NTSB CAROL · Event
Event WPR25LA069
Registry · N519CV
FAA Aircraft Registry record.
Make / Model
SLING AIRCRAFT (PTY) LTD SLING LSA
Year of manufacture
2022 · 2 years old at event
Engine
ROTAX 912 IS (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20230420
ADS-B equipped
Yes — Mode-S A68324
Registrant of record
AVIATION FINANCIAL CORP
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s decision to conduct a prolonged slip against warnings specified in the Pilot’s Operating Handbook which resulted in a total loss of engine power due to fuel starvation.
Factual narrative
The pilot reported that while about 3,000 ft mean sea level (msl), he slipped the airplane to descend 1,100 ft to get to the traffic pattern altitude. After leveling off, he saw the fuel pressure drop. He checked to make sure that both fuel pumps were on. Shortly after, the airplane lost all fuel pressure and engine RPM. After troubleshooting, he was unable to restore engine power, and initiated a forced landing to a golf course, where the airplane impacted trees and sustained substantial damage to the fuselage, empennage, and wings. The Pilot’s Operating Handbook for the airplane, stated in part “the fuel lift pipe in the fuel tank is situated adjacent to the lower inside wall of the tank. The aircraft should at no time be subjected to a sustained side slip towards a near empty fuel tank (i.e. -right wing down) as, despite the baffling, this may have the consequence that the fuel runs towards the outer edge of the tank exposing the fuel pipe to suck air, thereby starving the engine of fuel leading to engine failure. This poses a particular threat when at low altitude, typically prior to landing.” The pilot did not initially report that there was no mechanical malfunction or failure that would have precluded normal operation; however, upon reviewing the recorded flight data with his chief flight instructor, that included the bank angle indicator, slip/skid indicator, and fuel pressure, the pilot concluded that the loss of power was likely from the left fuel lift pipe becoming exposed, starving the engine of fuel. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Personnel issues-Action/decision-Action-Incorrect action performance-Pilot
- — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR25LA069.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 starvation, 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…
Browse the full corpus — academia portal ↗