Phoenix, AZ, USA
N971PA
Piper PA-44-180
The airplane veered off of the runway after the left engine lost power during the takeoff roll. The purpose of the flight was an intermediate stage-check for the student, prior to his multi-engine checkride. The preflight and run-up were uneventful. Approximately 5 seconds after the takeoff roll commenced, the left engine lost power and the airplane veered to the left. The CFI assumed control of the airplane, closing both throttles. The airplane continued turning to the left and the airplane departed the runway surface. The right main gear collapsed and the right engine impacted the ground and stopped. The left engine was idling after the airplane came to a stop. The left engine was test-run following the accident; no mechanical malfunctions were noted.
On November 20, 2003, at 1103 mountain standard time, a Piper PA 44-180, N971PA, veered off the runway during takeoff from the Deer Valley Airport (DVT), Phoenix, Arizona, collapsing the right main landing gear. Pan Am International Flight Academy was operating the flight under the provisions of 14 CFR Part 91. The certified flight instructor (CFI) and one commercial student were not injured; the airplane sustained substantial damage. Visual meteorological conditions prevailed and no flight plan had been filed. The local area flight was originating at the time. The Federal Aviation Administration (FAA) coordinator reported that the CFI and student were departing from runway 7R. During the takeoff roll, the airplane departed the runway to the left and came to rest in a dirt area next to the runway. The nose of the airplane was approximately 180 degrees from its original takeoff heading. In a written statement, the CFI reported that the purpose of the flight was for the student's intermediate stage check for a multiengine rating. After an uneventful run-up, the student powered up both engines and began the takeoff roll. The left engine sputtered and the airplane veered to the left. At this time, the CFI assumed control of the airplane and retarded both throttles. The airplane departed the runway 60 degrees left of the centerline. It traveled into the dirt and spun to the left, collapsing the right gear, and then the right engine impacted the ground and stopped. The left engine was running at idle. The CFI felt the accident could have been prevented if he had taken control of the airplane sooner. Furthermore, the CFI felt an emergency briefing covering all takeoff roll emergencies would assist in preventing future accidents. A post accident examination of the left engine by a mechanic and a test run did not reveal any mechanical malfunction that would have resulted in the partial loss of power.
the flight instructor's inadequate supervision of the flight and delayed remedial action, which resulted in a loss of directional control. The reason for the partial power loss in the left engine was not determined.
Source: NTSB Aviation Accident Database
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