NTSB CAROL · Event
Event NYC95LA134
Registry · N16WW
FAA Aircraft Registry record.
Make / Model
BELL HELICOPTER TEXTRON CANADA 429
Year of manufacture
2018
TCDS
R00003RD · BELL HELICOPTER TEXTRON CANADA LTD
Engine
P&W CANADA PW207D1/D2 (621 hp)
Seats / Engines
9 seats · 2 engines
Last airworthiness date
20180629
ADS-B equipped
Yes — Mode-S A0F15E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to assure that an inadequate oil supply was available fot the flight.
Factual narrative
On June 28, 1995, about 0820 eastern daylight time, a Piper PA-24-180, N16WW, collided with a mobile home after a forced landing at the Morehead-Rowan County Airport (I32), Morehead, Kentucky. The airplane was substantially damaged. The private pilot and one passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed. The personal flight was being conducted under 14 CFR Part 91. While en route from Huntington, West Virginia to Broomfield, Colorado, and at a cruise altitude of 4500 feet mean sea level, the pilot stated that the "annunciator lights started blinking and then became solid." The pilot then noted that the oil pressure "needle registered no oil." The engine lost power, and the pilot elected to land at I32. The airplane touched halfway down runway 23, which had high obstructions at the approach end, and was 2600 feet long and 75 feet wide. The pilot stated she was unable to stop the airplane on the remaining runway, skidded across "low grass with a heavy dew" and impacted with the back porch of a mobile home. The FAA examined the engine at the accident site and observed that it was depleted of oil. The engine was disassembled on July 14, 1995. The following discrepancies were noted by the FAA Inspector during the disassembly: Both compression rings on number two (2) cylinder were fractured in several pieces; the camshaft was engraved with the wording "Not a certified part;" and all eight rod bolt nuts were installed upside-down. The engine records, revealed that the last overhauled on the engine was on July 5, 1992. The private pilot's total flight time was 1,400 hours, of which 200 hours were in this make and model airplane. At the time of the accident the wind was variable, from 230 degrees. THE PILOT STATED THAT WHILE AT A CRUISE ALTITUDE OF 4,500 FEET MSL THE 'ANNUNCIATOR LIGHTS STARTED BLINKING AND THEN BECAME SOLID.' HE THEN NOTED THAT THE OIL PRESSURE 'NEEDLE REGISTERED NO OIL.' THE ENGINE LOST POWER, AND THE PILOT ELECTED TO LAND AT THE NEAREST AIRPORT. THE AIRPLANE TOUCHED DOWN HALFWAY DOWN A 2,600-FOOT RUNWAY WHICH HAD HIGH OBSTRUCTIONS AT THE APPROACH END. THE PILOT WAS UNABLE TO STOP THE AIRPLANE ON THE REMAINING RUNWAY, SKIDDED ACROSS GRASS WITH HEAVY DEW AND IMPACTED A BACK PORCH OF A MOBILE HOME. EXAMINATION OF THE ENGINE REVEALED IT WAS DEPLETED OF OIL. THE ENGINE TEARDOWN REVEALED THAT BOTH COMPRESSION RINGS ON THE NUMBER TWO CYLINDER WERE FRACTURED IN SEVERAL PIECES; THE CAMSHAFT WAS ENGRAVED WITH THE WORDING 'NOT A CERTIFIED PART;' AND ALL EIGHT ROD BOLT NUTS WERE INSTALLED UPSIDE DOWN. THE ENGINE RECORDS REVEALED THAT THE LAST ENGINE OVERHAUL WAS ON 7/5/92. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_NYC95LA134.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 (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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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