Probable cause
The partial loss of engine power during initial climb for undetermined reasons.
NTSB analysis
The accident occurred during initial flight testing of the experimental amateur-built airplane. The pilot reported that there were no anomalies with the engine during a before-takeoff engine check or when he applied power for takeoff. He stated that shortly after liftoff he perceived that the engine was not producing maximum takeoff power and that the engine tachometer was indicating several hundred rpm lower than expected. Since there was insufficient runway remaining to land safely, he elected to land on the airport's crossing runway. The left wingtip collided with terrain as he maneuvered the airplane toward the crossing runway. A postaccident examination of the airplane did not reveal any mechanical malfunctions or failures that would have precluded normal operation of the airplane. Additionally, the accident engine demonstrated the ability to produce rated horsepower during a postaccident operational test run. Although the potential for serious carburetor icing existed while operating at glide power, the postaccident investigation was unable to conclusively determine if carburetor icing had contributed to the partial loss of engine power.
Text from the NTSB. Open the NTSB docket for CEN11LA618 for the full record.
Event
- Date
- Sep 2, 2011
- Type
- Accident
- Place
- Marion, Illinois
- Nearest airport
- Williamson County Regional (KMWA)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Amateur-built Waiex
- N-number
- N100VY
- Category
- Airplane
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Flight test
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.