NYC90LA164
1990-07-14 · SHIRLEY, New York, United States · Minor · 1 aircraft · Status: Completed
Airport HWV
N44HH has since been reassigned. It is now registered to a different aircraft (DIAMOND AIRCRAFT DA 40 NG, built 2017), which was not involved in this event.
Aircraft involved
Probable cause & findings
THE PILOT'S LACK OF QUALIFICATIONS, THE IMPROPER USE OF FLIGHT CONTROLS, THE SECOND PILOT'S LACK OF QUALIFICATIONS, AND HIS DECISION TO SIMULATE THE ENGINE FAILURE.
Factual narrative
THE PILOT AT THE CONTROLS HELD A PRIVATE PILOT CERTIFICATE WITH A SINGLE ENGINE LAND AIRPLANE RATING. THE SECOND PILOT HELD A COMMERCIAL CERTIFICATE WITH A MULTI ENGINE RATING, BUT DID NOT HOLD A FLIGHT INSTRUCTOR CERTIFICATE. THE PRIVATE PILOT INITIATED A TAKEOFF IN THE MULTI ENGINE AIRPLANE AND WAS OBSERVED BY A POLICE OFFICER/PILOT TO BE APPROXIMATELY 75 TO 100 FEET IN THE AIR. THE AIRPLANE THEN DESCENDED AND CONTACTED THE GROUND OFF THE RIGHT SIDE OF THE DEPARTURE RUNWAY AFTER A SIMULATED ENGINE FAILURE. THE PILOT INDICATED HE HAD A TOTAL TIME OF 4 HOURS IN MAKE AND MODEL. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_NYC90LA164.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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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…