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Atlas / NTSB / FTW93LA261

NTSB CAROL · Event

Event FTW93LA261

1993-09-17 CARLSBAD, New Mexico, United States Airport · 62M Minor 1 aircraft Status: Completed

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 ↗.

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.

Browse the full corpus — academia portal ↗