CHI99LA348
1999-09-26 · DES MOINES, Iowa, United States · None · 1 aircraft · Status: Completed
Airport DSM
Current FAA registration · N738FA
- Make / Model
- CESSNA 172N
- Year of manufacture
- 1977 · 22 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19771119
- ADS-B equipped
- Yes — Mode-S A9E941
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's improper in-flight planning and decisions which led to fuel exhaustion. A factor relating to this accident was the telephone pole.
Factual narrative
On September 26, 1999, at 2246 central daylight time, a Cessna 172N, N738FA, operated by a private pilot, sustained substantial damage when during a forced landing to a street in a residential neighborhood, the airplane's wing struck power lines and a pole, and subsequently impacted the ground. Previous to the forced landing, the airplane's engine lost power while descending for approach and landing at the Des Moines International Airport, Des Moines, Iowa. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted on a VFR flight plan operating under 14 CFR Part 91. The pilot reported no injuries. The cross-country flight originated at Woodruff, Wisconsin, at 1900 cdt, and was en route to Des Moines, Iowa. In his written statement, the pilot said that "he encountered engine failure" at 3,000 feet mean sea level. "An emergency landing was attempted on McKinley Street. Upon landing, I struck a telephone pole with the left wing." Federal Aviation Administration inspectors examined the airplane at the accident site. The airplane was found resting upright, backed up against some trees, in the hollow of a vacant lot, in a residential neighborhood located 1.6 miles east of the Des Moines International Airport. Preceding the airplane, a power pole was found pushed over. There was metal skin from the airplane's left wing suspended in a power line coming off of the pole. The airplane's left wing leading edge was torn out at mid-span. The airplane's right wing tip was broken off. The nose wheel was broken aft. The engine mounts and firewall were bent up and aft. The airplane's wing and fuselage skins showed heavy buckling and bending. The propeller showed no damage. Examination of the airplane's two main fuel tanks, which were found intact, revealed no fuel in either tank. Approximately 1 pint of fuel was recovered from the accumulator tank and lines to the engine. Flight control continuity was confirmed. Examination of the engine, engine controls and other airplane systems revealed no anomalies. The pilot said that 'he encountered engine failure' at 3,000 feet mean sea level. The pilot performed a forced landing to a street in a residential area, 1.6 miles east of the Des Moines International Airport, Des Moines, Iowa. The pilot said, 'Upon landing, I struck a telephone pole with the left wing.' Examination of the airplane's two main fuel tanks revealed no fuel. Approximately 1 pint of fuel was recovered from the accumulator tank and lines to the engine. No other anomalies were found. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_CHI99LA348.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.
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion, 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…