NTSB CAROL · Event
Event ATL06IA071
Registry · N90CH
FAA Aircraft Registry record.
Make / Model
BEECHCRAFT CORP C90GTI
Year of manufacture
2014
Engine
P&W CANADA PT6A-135A (750 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
20140304
ADS-B equipped
Yes — Mode-S AC6D0D
Registrant of record
UNIT B LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The inadequate manufacturing process, which resulted in a windshield fire and subsequent emergency landing.
Factual narrative
On April 27, 2006, at 1425 eastern daylight time, a Beech C90A, N90CH, registered to Chartco, LLC, and operated by Carolina Air Charter, Inc., as a 14 CFR Part 91 corporate flight, encountered a windshield deicing mechanism fire in the cockpit while in cruise flight from Concord, North Carolina, to Washington Dulles International Airport, Dulles, Virginia. Instrument meteorological conditions prevailed, and an instrument flight rules flight plan was filed. The pilot and the two passengers reported no injuries, and the airplane received minor damage. The flight originated from the Concord Regional Airport, Concord, North Carolina on April 27, 2006, at 1331. According to the pilot, while in cruise flight at 17,000 feet, he smelled smoke. He stated that, a few seconds later, flames and smoke started shooting out of the lower left windshield. The pilot stated he believed it was the windshield heat unit, so he turned off the windshield heat, and the flames went out, but the smoke persisted. The pilot declared an emergency with air traffic controllers and diverted to Raleigh-Durham International Airport in Raleigh, North Carolina. The airplane landed safely, and the pilot and passengers deplaned on the tarmac. Examination of the airplane found scorch marks and soot on the left windshield near the terminal block. The damaged windshield was shipped to PPG Industries, Inc., for further examination. Examination revealed the unit showed a condition similar to other units that were found to have overheated blocks during late 1996 and early 1997. These blocks were subject to a joint investigation by Raytheon Aircraft Company and PPG during 1997. That investigation identified the root cause of the terminal block overheating, relating to the manufacturing process. The manufacturing process was corrected by PPG in August 1996. Raytheon issued Safety Communiqué No. 134, describing the events, part numbers affected, and procedures to perform in case of such an event. These procedures were added to the FAA-approved airplane operating handbook in June 1997. The damaged windshield from this incident was one of the windshields manufactured just prior to the correction of the manufacturer process. While in cruise flight at 17,000 feet, the pilot smelled smoke. A few seconds later, flames and smoke started shooting out of the lower left windshield. The pilot turned off the windshield heat, and the flames went out, but the smoke persisted. The pilot declared an emergency with air traffic controllers, diverted, and landed the airplane safely. Examination of the airplane found scorch marks and soot on the left windshield near the terminal block. The damaged windshield was shipped to the manufacturer, PPG Industries, Inc., for further examination. Examination revealed the unit showed a condition similar to other units that were found to have overheated blocks during late 1996 and early 1997. These blocks were subject to a joint investigation by Raytheon Aircraft Company and PPG during 1997. That investigation identified the root cause of the terminal block overheating, relating to the manufacturing process. The manufacturing process was corrected by PPG in August 1996. Raytheon issued Safety Communiqué No. 134, describing the events, part numbers affected, and procedures to perform in case of such an event. These procedures were added to the FAA-approved airplane operating handbook in June 1997. The damaged windshield from this incident was one of the windshields manufactured just before the manufacturing process was corrected. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_ATL06IA071.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). 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 · 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…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗