NTSB CAROL · Event
Event NYC99LA038
Registry · N42RR
FAA Aircraft Registry record.
Make / Model
BEECH 76
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
4 seats · 2 engines
Last airworthiness date
19861021
ADS-B equipped
Yes — Mode-S A4FACD
Registrant of record
WALLA WALLA UNIVERSITY
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor's delay in initiating remedial action. Factors include a wet runway, and the student's inability to maintain airplane directional control during a simulated, on-ground engine failure.
Factual narrative
On December 19, 1998, about 1430 Eastern Standard Time, a Beech BE-76 Duchess, N42RR, was substantially damaged during the takeoff roll at Cincinnati Municipal-Lunken Field (LUK), Cincinnati, Ohio. The certificated flight instructor and private pilot were uninjured. Visual meteorological conditions prevailed at the time of the accident. A round robin instrument flight plan was filed for the instructional flight, which was conducted under 14 CFR Part 91. According to the flight instructor, he was giving instruction to the private pilot in anticipation of a multi-engine flight test. It had rained earlier, and the runway was still wet. The instructor gave the private pilot a simulated engine failure during the takeoff roll. He allowed the airplane to accelerate, and pulled back the mixture to the left engine at approximately 30 knots. The airplane veered quickly to the left, about 30 degrees. The private pilot did not retard both throttles immediately, so the flight instructor advanced the mixture on the left engine; however, the corrective action was too late, and the airplane departed the runway. The flight instructor reduced the power, and the brakes were applied. The airplane continued through the wet grass, then ran into an elevated asphalt driveway at 10 to 15 knots. The nose gear collapsed, and the airframe was bent. The flight instructor was giving instruction to the private pilot in anticipation of a multi-engine flight test. It had rained earlier, and the runway was still wet. The instructor gave the private pilot a simulated engine failure during the takeoff roll. He allowed the airplane to accelerate, and pulled back the mixture to the left engine at approximately 30 knots. The airplane veered quickly to the left, about 30 degrees. The private pilot did not retard both throttles immediately, so the flight instructor advanced the mixture on the left engine; however, the corrective action was too late, and the airplane departed the runway. The flight instructor reduced the power, and the brakes were applied. The airplane continued through the wet grass, then ran into an elevated asphalt driveway at 10 to 15 knots. The nose gear collapsed, and the airframe was bent. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_NYC99LA038.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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