NTSB CAROL · Event
Event NYC99LA209
Registry · N312BW
FAA Aircraft Registry record.
Make / Model
MORRISEY 2150A
Year of manufacture
1962 · 37 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19620427
ADS-B equipped
Yes — Mode-S A34E6D
Registrant of record
GIACINTO LUCCI A JR
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's delay in applying carburetor heat which resulted in the loss of power, and his misjudgment of the flare during the forced landing.
Factual narrative
On August 24, 1999, at 1406 Eastern Daylight Time, a Morrisey 2150A, N312BW, was substantially damaged during a forced landing to a field near Ellisburg, New York. The certificated private pilot was seriously injured, and the passenger received minor injuries. Visual meteorological conditions prevailed at the time of the accident. No flight plan was filed for the local flight, which originated from Drake Airfield, Adams, New York. The personal flight was conducted under 14 CFR Part 91. According to the passenger, who was also the pilot's son, the passenger conducted the preflight inspection of the airplane. He stated that when he checked all three fuel tanks, they were absent of water and contaminants. He also checked all leading edges, rudders, flaps and ailerons. The pilot later performed a successful engine check, and afterwards, about 1335, they departed and headed out over Lake Ontario. En route, the pilot climbed the airplane to an unspecified altitude, then descended to 1,100 feet. Once at that altitude, the pilot attempted to increase power three times, and on the third attempt, the engine stalled. In an interview with Federal Aviation Administration (FAA) Inspectors, the pilot stated that he thought he had encountered carburetor icing, but that he had applied carburetor heat prior to the descent. He also stated that he recycled the heat when the engine lost power, then headed for a field. He left the flaps up during the descent, because he thought they would produce too much drag. The airplane reached the field, then dropped quickly, and impacted the ground in an upright position. The FAA Inspector said that the landing gear mounts were driven up through the wings, and that the airplane came to rest about 2/3 into a 600-yard by 250-yard field. Watertown International Airport (ART) was about 17 nautical miles north of the accident site. Weather recorded at 1350 included winds from 160 degrees magnetic at 8 knots, a temperature of 31 degrees Celsius, and a dewpoint of 11 degrees Celsius. An icing probability chart for those conditions indicated a probability of light icing - glide and cruise power. Although Watertown International Airport was the closest recording station to the accident, it was located inland, about 3 nautical miles from any large bodies of water. When the temperature and dewpoint were recorded there, the winds were coming from over the land. About 35 nautical miles to the northwest of the accident site was Kingston Airport (YGK), Kingston, Ontario. At 1400, winds there were recorded as being similar to Watertown's, from 160 degrees magnetic, at 6 knots. However, unlike Watertown, winds at Kingston had passed over the lake before reaching the recording station. Temperature and dewpoint results were different from those at Watertown, being recorded as 26 degrees Celsius, and 18 degrees Celsius, respectively. Using that data, an icing probability chart indicated a probability of moderate icing - cruise power, or serious icing - glide power. The pilot did not respond to requests for information. The pilot's latest third class medical certificate was issued on August 18, 1982. At that time, the pilot stated that he had 334 hours of flight time. The airplane was registered to the pilot on May 13, 1992. The airplane climbed to an unspecified altitude, then descended to 1,100 feet over Lake Ontario. The pilot attempted to increase power three times, and on the third attempt, the engine lost power. The pilot stated he applied carburetor heat prior to the descent, then recycled the heat when the engine lost power, and headed for a field. He left the flaps up during the descent to reduce drag. The airplane reached the field, then dropped quickly, and impacted the ground in an upright position. The landing gear mounts were driven up through the wings, and the airplane came to rest about 2/3 of the way into a 600- by 250-yard field. An icing probability chart indicated a probability of moderate icing - cruise power, or serious icing - glide power. The pilot's latest third class medical certificate was issued on August 18, 1982. At that time, the pilot had 334 hours of flight time. The airplane was registered to the pilot on May 13, 1992. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_NYC99LA209.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 (icing, stall). 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 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other
[Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…
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