NTSB CAROL · Event
Event ERA25LA361
Registry · N78938
FAA Aircraft Registry record.
Make / Model
CESSNA 172K
Year of manufacture
1968 · 57 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19681212
ADS-B equipped
Yes — Mode-S AAB4D7
Registrant of record
WINGS OVER TEXAS HOLDINGS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On September 20, 2025, about 1733 eastern daylight time, a Cessna 172K, N78938, was substantially damaged when it was involved in an accident near Salisbury, Connecticut. The flight instructor and pilot receiving instruction sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. The flight instructor reported that after departing they climbed to 7,000 ft mean sea level (msl) and had been in cruise flight for about 10 minutes when the engine rpm dropped about 100 rpm. The flight instructor turned on the carburetor heat and the engine rpm continued to drop to about 1,400 rpm as the airplane began to descend. The engine then began to “pulsate” between 1,400 and 2,000 rpm until the airplane reached about 3,500 ft msl, when the engine then experienced a total loss of power. The flight instructor reported the issue to air traffic control as soon as he noticed the engine rpm issues and was informed that the closest airport was 20 miles away. The flight instructor noted that they were flying above a racetrack and decided that would be the safest place to conduct the forced landing. He completed the “rough running engine in flight” and “engine failure during flight” checklists but was unable to restore engine power. The flight instructor subsequently conducted a forced landing to the racetrack. The airplane impacted a guardrail, which resulted in substantial damage to the engine mounts and fuselage. The airplane was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_ERA25LA361.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…
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