Zepp, VA, USA
N60579
CESSNA 150
The flight instructor reported that, during a long cross-country flight, they encountered deteriorating weather conditions, and to remain visual flight rules, he altered course and destination. En route and while approaching a ridge line, he "noticed that [the airplane's] airspeed started to drop toward 65 miles an hour." He added that "[he] thought that maybe [the airplane was] picking up carburetor ice and [he] reached for the carburetor heat and pulled it out." The student pilot reported that, after the flight instructor stated, "watch your airspeed," he looked at the rpm gauge and noted that it was indicating 1,800 to 1,900 rpm. He added that the flight instructor took over the flight controls and that the airplane then impacted the top of a ridge. The airplane sustained substantial damage to the right wing. Atmospheric conditions reported at the time of the accident around the accident site were conducive to serious icing at cruise power. It is likely that carburetor ice accumulated due to the student pilot's failure to apply carburetor heat and the flight instructor's delayed application of carburetor heat, which resulted in a partial loss of engine power.
The flight instructor reported that, during a long cross-country flight, they encountered deteriorating weather conditions, and in order to remain VFR, altered course and destination. En route, while approaching a ridge line, he "noticed that [the airplane's] airspeed started to drop toward 65 miles an hour". He added that "[he] thought that maybe [they] were picking up carburetor ice and [he] reached for the carburetor heat and pulled it out". The student pilot reported that after the flight instructor stated, "watch your airspeed", he looked at the Revolutions Per Minute (RPM) gauge and noted that it was indicating 1800-1900 RPM. He added that, the flight instructor took over the flight controls and the airplane impacted the top of the ridge. A review of multiple weather observation stations, located around the four corners of the accident site, revealed similar conditions, temperature 55°F, and dew point 43°F. Review of the Federal Aviation Administration Carburetor Icing Chart for the given temperature and dew point revealed that the conditions were conducive to "serious icing at cruise power". (For more information see Special Airworthiness Information Bulletin CE-09-35 in the public docket.) The airplane sustained substantial damage to the right wing.
A partial loss of engine power due to the formation of carburetor icing, which resulted from the student pilot’s failure to apply carburetor heat and the flight instructor’s delayed response in applying carburetor heat while operating in conditions conducive to carburetor icing.
Source: NTSB Aviation Accident Database
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