FTW98LA179
1998-04-10 · CARLISLE, Arkansas, United States · Minor · 1 aircraft · Status: Completed
N7046Y has since been reassigned. It is now registered to a different aircraft (VAN'S AIRCRAFT RV-9A, built 2007), which was not involved in this event.
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight and inflight planning/decision, which resulted in fuel exhaustion and the lost of engine power. A factor was the lack of suitable terrain for a forced landing.
Factual narrative
On April 10, 1998, at 0800 central daylight time, a WSK-PZL-Mielec PZL-M-18 agricultural airplane, N7046Y, nosed over during a forced landing following a loss of engine power near Carlisle, Arkansas. The airplane was operated by Almond Aviation, Carlisle, Arkansas, under Title 14 CFR Part 137. The airline transport rated pilot received minor injuries and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the local aerial application flight and a flight plan was not filed. The flight departed the Carlisle Municipal Airport at 0740. During an interview, conducted by the FAA inspector, the pilot reported that this was the second aerial application flight for the day and he was spraying fungicide on the wheat fields. During the pull up of the airplane for the turn around maneuver, the engine began to cut out and using the wobble pump did not restore engine power. During the forced landing in a plowed field with soft ground, the airplane rolled about 400 feet before it flipped over to the inverted position. The FAA inspector and the operator examined the airplane at the site. Structural damage occurred to the cockpit, propeller blades, engine mounts, elevators, vertical stabilizer, and rudder. Flight control continuity was confirmed. There was no physical evidence of fuel leakage or spillage. The FAA inspector stated that the fuel tank reading "indications represented empty tanks." The operator stated that he determined the "aircraft ran out of fuel." On the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) the pilot stated that the fuel gauges indicated 1/2 full at the time of departure. At the time when the fuel gauges were indicating slightly over 1/4 full, engine failure occurred. During the forced landing to a plowed open field, the airplane rolled about 50 yards before the tires began sinking into the soft ground. The airplane nosed over, landed upside down, and slid backwards about 20 feet before stopping. While climbing for the turn-around maneuver during an aerial application, the engine began to lose power. Despite his efforts during using the wobble pump, the engine lost power. A forced landing was performed to a plowed, soft field. The airplane nosed over during the landing. The pilot reported that the fuel gages indicated over 1/2 at the time of departure, and slightly over 1/4 full when the engine lost power. Examination of the fuel tank revealed readings representative of 'empty.' Inspection of the fuel tanks did not reveal any fuel leakage or spillage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_FTW98LA179.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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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.
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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…