NTSB CAROL · Event
Event ATL82DA178
Registry · N4214Y
FAA Aircraft Registry record.
Make / Model
BELLANCA 7ECA
Year of manufacture
1977 · 5 years old at event
Engine
LYCOMING 0-235 SERIES (115 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19770304
ADS-B equipped
Yes — Mode-S A50251
Registrant of record
ANGRAN NATE J
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PILOT REPORTED THAT THE CARBURETOR HEAT OPERATED DURING AN ENGINE RUN-UP BEFORE TAKEOFF, AND THAT HE USED THE CARBURETOR HEAT DURING EACH LANDING. DURING A TOUCH-AND-GO, HE LIFTED OFF AT 65 KTS, BUT THE PLANE SETTLED AND WOULD NOT CLIMB OUT OF GROUND EFFECT. HE ABORTED THE TAKEOFF AND THE PLANE CONTINUED OFF THE END OF THE RUNWAY. THE PILOT SAID THAT HE INTENTIONALLY GROUND LOOPED THE PLANE TO AVOID OBSTRUCTIONS. DURING THE GROUND LOOP, THE LEFT MAIN GEAR ATTACHMENT U-BOLT FAILED AT AN OLD CRACK. AN INVESTIGATION REVEALED THAT A CARBURETOR HEAT CONTROL CLAMP WAS LOOSE AND ALLOWED THE CARBURETOR HEAT TO REMAIN "OFF." THE CABLE HAD BEEN RE-RIGGED ABOUT 71 TACH HRS PRIOR TO THE ACCIDENT. ALSO, THE AIR INTAKE BOOT WAS IMPROPERLY POSITIONED AND ALLOWED UNFILTERED AIR TO ENTER THE CARBURETOR. THE TEMPERATURE AND DEW POINT WERE 81 AND 65 DEGREES FAHRENHEIT. ACCORDING TO ICING PROBABILITY CHARTS, A SERIOUS CARBURETOR ICING HAZARD WOULD HAVE OCCURRED AT LOW POWER SETTINGS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1982_ATL82DA178.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 ↗