NTSB CAROL · Event
Event NYC07CA184
Registry · N171TA
FAA Aircraft Registry record.
Make / Model
CESSNA 550
Year of manufacture
2000 · 7 years old at event
Engine
P&W CANADA PW530A
Seats / Engines
8 seats · 2 engines
Last airworthiness date
20241221
ADS-B equipped
Yes — Mode-S A11E8E
Registrant of record
TEAM AERO LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The certified flight instructor's delayed remedial action, which resulted in an in-flight collision with trees.
Factual narrative
The certified flight instructor (CFI) and a student pilot were practicing an engine failure, with a 180-degree turn, in a Schweizer 269C helicopter. According to the CFI, the student pilot attempted to "stretch," to reach a field to the helicopter's left, even though a more obtainable field was located to the helicopter's right. The CFI called for a go-around at 150 feet above the ground; however, when the student pilot rolled on the throttle and pulled up on the collective, the rpm began to drop quickly, and the helicopter continued to descend. The CFI took the controls; however, the helicopter struck pine trees, and descended to the ground. Examination of the helicopter by a Federal Aviation Administration inspector did not reveal any preimpact malfunctions; nor did the CFI report any. The CFI reported 340 hours of total flight experience, which included 238 hours accumulated in helicopters. The certified flight instructor (CFI) and a student pilot were practicing an engine failure, with a 180-degree turn. According to the CFI, the student pilot attempted to "stretch," to reach a field to the helicopter's left, even though a more obtainable field was located to the helicopter's right. The CFI called for a go-around at 150 feet above the ground; however, when the student pilot rolled on the throttle and pulled up on the collective, the rpm began to drop quickly, and the helicopter continued to descend. The CFI took the controls; however, the helicopter struck pine trees, and descended to the ground. Examination of the helicopter did not reveal any preimpact mechanical malfunctions. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_NYC07CA184.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, engine failure, go-around). 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 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
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