Mitsubishi MU-2B-25 accident near Hillsboro, OR

On May 25, 2005, a Mitsubishi MU-2B-25 (airplane) was involved in an accident near Hillsboro, OR. 4 people died. Damage to the aircraft: substantial.

Date
May 25, 2005
Place
Hillsboro, OR
Aircraft
Mitsubishi MU-2B-25 · Airplane
Injuries
4 fatal, 0 serious, 0 minor
Damage
Substantial
Position
45.533°N, 122.950°W
NTSB ID
20050608X00732

NTSB summary

HISTORY OF FLIGHT On May 24, 2005, at 1752 Pacific daylight time, a Mitsubishi MU-2B-25, N312MA, registered to Max Aviation Inc. and operated by the pilot as a 14 CFR Part 91 personal flight, collided with the terrain shortly after takeoff from Portland-Hillsboro Airport, Hillsboro, Oregon. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft was substantially damaged and the commercial pilot and his three passengers were fatally injured. The flight was departing for Salem, Oregon. Several witnesses were around or on the airport at the time of the accident. One witness, a commercial pilot located in his office near the southwest side of runway 30, stated that he observed the aircraft land on runway 30, and then turn off about 1,320 feet from the end of the runway at the crossing runway. The aircraft was seen to taxi to Hillsboro Aviation where both engines were shut down. A short time later, this witness observed the aircraft make a tight turn-around between two rows of aircraft, and then proceed directly to runway 30 without stopping and roll onto the runway and take off. The witness stated that the flaps were down and that the aircraft was airborne by the crossing runway. After the aircraft rotated, he observed the aircraft in a steep climb angle. The aircraft gained an altitude of about 1,000 feet above ground level (agl) when the pitch attitude of the aircraft lowered slightly for a second before the aircraft entered a left hand turn that did not appear to be coordinated as the nose was pointing more towards the west, but the

Probable cause

The pilot's failure to obtain minimum controllable airspeed during the takeoff climb, which resulted in a loss of aircraft control when the left engine lost partial power. A fatigue failure to an oil tube, which resulted in the partial power loss to the left engine, procedures/directives not followed by the pilot, and the pilot's lack of recent experience and no recurrent training in the type of a

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