NTSB CAROL · Event
Event LAX04CA326
Registry · N823WT
FAA Aircraft Registry record.
Make / Model
IAR SA BRASOV IAR 823
Year of manufacture
1976 · 28 years old at event
Engine
LYCOMING IO-540-G1D5 (290 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
20110603
ADS-B equipped
Yes — Mode-S AB3E06
Registrant of record
HILLERMAN DAVID A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to verify the fuel quantity on board prior to departure, which resulted in fuel exhaustion and loss of engine power due to an inadequate fuel supply.
Factual narrative
On September 20, 2004, about 1500 Pacific daylight time, an experimental IAR SA Brasov 823, N823WT, experienced a loss of engine power and collided with terrain during a forced landing near Denair, California. The pilot/owner was operating the airplane under the provisions of 14 CFR Part 91. The commercial pilot and one passenger were not injured; the airplane sustained substantial damage. The personal cross-country flight departed Reno/Stead Airport, Reno, Nevada, about 1330, with a planned destination of Turlock Municipal Airport, Turlock, California. Visual meteorological conditions prevailed, and a flight plan had not been filed. In a written statement, the pilot reported that he had flown to Reno several days prior to the accident, and during the duration of his stay, he parked the airplane in a tie down area on the ramp. Prior to departing, the pilot performed a preflight inspection, at which time he visually verified the airplane's fuel quantities by both physically looking inside the wing tanks, and by checking his fuel computer/totalizer inside the cockpit. The pilot did not use a dipstick or other means to physically verify the quantity. He estimated about 33 gallons of fuel on board, which he thought would be more than adequate for the 1- to 1 1/2-hour flight. Having flown the same route of flight many times before, he calculated the airplane's fuel burn to be about 13.4 gallons per hour. The pilot stated that while en route, he compared the "fuel remaining time" with the "time en route remaining" on his gauges numerous times. As he came in the proximity of Turlock, about 3 miles away, he maneuvered the airplane in a descent to 1,000 feet above ground level in preparation to enter the left downwind leg of the traffic pattern for runway 30. The engine coughed once and subsequently quit. In an effort to troubleshoot the engine's loss of power, he turned the boost pump to the "on" position, manipulated the mixture knob to the "full rich" position, and verified the fuel selector was in the "both" position. Despite his efforts, the engine would not restart and the pilot configured the airplane for an emergency landing; he opted to land between sprinkler systems in alfalfa field. While descending, the left wing tip contacted the ground first, and the landing gear touched down on the soft wet ground. The pilot further noted that after egressing the airplane, he tried to troubleshoot the engine failure. He discovered that the left wing tank was empty, and the right tank had a very minimal amount of fuel left inside. The fuel computer/totalizer indicated 13.1 gallons remaining. The airplane incurred damage to wings, landing gear, and propeller. After recovery, under the auspice of a Federal Aviation Administration inspector, the pilot drained both fuel tanks and found about 1 gallon of fuel remaining. The pilot opined that 12 gallons of fuel was siphoned from the airplane while on parked on the ramp at Reno. He stated that this missing amount of fuel would not be detected by the fuel calculator/ totalizer, and would be difficult to assess when visually inspecting the fuel tanks (about an inch difference). He further noted that the accident could have been prevented if he had used a quantity dipstick. The pilot reported no mechanical malfunctions of failures with the airplane prior to impact. The airplane experienced a loss of engine power and collided with terrain during a forced landing in a soft, wet field. Prior to departure, the pilot performed a preflight inspection, at which time he visually verified the airplane's fuel quantities by both physically looking inside the wing tanks, and by checking his fuel computer/totalizer inside the cockpit. The pilot did not use a dipstick or other means to physically quantify the fuel on board. He determined that he had a more than adequate amount of fuel for the 1- to 1 1/2-hour flight. While en route, the pilot compared the "fuel remaining time" with the "time en route remaining" on his gauges numerous times. As he came in the proximity of the airport the engine coughed once and subsequently quit. Despite his efforts, the engine would not restart and the pilot made an emergency landing. While descending, the left wing tip contacted the ground first, and the landing gear touched down on the soft wet ground. The pilot drained both fuel tanks and found about 1 gallon of fuel remaining. The pilot opined that 12 gallons of fuel was siphoned from the airplane prior to departure. The pilot stated that the accident could have been prevented if he had used a fuel quantity dipstick. The pilot reported no mechanical malfunctions of failures with the airplane prior to impact. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_LAX04CA326.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 (fuel exhaustion, engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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