Othello, WA, USA
N7981Y
PIPER PA 30
The private pilot of the twin-engine airplane was preparing to take off for a cross-country flight. He reported that during the power up for takeoff, the left engine was at 2,200 rpm while the right engine was at 2,600 rpm. He leaned the mixture on the left engine to bring the rpm up to 2,600 and proceeded with the takeoff. After the takeoff roll, he started to climb the airplane and noted that the exhaust gas temperature on the left engine was much higher than on the right engine. The left engine rpm suddenly dropped to 2,000, and the airplane yawed to the left and started to descend. The pilot could not stop the yaw and descent, and the airplane impacted the ground, which resulted in substantial damage. The pilot reported that he should not have leaned the left engine for takeoff. A review of the left engine's logbook revealed a logbook entry about 4 months before the accident noting that the fuel flow divider, fuel servo, and turbo charger had been removed, repaired, and reinstalled. The entry also noted that a flow test was performed and that the engine was tested, checked for leaks, and returned to service. The airplane and engines were sold for salvage and were not available for examination; therefore, the reason for the partial loss of engine power could not be determined.
On July 17, about 1515 Pacific daylight time, a Piper PA-30 twin-engine airplane, N7981Y, was substantially damaged following a partial loss of power on the left engine, and a collision with terrain during takeoff/initial climb at the Othello Municipal Airport, Othello, Washington. The private pilot and the three passengers were not injured. The airplane was registered to Warden Air, LLC and operated by the pilot as a Title 14 Code of Federal Regulations Part 91 personal flight. An instrument flight rules (IFR) flight plan was filed for the cross-country flight. The airplane was departing at the time and was destined for Klamath Falls, Oregon. The pilot reported that during the power up for takeoff, the left engine revolutions per minute (RPM) was 2,200 while the right engine was 2,600 RPM. He leaned the mixture on the left engine to bring the RPM up to 2,600 and proceeded with the takeoff. After the takeoff roll he initiated a climb and noted that the exhaust gas temperature (EGT) on the left engine was much higher than the EGT of the right engine. The left engine RPM suddenly dropped to 2,000 RPM and the airplane yawed to the left and started to descend. The pilot was unable to overcome the yaw and descent, and the airplane impacted the ground. The pilot reported that he should not have leaned the left engine for takeoff. A review of the left engine's logbook revealed a logbook entry dated March 21, 2014 indicating that the fuel flow divider had been removed, repaired, and reinstalled. The fuel servo and turbo charger had also been removed, repaired, and reinstalled. The entry also noted that a flow test was performed, the engine was run tested and checked for leaks, and returned to service. The pilot did not provide the time the airplane had flown since the maintenance work was completed. The NTSB did not respond to the accident site and the wreckage was retained by the insurance company. Prior to examination, the wreckage and engines were sold for salvage and no longer available for examination.
The partial loss of engine power for reasons that could not be determined based on the available information.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
