NTSB CAROL · Event
Event ENG20LA043
Registry · N561NN
FAA Aircraft Registry record.
Make / Model
BOMBARDIER INC CL-600-2D24
Year of manufacture
2014 · 6 years old at event
Engine
GE CF34-8C5
Seats / Engines
95 seats · 2 engines
Last airworthiness date
20141217
ADS-B equipped
Yes — Mode-S A72BDA
Registrant of record
AMERICAN AIRLINES INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The windshield failed due to arcing from an inadequate solder connection at the anti-ice power terminal block.
Factual narrative
The damaged left side windshield (P/N NP139321-17 S/N 18338H6714) from N561NN was removed from the airplane and shipped to PPG Aerospace in Huntsville, Alabama. PPG examined the window in November 2020. The windshield serial number indicated that the windshield was a new unit and was completed in December of 2018. The subject windshield was installed on N561NN and had accumulated 3238.53 flight hours and 2870 flight cycles. PPG Aerospace completed manufacture of the window in December 2018. A teardown of the unit identified the failure origin underneath the power terminal block at the power braid A location. Removal of the terminal block and sealant revealed an arcing hot spot where the failure occurred at power braid wire position A. There was no visible solder at the connection point of braid wire A. The braid wire solder connection point at position B was still intact. The arcing/overheating of the braid wire caused the fire event in the cockpit. Removal of the terminal block and sealant revealed an arcing hot spot where the failure occurred at power braid wire position A. There was no visible solder at the connection point of braid wire A, which led to the arcing of the power braid wire and the fire event in the cockpit. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Aircraft-Aircraft systems-Ice/rain protection system-Ice/rain prot sys wiring-Failure
Verbatim from NTSB's published report. Source file
NTSB_2020_ENG20LA043.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…
Browse the full corpus — academia portal ↗