No fatalities

19 Aug 2016: CESSNA 150 M (N9230U) — Aptis Aviation — Littleton, MA

Littleton, MA, United States

On 19 Aug 2016, a CESSNA 150 M (registration N9230U) operated by Aptis Aviation was involved in an aviation accident near Littleton, MA. No fatalities were reported. Investigators recorded the probable cause as: Engine failure due to carburetor ice. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On August 19, 2016, a Cessna 150M was substantially damaged during a forced landing near Littleton, Massachusetts. The student pilot was not injured. The engine lost partial then total power; carburetor ice was cited as the cause.

Accident Details

On August 19, 2016, at 1349 eastern daylight time, a Cessna 150M (registration N9230U) was substantially damaged when it impacted trees and terrain during a forced landing near Littleton, Massachusetts. The student pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the solo instructional flight, which operated under 14 CFR Part 91. The flight departed from Sanford Seacoast Regional Airport (SFM), Sanford, Maine, with the intended destination of Minute Man Air Field (6B6), Stow, Massachusetts.

According to the student pilot, he was on a solo cross-country flight and had topped off the fuel tanks with 100 low lead aviation fuel prior to departure. He departed 6B6, landed at Laconia Municipal Airport (LCI), Laconia, New Hampshire, and then continued to SFM. After departing SFM, while in a cruise descent from 4,500 feet mean sea level (msl) on a 4-mile straight-in approach to runway 21 at 6B6, the engine lost partial power when the rpm decreased from 2,500 to 1,300 rpm around 2,500 feet msl. The student thought he could make it to the runway but then began searching for a field to perform a forced landing. He located a field, turned toward it, and began troubleshooting. He advanced the mixture to full rich and applied carburetor heat; however, engine performance did not change. As he turned onto the final leg of the traffic pattern to the field, at about 800 feet msl, the engine lost total power. The pilot landed in the selected field, which was about 300 feet msl; the airplane impacted a stone wall and trees and came to rest upright.

Aircraft and Pilot Information

The student pilot received his student pilot certificate in September 2014. His most recent third-class medical certificate was issued on September 18, 2014. At the time of the accident, he had accumulated 73 hours of total flight time, of which 51 hours were in the same make and model as the accident airplane and 11 hours as pilot-in-command.

The airplane was manufactured in 1976, issued an airworthiness certificate in May 2015, and was registered to a flight school. It was equipped with a Lycoming O-200 series, 100-horsepower engine. According to the flight instructor, a 100-hour inspection was performed on August 4, 2016, at a total time of 8,216.4 hours and a tach time of 969 hours. At the time of the accident, the tachometer indicated 986.8 hours.

Engine Examination

Examination of the airplane revealed that both wings were partially separated from the fuselage and the leading edges were impact damaged. The engine was examined, and fuel was noted in the carburetor bowl. The fuel was free of water and debris. The rocker arm covers were removed, and no anomalies were noted. Crankshaft and valve train continuity was confirmed from the propeller to the accessory section by rotating the propeller. Evidence of compression was observed on all cylinders. The magnetos produced spark on all towers, the spark plugs exhibited normal wear, and were in "new condition." During recovery, about 10 gallons of fuel were drained from the airplane.

Weather Conditions

The reported weather around the time of the accident at Laurence G Hanscom Field (BED), Bedford, Massachusetts, located 10 miles east of the accident location, indicated wind from 330° at 4 knots, 10 miles visibility, few clouds at 6,000 feet above ground level, temperature 31°C, dew point 13°C, and an altimeter setting of 29.90 inches of mercury.

The carburetor icing probability chart from FAA SAIB CE-09-35 shows a probability of icing at glide and cruise power at the temperature and dew point reported at the time of the accident.

Probable Cause

According to the NTSB Pilot/Operator Report filed by the flight instructor, under the mechanical malfunction/failure section, it stated that the engine failed due to carburetor ice.