Casualties unknown

2005-11-16: Cessna 177 (N821KF) — New Bern, NC

New Bern, NC, US

On November 16, 2005, a Cessna 177 (registration N821KF) was involved in an aviation accident near New Bern, NC. Investigators recorded the probable cause as: The pilot's failure to activate the carburetor heat during approach resulting in a total loss of engine power due to carburetor ice. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A pilot on an IFR flight executed a VOR runway 22 approach without carburetor heat, resulting in an engine power loss at minimum descent altitude and a forced landing into a river.

Approach and Descent

The pilot was conducting an instrument flight rules (IFR) flight and received clearance from the controller for a VOR runway 22 approach at the destination airport. During the descent, the pilot did not apply carburetor heat. The aircraft's Let-Down procedures checklist states, "Carburetor Heat - AS REQUIRED to prevent carburetor icing."

Power Loss at Minimum Descent Altitude

Upon reaching the minimum descent altitude (MDA) for the approach, the pilot advanced the throttle but did not obtain an engine response. Recognizing that the runway could not be reached, the pilot executed a forced landing into a river.

Weather Conditions

The surface weather observation at the destination airport reported a temperature of 75 degrees Fahrenheit and a dew point temperature of 61 degrees Fahrenheit. Review of the Department of Transportation Icing Probability Chart indicates that under these conditions, an aircraft at glide power would encounter serious icing conditions.

Engine Examination

Following the incident, the engine was mounted in a test stand and connected to an alternate fuel and battery source. Engine controls and magneto grounding wires were installed, and the mixture control was safetied in the full rich position. The engine was started and ran at idle power. After warm-up, the throttle was advanced to full power, and the engine stabilized at a takeoff rpm of 2,000. The throttle was then returned to idle, the safety wire on the mixture was cut, and the engine was shut down using the mixture control.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20051209X01957. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.