ERA25LA281
2025-07-30 · Kissimmee, Florida, United States · None · 1 aircraft · Status: In work
Airport ISM
Current FAA registration · N121CW
- Make / Model
- CESSNA 172S
- Year of manufacture
- 2001 · 24 years old at event
- Engine
- LYCOMING IO-360-L2A (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 20011023
- ADS-B equipped
- Yes — Mode-S A057B0
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On July 30, 2025, at 11:28 eastern daylight time, a Cessna 172S, N121CW, was substantially damaged when it was involved in an accident near Kissimmee, Florida. The private pilot and flight instructor were uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. According to the flight instructor, the purpose of the flight was to provide commercial instruction for the private pilot. The instructor reported that during the preflight, the airplane had sufficient fuel, and the engine had sufficient oil for the cross-country flight. The pilot stated that the taxi, runup, and takeoff were all normal. After departing the Kissimmee Gateway Airport (ISM), Orlando, Florida, while climbing through 1,900 ft mean sea level (msl), both pilots reported feeling engine vibrations, and shortly after, heard a loud bang, and the windshield became covered with engine oil. The instructor took control of the airplane and began to head back to ISM; however, after determining that they had insufficient altitude to return to the airport, they elected to perform a forced landing on a road. The pilots reported their visibility was significantly reduced due to the oil covering the windshield. The pilot receiving instruction looked out the side window, and the instructor utilized her peripheral vision to guide the airplane onto the road. During the forced landing, the airplane impacted a car, and the airplane came to rest on the side of the road. A postaccident examination by the Federal Aviation Administration revealed that the fuselage sustained substantial damage and the engine had experienced a catastrophic internal engine failure. A large portion of the top crankcase had broken free from the rest of the crankcase, and the no. 2 connecting rod had released from its crankshaft journal. The wreckage was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_ERA25LA281.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (engine failure). All research papers
- 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…