Santa Fe, NM, USA
N378CT
FLIGHT DESIGN GMBH CTSW
On an instructional flight, a flight instructor and the pilot receiving instruction practiced touch and go landing maneuvers and were en route back to their destination. The pilot noticed the oil pressure had decreased and positioned the airplane to fly over a suitable landing environment. However, the oil pressure continued to decrease and when the pressure reached about 4 psi, the engine abruptly stopped. Subsequently, the flight instructor made a forced landing on a dirt field. During the ground roll, the nose wheel struck a rock and the airplane nosed over. Postaccident examination of the airplane revealed a leak in the oil line supplying oil to the engine. The leak in the oil line likely led to the loss of oil during flight and resulted in the abrupt loss of engine power. The damage to the oil line was consistent with heat damage, which was likely a result of it having been routed too close to the exhaust manifold.
On April 22, 2021, about 1004 mountain daylight time, a Flight Design GMBH, CSTW light sport airplane, N378CT, was substantially damaged when it was involved in an accident near Santa Fe, New Mexico. The flight instructor was not injured and the pilot receiving instruction sustained a minor injury. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. The flight instructor reported they were returning to their departure airport at an altitude of of about 7,500 ft mean sea level when he noticed the oil pressure had decreased and of theother engine indications appeared normal. He climbed to a higher altitude, monitored the oil pressure, and positioned the airplane to fly over a suitable landing environment. The oil pressure continued to decrease and when the pressure reached about 4 psi, the engine abruptly came to a complete stop. The flight instructor made a forced landing on a dirt field about 8 miles south of the airport. During the ground roll, the nose wheel struck a rock and the airplane nosed over. Additionally, the flight instructor reported that during the preflight inspection the oil level was correct and there were no indications of an oil leak A review of the data provided by the Dynon EMS-D120 device revealed the oil pressure steadily decreased for about the last 25 minutes of flight. About 3 minutes before the off-field landing, the oil pressure rapidly decreased to zero. Shortly thereafter, the engine rpm decreased to zero. Postaccident examination of the airplane revealed that the oil supply line from the oil tank to the oil pump, which supplied the engine, was observed to leak once compressed air was introduced into the line. The leak was in the area where the oil line rested against the exhaust manifold. The damage to the oil line was consistent with it being subjected to heat from the exhaust manifold. The oil line was connected correctly but routed to close to the exhaust manifold.
A leak in the oil line that supplied the engine with oil, which resulted in oil exhaustion and the total loss of engine power. Contributing to the accident was the routing of the oil line to close to the exhaust manifold.
Source: NTSB Aviation Accident Database
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