NTSB CAROL · Event
Event FTW93LA261
Registry · N44680
FAA Aircraft Registry record.
Make / Model
POWRACHUTE PEGESUS
Year of manufacture
2004
Engine
ROTAX 582SER (65 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20080124
ADS-B equipped
Yes — Mode-S A56470
Registrant of record
DRONE DENNIS E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
AN INADVERTENT STALL WHEN THE PILOT LOWERED THE LANDING GEAR. A FACTOR WAS A LEAKING O-RING IN THE PROPELLER GOVERNOR.
Factual narrative
On September 17, 1993, at approximately 1015 mountain daylight time, N44680, a Culver V, struck power lines and impacted terrain during a landing approach to Seven Rivers Airport, Carlsbad, New Mexico. The airplane was destroyed, and the private pilot and passenger received minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight. According to the pilot, he took off on runway 10 and climbed to 150 feet AGL (above ground level). He raised the landing gear, then noted light colored smoke coming from the right side of the engine cowling and the engine began losing power. The pilot turned back towards the airport and aligned the airplane with runway 22, losing about 50 feet in the process. The pilot saw high power lines ahead. He reported that he lowered the landing gear and the left wing dropped and he "could not recover." When the left wing contacted the power lines control was lost and the airplane impacted the ground. Post-accident investigation disclosed a deteriorated O-ring in the propeller governor was leaking. There was no evidence of fire within the engine compartment. THE AIRPLANE TOOK OFF AND CLIMBED TO AN ALTITUDE OF 150 FEET. AS THE PILOT RETRACTED THE LANDING GEAR HE NOTICED A LIGHT COLORED SMOKE COMING FROM THE ENGINE COWLING AND THE ENGINE BEGAN LOSING POWER. THE PILOT TURNED THE AIRPLANE BACK TOWARDS THE AIRPORT AND ALIGNED IT WITH THE RUNWAY. WHEN THE PILOT LOWERED THE LANDING GEAR THE LEFT WING DROPPED AND THE PILOT COULD NOT RECOVER. THE AIRPLANE STRUCK POWER LINES AND IMPACTED THE GROUND OUT OF CONTROL. POST-ACCIDENT INVESTIGATION DISCLOSED A DETERIORATED AND LEAKING O-RING IN THE PROPELLER GOVERNOR. THERE WAS NO EVIDENCE OF FIRE IN THE ENGINE COMPARTMENT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_FTW93LA261.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). 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
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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗