No fatalities

31 May 2013: CESSNA 172A — REID MATTHEW J — Eatonville, WA

Eatonville, WA, United States

On 31 May 2013, a CESSNA 172A operated by REID MATTHEW J was involved in an aviation accident near Eatonville, WA. No fatalities were reported. Investigators recorded the probable cause as: A partial loss of engine power due to carburetor icing and the pilot's failure to maintain adequate airspeed during a go-around, which resulted in a stall. 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

A pilot diverted after engine power loss suspected from carburetor ice. During go-around, engine failed to accelerate, leading to a stall and impact with a house.

Incident Summary

A pilot reported experiencing a loss of engine power while flying at 3,000 feet, after descending from 6,500 feet. Approximately 35 miles from the intended destination, the pilot reduced power and applied carburetor heat. Upon leveling off, the engine rpm stabilized between 1,800 and 2,000 rpm. Suspecting carburetor ice, the pilot applied carburetor heat again, but full power was not restored.

Diversion and Landing Attempt

The pilot diverted to a nearby airport and entered the traffic pattern for the northern runway. During the landing sequence, the pilot realized the aircraft would land long. Power was applied for a go-around, but the engine only accelerated to 1,500–1,600 rpm. While maneuvering in a left turn to avoid trees, the airplane stalled, entered a descent, and impacted a house.

Carburetor Icing Conditions

According to the carburetor icing chart, the reported temperatures at the time were conducive to serious carburetor icing. The Pilot's Handbook of Aeronautical Knowledge (FAA-H-8083-25A) notes that a decrease in engine rpm is the first indication of carburetor ice in an airplane with a fixed-pitch propeller. It further states that when conditions are favorable for carburetor icing, carburetor heat should be applied immediately and left on until all ice is removed. Applying partial heat or insufficient time may worsen the situation.

Postaccident Examination

Postaccident examination of the airframe and engine revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation.

Contributing factors

Attain/maintain not possibleEffect on equipmentPilot