NTSB CAROL · Event
Event WPR25LA070
Registry · N1FB
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV7A
Year of manufacture
2009 · 15 years old at event
Engine
SUPERIOR IO-360 SER (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20090313
ADS-B equipped
Yes — Mode-S A00081
Registrant of record
ALALOU SAAD
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On December 22, 2024, about 1639 mountain standard time, an experimental amateur-built Van’s RV-7A, N1FB, was substantially damaged when it was involved in an accident near Gila Bend, Arizona. The pilot sustained minor injuries, and the passenger was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that about four minutes after departing Phoenix Goodyear Airport (GYR), Phoenix, Arizona, he leveled off at 4,400 ft msl and felt abnormal vibrations emanating from the engine. To troubleshoot the anomaly, he slowly enriched the mixture, and the engine continued to run rough. Additionally, he ensured that the fuel selector was in right fuel tank position and in the detent, the propeller control was full forward, and full throttle was applied, however, engine RPM appeared to be decreasing. The pilot stated that manipulation of the mixture control had no corresponding effect and he noticed that there was a lack of tension on the mixture control cable. He moved the throttle control about halfway toward idle, and the engine roughness slightly subsided, and engine appeared to lose total power. The pilot applied full throttle which produced a corresponding yet intermittent surge in engine power. The pilot contacted Albuquerque Center, transmitted that he had an engine failure, and made a left turn toward Gila Bend Municipal Airport (E63), Gila Bend, Arizona. Unable to make it to E63, the pilot initiated a forced landing to a field with tall desert vegetation. During the landing, the airplane nosed over. Post-accident examination of the airplane revealed that the left wing sustained substantial damage. The wreckage was recovered to a secure facility for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR25LA070.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 (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 ↗