QUICKSILVER GT400 near Bolingbrook, IL — 2011-09-10
- Date
- 2011-09-10
- Location
- Bolingbrook, IL, USA
- Airport
- 1C5
- Aircraft
- QUICKSILVER GT400
- Registration
- N2590A
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Initial climb
Probable cause
The loss of engine power for reasons that could not be determined during postaccident examination of the engine or airframe.
NTSB narrative
The pilot reported that following a slight reduction in engine power during climb-out a crackling sound was heard. The pilot stated that the engine then “faltered.” He moved the throttle full forward and there was no improvement in engine performance, so he made an off-field landing. The airplane was not operating in conditions favorable for the formation of carburetor icing, and the engine did not exhibit any anomalies during a postaccident engine run. The reason for the loss of engine power could not be determined.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have checked fuel system for anomalies before flight.
NTSB coding
Evidence available
- Photos
- 6 docket documents
Docket documents6
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Correspondence - Kit Manufacturer's Comments In Reference To A Primer Bulb By-pass Fuel Lineother
- Miscellaneous - Austrian Civil Aviation Safety Investigation Authority Commentsother
- Miscellaneous - Carb Icing Chartother
- Miscellaneous - Rotax supplied fuel system documentationother
- Photo - View of the engine operation during a test runphotos
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