ATL01LA053
2001-05-15 · Fort Lauderdale, Florida, United States · Minor · 1 aircraft · Status: Completed
Airport FXE
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO PRE-FLIGHT ADEQUATE FUEL FOR THE FLIGHT.
Factual narrative
On May 15, 2001, at 1337 eastern daylight time, a Cessna P337H, N1013V, collided with the ground 1/2 mile west of Fort Lauderdale Executive Airport in Fort Lauderdale, Florida. The local flight was operated by the pilot under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The airplane sustained substantial damage. The air transport pilot and passenger both received minor injuries. The flight departed Fort Lauderdale Executive Airport in Fort Lauderdale, Florida, at 1207 eastern daylight time. Reportedly, the pilot was conducting multiple approaches and landings. During the accident approach and landing, both engines lost power and the pilot initiated emergency procedures. During the emergency approach and landing, the airplane hit the middle marker beacon that is 1/2 mile west of the airport. Then the airplane impacted the ground, collided with a chain link fence, skidded across the south lane of NW 31st Avenue, through the medium, across the north lane of NW 31st Avenue and came to a stop on the chain link fence. Examination of the airplane showed the left wing tank was dry. Approximately 4.5 gallons of aviation fuel were recovered from the right wing tank. No noticeable fuel leaks were on the ground. Post accident investigation and engine run-up revealed no mechanical malfunction. The pilot was advised by the Fixed Base Operator Line Personnel that the airplane had only 38 gallons of total fuel on board. The pilot elected to fly without fueling up. The pilot told line personnel that the airplane had enough fuel for his 45 minute flight. Approximately one hour and 45 minutes later, the line personnel noticed that the airplane was down on the west side of the airport. According to Cessna, dual engine stoppage is possible if fuel is allowed to drop below 8.3 gallons. The pilot did not report any mechanical problems with the engines. WHILE MAKING A DAY VFR APPROACH TO THE DESTINATION AIRPORT, THE CESSNA EXPERIENCED A DUAL ENGINE FAILURE. THE AIRPLANE STRUCK THE MIDDLE MARKER BEACON THAT IS 1/2 MILE WEST OF THE AIRPORT. THEN IT IMPACTED THE GROUND AND SKIDDED THROUGH A CHAIN LINK FENCE. POST ACCIDENT INVESTIGATION REVEALED THE LEFT WING TANK WAS DRY. APPROXIMATELY 4.5 GALLONS OF FUEL WAS DRAINED FROM THE RIGHT TANK. POST ACCIDENT ENGINE RUN-UP REVEALED NO MECHANICAL MALFUNCTION, THE LOSS OF POWER WAS A RESULT OF FUEL EXHAUSTION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_ATL01LA053.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion, engine failure). All research papers
- arXiv 2022 · arXiv preprint Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
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- 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…