record.
Make / Model
KODIAK AIRCRAFT CO INC KODIAK 100
Year of manufacture
2023
Engine
P&W CANADA PT6A-34 (750 hp)
Seats / Engines
10 seats · 1 engine
Last airworthiness date
20230801
ADS-B equipped
Yes — Mode-S A36E4F
Registrant of record
SAVAUGE SEAPLANE II LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
contamination of the number 2 fuel injector nozzle that lead to a partial loss of engine power.
Factual narrative
On April 2, 2007, at 1729 Pacific daylight time, an experimental amateur built Carpenter Lancair 320, N320, experienced a partial loss of engine power on takeoff and made a forced landing on runway 12 at Whiteman Airport (WHP), Los Angeles, California. The airplane sustained substantial damage. The pilot/owner/builder, the sole occupant, was not injured. Visual meteorological conditions prevailed for the local area flight, and no flight plan had been filed. The flight was originating at the time. A Federal Aviation Administration (FAA) airworthiness inspector interviewed the pilot. Shortly after takeoff, abeam the tower at 100 feet agl, he felt a "jolt/engine burp" followed by a partial loss of engine power. He "backed off" the power, and landed on the remaining runway. The pilot reported that he had retracted the landing gear prior to the loss of power, and was not able to lower the landing gear prior to touchdown. The airplane contacted the runway, slid down the remaining runway, and came to a stop after impacting the airport perimeter fence. An FAA airworthiness inspector examined the airframe and engine. He removed the fuel injectors and noted debris in the number 2 fuel injector. He was not able to identify the debris, but indicated that it disintegrated when he touched it. A visual inspection of the cylinders revealed that the number 2 cylinder walls were white in appearance, akin to a lean running condition. The other cylinder walls were darker in appearance. He established mechanical and valve train continuity through manual rotation of the engine. The pilot/owner/builder also held a repairman experimental aircraft builder certificate for the accident airplane. According to the engine logbook, the last condition inspection had been completed on February 2, 2007. A differential compression check was conducted with no anomalies noted, and new spark plugs were installed. On March 12, 2007, the number 4 cylinder was removed for inspection of the intake valve. The pilot/owner replaced the "rings," reinstalled the cylinder on the engine, and tested it for leaks. He noted no discrepancies. According to the Airport Facility Directory, runway 12 at Whiteman Airport was 4,120 feet long by 75 feet wide. The airport tower was located midfield. The airplane collided with a fence during a rejected takeoff following a partial loss of engine power. The pilot reported that after the airplane lifted off the ground, he retracted the landing gear. Just abeam the tower, he felt a "jolt/engine burp," and noted that he was about 100 feet above the ground. He reduced the power, but was not able to lower the landing gear prior to the airplane touching down on the remaining runway. The airplane slid down the runway, and came to a stop after impacting the airport perimeter fence. A Federal Aviation Administration airworthiness inspector examined the engine following the accident and noted that the number 2 fuel injection nozzle was clogged with unidentified debris that would crumble when touched. Inspection of the number 2 cylinder combustion chamber revealed a white coloration on the cylinder walls consistent with a lean fuel condition. No anomalies were noted with the remaining fuel injection nozzles and the other cylinders' combustion chambers. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_LAX07CA120.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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