NTSB CAROL · Event
Event NYC96LA149
Aircraft involved
Probable cause & findings
the pilot's improper aborted takeoff by extending full flaps which resulted in a porpoise. Subsequently, the airplane veered off the runway and the nose gear collapsed.
Factual narrative
On July 12, 1996 about 2130 eastern daylight time, a Cessna 172P, N98730, was substantially damaged during an aborted takeoff at the Essex County Airport, Fairfield, New Jersey. The certificated private pilot and passenger were not injured. Visual meteorological conditions prevailed for the local flight. There was no flight plan for the personal flight conducted under 14 CFR Part 91. The pilot stated that he had performed two previous takeoff and landings. During a third takeoff, the control wheel would not move aft, and he aborted the takeoff. During the aborted takeoff, the airplane porpoised and veered off the runway, where the nose gear collapsed, and the propeller struck the ground. According to a Federal Aviation Administration (FAA) Inspector, the pilot reported that during the aborted takeoff, he reduced power and extended full flaps. Examination of the wreckage by the FAA Inspector revealed no evidence of malfunctions with the airplane. In the Pilot's Operating Handbook, in the emergency procedures, for engine failure during takeoff run, it stated to 1. Throttle-IDLE. 2. Brakes-APPLY. 3. Wing Flaps-RETRACT. . . . The amplified procedures further stated: ". . .the most important thing to do is stop the airplane on the remaining runway. . . ." During the takeoff roll, the control wheel would not move aft, and the pilot performed an aborted takeoff. During the aborted takeoff, the pilot reduced power, and extended full flaps. The airplane then porpoised and veered off the runway collapsing the nose gear. Examination of the wreckage did not disclose evidence of mechanical malfunctions. The Pilot's Operating Handbook, stated to retract the flaps when aborting the takeoff. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_NYC96LA149.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 (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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…
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