NTSB CAROL · Event
Event MIA01LA186
Registry · N1777W
FAA Aircraft Registry record.
Make / Model
MAGNI GYRO SRL M24 ORION PLUS
Year of manufacture
2022
Engine
ROTAX 915 IS (135 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20220225
ADS-B equipped
Yes — Mode-S A13690
Registrant of record
MAGNIFLIGHT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons and the pilot's failure to maintain adequate airspeed which resulted in a stall.
Factual narrative
On July 14, 2001, about 1230 eastern daylight time, a homebuilt Pitenpol Aircamper 1933, N1777W, registered to a private individual, operating as a Title 14 CFR Part 91 personal flight, impacted with terrain during a forced landing near Hernando, Florida. Visual meteorological conditions prevailed. No flight plan was filed. The airplane was destroyed. The commercial-rated pilot, and a passenger/owner reported serious injuries. The flight had departed from Spruce Creek, Florida, en route to Hernando, at 1100. The pilot stated, "...engine failure occurred...pilot attempted to re-start using back-up ignition with no results. Pilot then located an emergency landing site and negotiated landing...upon impact...landing gear collapsed and wing collapsed...fuel tank was ruptured and ignited...." According to the airplane's owner, who was seated in the front seat, "..…flight normal to within 5 miles of destination. Cruise speed 80 mph. Cruise altitude 800 feet. Shortly after power reduction to low cruise setting, engine quits. Pilot attempts re-start, but does not use carb heat. Pilot attempts a landing on a smooth field…..at approximately 80 feet AGL and 50 mph, pilot attempts sharp bank. Plane stalls and spins into ground..…plane ignites 60 seconds after impact..…engine recovered on Oct. 15, 2001, put on test stand and run. Engine runs perfectly. Engine torn down and inspected by A&P mechanic. No damage of any type found." According to the airplane's owner, at 800 feet cruise altitude, and within 5 miles of the destination airport, at a speed of 80 mph, and shortly after the pilot reduced power the engine stopped. The pilot attempted a re-start, without using carburetor heat, and was not successful. He attempted a forced landing in a field, but about 80 feet AGL and at 50 mph, he attempted a sharp bank, which resulted in a stall and spin into ground. The airplane ignited 60 seconds after impact. The engine was placed on test stand and ran without any discrepancies. In addition, the engine was torn down and inspected by an A&P mechanic. No damage of any type was found. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_MIA01LA186.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 (stall, 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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
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