FTW00LA104
2000-03-24 · ROANOKE, Texas, United States · Serious · 1 aircraft · Status: Completed
Airport 52F
Current FAA registration · N9847A
- Make / Model
- CESSNA 195A
- Year of manufacture
- 1950 · 50 years old at event
- Engine
- JACOBS L4 /R755-7 (245 hp)
- Seats / Engines
- 5 seats · 1 engine
- Last airworthiness date
- 19560604
- ADS-B equipped
- Yes — Mode-S ADBD4E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight resulting in loss of engine power due to water and rust contamination of the fuel. A factor was the lack of suitable terrain for the forced landing.
Factual narrative
On March 24, 2000, at 1530 central standard time, a Cessna 195A, single-engine airplane, N9847A, struck a tree and terrain following a loss of engine power during the takeoff/initial climb from runway 17 at the Northwest Regional Airport, near Roanoke, Texas. The airplane was owned and operated by the pilot under 14 Code of Federal Regulations Part 91. The private pilot, sole occupant, received serious injuries, and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the local flight, and a flight plan was not filed. The flight departed the airport approximately 1510. On the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot stated, in part: Preflight "Checked fuel-Visual; 30 gal each tank." During the second takeoff on runway 17, the "engine started to fail." The pilot performed a forced landing to an open field; however, during the left turn toward the field, the left wing of the airplane clipped a tree. The airplane came to rest approximately 60 yards east of the airport perimeter, upright in the field. The pilot reported "No catastrophic engine failure." A witness reported that he "heard the airplane making power sounded weak-idle-about 40 ft" agl. He further reported that the engine "quit about 3/4 down the runway." The FAA inspector responding to the accident site found "some contamination of rust and water in the fuel." The left wing leading edge and aileron were crushed aft, and the fuselage and cockpit were crumpled. The engine, propeller, and firewall were damaged. During the forced landing, following a loss of engine power on takeoff, the airplane struck a tree and terrain. The pilot reported that during the preflight he 'Checked fuel-Visual; 30 gal each tank.' He reported 'no catastrophic engine failure.' The FAA inspector responding to the accident site found 'some contamination of rust and water in the fuel.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_FTW00LA104.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 (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…