NTSB CAROL · Event
Event LAX97LA012
Aircraft involved
Probable cause & findings
the pilot's inadequate preflight planning/preparation and fuel consumption calculations resulting in fuel exhaustion. The pilot's failure to switch the fuel tanks to the auxiliary position and feather both propellers were factors.
Factual narrative
On October 8, 1996, at 2045 hours Pacific daylight time, a Cessna 310Q, N7833Q, crashed about 450 feet east of runway 28 at Truckee-Tahoe Airport, Truckee, California. The pilot was completing a visual flight rules personal flight. The airplane, registered to and operated by the pilot, sustained substantial damage. The certificated commercial pilot, the sole occupant, received serious injuries. Visual meteorological conditions prevailed. The flight originated at Reno International Airport, Reno, Nevada, about 2030. Safety Board investigators interviewed the pilot via telephone on October 8, 1996. The pilot said that when he was on the downwind leg of runway 28, he became preoccupied with the radios and forgot to switch the fuel tanks' selector handles from the auxiliary tanks to the main tanks. After he switched the fuel selector handles to the main tanks, both engines lost power. He attempted to restart the engines, but without success. The airplane's altitude was insufficient to make the airport and he landed short of the runway. The pilot also told the investigating FAA inspector from the Reno Flight Standards District Office that after both engines lost power, he turned on the boost pumps. He said that he didn't feather the propellers or retract the landing gear and was unable to extend the glide to the runway. The FAA inspector reported that he did not find any fuel in the main fuel tanks. He also said that the main fuel tanks and their associated components were not compromised during the impact sequence. While turning on the final approach, with the landing gear extended, the pilot switched the fuel tanks' selector handles from the auxiliary fuel tanks to the main fuel tanks. Shortly thereafter, both engines sustained a total loss of power. The pilot turned on the boost pumps to restart both engines, but without success. During the ensuing emergency landing, the pilot did not retract the landing gear or feather both propellers. The airplane landed about 450 feet short of the runway. The postaccident examination of the airplane disclosed that both main fuel tanks were empty. Neither the main fuel tanks nor their associated components were compromised during the impact sequence. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_LAX97LA012.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). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- AOPA Air Safety Institute 2023 · Safety advisor
Safety Advisor: Fuel Awareness
AOPA Air Safety Institute safety advisor on preventing fuel-exhaustion and fuel-starvation accidents in general aviation. Covers pre-flight fuel planning, reserve requirements (14 CFR 91.151, 91.167),…
- NASA NTRS 2019 · Abstract
U.S. Civil Rotorcraft Accidents, 1963 through 1997
The U.S. National Transportation Safety Board (NTSB) has recorded 8,436 rotorcraft accidents during the period mid - 1963 through the end of 1997.
- NASA NTRS 2019 · Contractor Report (CR)
A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2018 · Other
Parachuting to Safety
NASA's Langley Research Center awarded Ballistic Recovery Systems, Inc., three Small Business Innovation Research (SBIR) contracts to research and develop a new, low cost, lightweight recovery system …
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