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Atlas / NTSB / ATL06CA015

NTSB CAROL · Event

Event ATL06CA015

2005-11-13 Bryson City, North Carolina, United States Airport · GKT Minor 1 aircraft Status: Completed

Aircraft involved

Probable cause & findings

The loss of engine power due to carburetor icing, and the pilot's failure to use carburetor heat.

Factual narrative

According to the pilot, approximately 30 minutes into the instrument flight after reaching a cruise altitude of 7,000 feet in the clouds the engine surged, and began to lose power. The pilot switched fuel tanks, and turned on the electric fuel pump. No fuel pressure was noted on the fuel gauge, and the engine did not regain full power. The pilot reported that he did not apply carburetor heat during the loss of engine power. The pilot radioed air traffic control, and declared an emergency. During the emergency landing the airplane collided with trees. Post-accident examination of the airplane revealed the fuselage was buckled; both wing assemblies were separated from the fuselage. Post-accident examination of the airplane revealed no mechanical or flight control anomalies. Review of Advisory Circular 20-113 item 7.A-8 states: If induction system ice is suspected of causing a power loss, apply full heat or alternate air. Do not disturb the throttle until improvement is noted. Expect a further power loss momentarily and then a rise in power as the ice is melted. According to the pilot, approximately 30 minutes into the instrument flight after reaching a cruise altitude of 7,000 feet in the clouds the engine surged, and began to lose power. The pilot switched fuel tanks, and turned on the electric fuel pump. No fuel pressure was noted on the fuel gauge, and the engine did not regain full power. The pilot reported that he did not apply carburetor heat during the loss of engine power. The pilot radioed air traffic control, and declared an emergency. During the emergency landing the airplane collided with trees. Post-accident examination of the airplane revealed the fuselage was buckled; both wing assemblies were separated from the fuselage. Post-accident examination of the airplane revealed no mechanical or flight control anomalies. Review of Advisory Circular 20-113 item 7.A-8 states: "If induction system ice is suspected of causing a power loss, apply full heat or alternate air. Do not disturb the throttle until improvement is noted. Expect a further power loss momentarily and then a rise in power as the ice is melted." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2005_ATL06CA015.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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.

Browse the full corpus — academia portal ↗