WPR24LA229
2024-07-02 · San Diego, California, United States · Minor · 1 aircraft · Status: In work
Airport MYF
Current FAA registration · N74C
- Make / Model
- CESSNA 172N
- Year of manufacture
- 1978 · 46 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19780202
- ADS-B equipped
- Yes — Mode-S A9F063
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On July 2, 2024, about 1200 Pacific daylight time, a Cessna 172N, N74C, was substantially damaged when it was involved in an accident near San Diego, California. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that he completed his preflight inspection of the airplane, started the airplane and taxied to the run-up area for runway 28R at the Montgomery-Gibbs Executive Airport (MYF), San Diego, California. After completing the pre-takeoff engine run-up and checklist, he taxied to and departed runway 28R, with the intent to depart the area from the downwind leg of the airport traffic pattern. During the right turn from crosswind to the downwind leg, , about 1,000 ft above ground level, he heard a loud “pop” and noticed brown smoke emanating from the engine compartment. The airplane began shaking and subsequently the engine lost power. After several attempts to contact the tower controller, the pilot declared an emergency and the tower controller cleared the airplane to land runway 10L. The pilot stated that he performed the engine failure checklist and landed on runway 10L. The airplane subsequently overran the departure end of the runway and nosed over. Postaccident examination of the airplane revealed damage to the engine mount and both wings. The recorded weather at MYF about 7 minutes before the accident showed that the wind was 240° at 6 knots. The airplane has been transported to a secure facility for further investigation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng cyl section-Failure
- — Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng cyl section-Design
Verbatim from NTSB's published report. Source file
NTSB_2024_WPR24LA229.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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…