NTSB CAROL · Event
Event FTW03LA192
Registry · N9347T
FAA Aircraft Registry record.
Make / Model
CESSNA 172S
Year of manufacture
2012
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20120410
ADS-B equipped
Yes — Mode-S ACF7E4
Registrant of record
LEWIS UNIVERSITY
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power for an undetermined reason. A contributing factor was the lack of suitable terrain available for the forced landing.
Factual narrative
On August 7, 2003, at 2030 central daylight time, a Piper PA-38 single-engine airplane, N9347T, registered to and operated by private individuals, was destroyed during a forced landing following a partial loss of engine power during descent near Granbury, Texas. The airline transport pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The cross-country flight originated from San Marcos Municipal Airport (HYI), near San Marcos, Texas, at 1900, and was destined for the Pecan Plantation Airport (OTXI), near Granbury, Texas. The 11,000-hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that during a descent through 3,000 feet MSL the engine "ran rough for about 5 seconds, then went to 1,500 rpm." The pilot executed a forced landing into a nearby hay field, where the airplane landed hard and "flipped three times" coming to rest in an upright position. The FAA inspector, who responded to the accident site, reported that the fuselage aft of the cockpit was separated and folded underneath the cockpit area and the right wing. The vertical and horizontal stabilizers were bent. The wreckage of the aircraft was transported from the accident site to Southwest Texas Aviation, North Hangar, located in San Marcos, Texas, and examined by the FAA inspector. Engine continuity, compression and magnetos were checked and verified. The throttle and mixture were intact, and made full travel. The carburetor heat valve was intact; however, travel was partial due to the housing sliding in the clamp. The inspector was unable to verify if the fuel system was functional from the tank to the engine because the fuel had been removed. The owner of the aircraft stated to the inspector that all aspects of the fuel system were operating normally. Maintenance records were reviewed and no anomalies noted. According to the aircraft's maintenance records, the most recent annual inspection was completed on July 14, 2003. A partial loss of engine power occured during a descent through 3,000 feet MSL. The 11,000-hour pilot stated the engine "ran rough for about 5 seconds, then went to 1,500 rpm." The pilot executed a forced landing into a nearby hay field. Engine continuity, compression and magnetos were checked and verified. The carburetor heat valve was intact; however, travel was partial due to the housing sliding in the clamp. The FAA inspector was unable to verify if fuel system was functional from the tank to the engine because the fuel had been removed. Maintenance records were reviewed and no anomalies noted. According to the aircraft's maintenance records, the most recent annual inspection was completed on July 14, 2003. The reason for the loss of engine power was not determined. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_FTW03LA192.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 (maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- Semantic Scholar 2025 · Article (Applied Sciences)
Decision-Making Framework for Aviation Safety in Predictive Maintenance Strategies
The implementation of predictive maintenance (PM) in aviation presents unique challenges due to strict safety requirements, complex operational environments, and regulatory constraints.
- Embry-Riddle Scholarly Commons 2024 · Journal article (JAAER)
Low-Resource Automatic Speech Recognition Domain Adaptation – A Case-Study in Aviation Maintenance
With timeliness and efficiency being critical in the aviation maintenance industry, the need has been growing for smart technological solutions that optimize and streamline the different underlying ta…
- Embry-Riddle Scholarly Commons 2024 · Journal article (JAAER)
A New Trajectory in UAV Safety: Leveraging Reinforcement Learning for Distance Maintenance Under Wind Variations
In the field of aviation, safety is a critical cornerstone, and the operation of Unmanned Aerial Vehicle (UAV) systems is deeply connected with this principle.
- Embry-Riddle Scholarly Commons 2024 · Journal article (IJAAA)
Just Culture in Aviation: A Metaphorical Study on Aircraft Maintenance Students
Just Culture, a sub-dimension of safety culture, has been a prominent and debated topic in aviation safety in recent years.
- Embry-Riddle Scholarly Commons 2024 · Journal article (IJAAA)
Performance PRISM: A Comprehensive Framework For Performance Measurement In Aircraft Maintenance
Aircraft maintenance is governed by rigorous safety requirements and high operational complexity, demanding robust performance measurement frameworks to ensure optimal maintenance practices.
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