CZECH AIRCRAFT WORKS SPOL SRO SPORTCRUISER near Swainsboro, GA — 2008-10-05
- Date
- 2008-10-05
- Location
- Swainsboro, GA, USA
- Aircraft
- CZECH AIRCRAFT WORKS SPOL SRO SPORTCRUISER
- Registration
- N742EA
- Category
- Airplane
- Highest injury
- Minor
- Fatalities
- 0
- Phase of flight
- Cruise
Probable cause
A loss of engine power due to carburetor icing as a result of the pilot's failure to use carburetor heat.
NTSB narrative
The pilot was performing slow flight over his property at 60 knots and 1,000 feet above ground level. He noticed that the airplane was descending and applied full throttle. The engine did not respond as expected, so he looked for a place to land. He did not recall if the engine stopped running. While attempting a forced landing, the airplane collided with trees and terrain in a wooded area. Examination of the airframe did not reveal evidence of a preimpact malfunction or failure. Examination of the propeller at the accident site did not reveal evidence of rotation at impact. The carburetor heat control was found in the closed (cold) position. Following the recovery of the wreckage, the engine was tested on the airframe and attained 3,300 rpms with no misfiring or hesitation. The airplane had accumulated 88 hours since new. Review of a Federal Aviation Administration Carburetor Icing Probability Chart indicated "Serious icing (glide power)" for the reported temperature and dew point conditions.
Analysis
- Primary failure mode
- Engine power loss
- First missed decision gate
- Pilot could have checked carburetor settings before flight to prevent icing.
NTSB coding
Evidence available
- FDR / data
- Photos
- 14 docket documents
Docket documents14
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Miscellaneous - Memo of Record, Pilot Interview.interview
- Pilot's Written Statementinterview
- Reports from Federal Agencies - FAA Inspector's Statementinterview
- Witness Statementinterview
- Miscellaneous - Excerpt from Special Airworthiness Bulletin CE-09-35other
- Photo 1) Main Wreckage Against Trees. FAA digital photo.photos
- Photo 2) Main Wreckage, Side View. FAA digital photo.photos
- Photo 3) Fuselage with Wings and Top Cowl Removed After Recovery. NTSB digital photo.photos
- Photo 4) Top Spark Plugs. NTSB digital Photo.photos
- Photo 5) Engine Run. NTSB digital photo.photos
- Photo 6) Engine Monitoring System Display During Engine Run. NTSB digital photo.photos
- GPS 17 - Factual Report of Group Chairmanreport
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