Piper PA-28-235 accident near Mulino, OR

On October 6, 1995, a Piper PA-28-235 (airplane) was involved in an accident near Mulino, OR. 2 people were seriously injured. Damage to the aircraft: substantial.

Date
October 6, 1995
Place
Mulino, OR
Aircraft
Piper PA-28-235 · Airplane
Injuries
0 fatal, 2 serious, 0 minor
Damage
Substantial
Position
45.200°N, 122.539°W
NTSB ID
20001207X04788

NTSB summary

On October 5, 1995, approximately 1730 Pacific daylight time, a Piper PA-28-235, N8845W, impacted a tree during an attempted forced landing about one-quarter mile south of Mulino Airport, Mulino, Oregon. The certified flight instructor and the private pilot both received serious injuries, and the aircraft sustained substantial damage. The local instructional flight, which had been in the air approximately one hour, was being operated in visual meteorological conditions. No flight plan had been filed, and there was no report of an ELT activation. According to the private pilot, who was the owner of the aircraft, the engine suddenly lost power while he was descending at less than cruise power. The power loss occured about five miles south of Mulino, and both pilots agreed they should try to glide to the airport at Mulino. While gliding toward Mulino, they unsuccessfully attempted to restart the aircraft's engine. As they neared Mulino Airport, they realized they did not have sufficient altitude to reach the airport, and therefore decided to attempt a landing in a field short of the airport. While attempting the emergency landing, the aircraft collided with a tree at the edge of the field. At the time of the accident, the nearest reported temperature and dew-point data was taken at Portland International Airport, about 40 miles north of Mulino. The temperature recorded at that time was 69 degrees fahrenheit, and the dew point was 44 degrees. According to the Carburetor Icing Probability Chart (DOT/FAA/CT- 82/44), the descent was taking place in conditions conducive to carburet

Probable cause

the failure of the pilots to use carburetor heat during a reduced power descent. A factor was the carburetor icing conditions.

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